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标题:
Flight Attendant Manual 747/400
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作者:
帅哥
时间:
2008-12-28 03:09:29
标题:
Flight Attendant Manual 747/400
Revision Number: 02 Revision Date: January 15, 2004 January 15, 2004 Copyright Information Boeing claims copyright in each page of this document only to the extent that the page contains copyrightable subject matter. Boeing also claims copyright in this document as a compilation and/or collective work. The right to reproduce, distribute, display, and make derivative works from this document, or any portion thereof, requires a license from Boeing. For more information, contact The Boeing Company, P.O. Box 3707, Seattle, Washington 98124. Boeing 707, 717, 727, 737, 747, 757, 767, 777, DC-8, DC-9, DC-10, MD-10, MD-11, MD-80, MD-90, BBJ, Boeing Business Jet, the Boeing logo symbol, and the red-white-and-blue Boeing livery are all trademarks owned by The Boeing Company; and no trademark license (either expressed or implied) is granted in connection with this document or otherwise. January 15, 2004 747-400 Flight Attendant Manual Preface Chapter 0 Table of Contents Section 0 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 0.0.1 0.0 Preface-Table of Contents Preface.....................................................................................................0 Airplane Description ...............................................................................1 Control Panels.........................................................................................2 Cabin Management System .................................................................2A Lighting...................................................................................................3 Communication.......................................................................................4 Lavatories................................................................................................5 Galleys ....................................................................................................6 Doors, Slides, and Emergency Exits.......................................................7 Emergency Equipment............................................................................8 Non-Normal Situation Guidelines ..........................................................9 Miscellaneous........................................................................................10 Crew Rest..............................................................................................11 June 1, 2001 747-400 Flight Attendant Manual Preface - Table of Contents Copyright © The Boeing Company. See title page for details. 0.0.2 D6-30151-TBC (pax) Intentionally Blank June 1, 2001 747-400 Flight Attendant Manual Preface Chapter 0 Model Identification Section 1 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 0.1.1 0.1 Preface-Model Identification General The airplanes listed in the table below are covered in this flight attendant manual. The numbers are used to distinguish data peculiar to one or more, but not all of the airplanes. Where data applies to all airplanes listed, no reference is made to individual airplane numbers. This TBC manual covers typical representative airplanes. This manual is intended as a general reference for Boeing organizations and customers who do not yet have a customized manual. The Flight Attendant Manual will be revised as necessary. Airplane Number Registry Number Serial Number Tabulation Number OEG VH-OEG 32911 RF003 008 HL7428 28552 RM071 January 15, 2004 747-400 Flight Attendant Manual Preface - Model Identification Copyright © The Boeing Company. See title page for details. 0.1.2 D6-30151-TBC (pax) Intentionally Blank January 15, 2004 747-400 Flight Attendant Manual Preface Chapter 0 Model Identification Section 1 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 0.1.1 0.1 Preface-Model Identification General The airplanes listed in the table below are covered in this flight attendant manual. The numbers are used to distinguish data peculiar to one or more, but not all of the airplanes. Where data applies to all airplanes listed, no reference is made to individual airplane numbers. This TBC manual covers typical representative airplanes. This manual is intended as a general reference for Boeing organizations and customers who do not yet have a customized manual. The Flight Attendant Manual will be revised as necessary. January 15, 2004 747-400 Flight Attendant Manual Preface - Model Identification Copyright © The Boeing Company. See title page for details. 0.1.2 D6-30151-TBC (pax) Intentionally Blank January 15, 2004 747-400 Flight Attendant Manual Preface Chapter 0 Introduction Section 2 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 0.2.1 0.2 Preface-Introduction Foreword The material in this publication provides introductory information about the Boeing 747-400 airplane and the information is operationally oriented. It must be understood that the material is general in nature and is not intended, in any way, to replace official engineering drawings, documents, and handbooks for the 747-400 airplane. It is suggested that appropriate sections of the Flight Crew Operations Manual and Airplane Flight Manual be consulted to supplement the material contained in this publication. General This Flight Attendant Manual (FAM) has been prepared by Boeing Commercial Airplanes, Commercial Aviation Services organization. The purpose of this FAM is to: • provide the guidelines and systems information the flight attendant needs to safely and efficiently operate the 777 airplane during all anticipated airline operations • serve as a reference for use during transition training for the 777 airplane • serve as a review guide for use in recurrent training and proficiency checks • establish standardized guidelines and practices to enhance Boeing operational philosophy and policy This manual is prepared for the owner/operator named on the title page specifically for the airplanes listed in the “Model Identification” section. It contains operational guidelines and information, which apply only to these airplanes. The manual covers the Boeing delivered configuration of these airplanes. Changes to the delivered configuration are incorporated when covered by contractual revision agreements between the owner/operator and The Boeing Company This manual is not suitable for use for any airplanes not listed in the “Model Identification” section. Further, it may not be suitable for airplanes that have been transferred to other owners/operators. January 15, 2004 747-400 Flight Attendant Manual Preface - Introduction Copyright © The Boeing Company. See title page for details. 0.2.2 D6-30151-TBC (pax) Owners/operators are solely responsible for ensuring the operational documentation they are using is complete and matches the current configuration of the listed airplanes. This includes the accuracy and validity of all information furnished by the owner/operator or any other party. Any questions about the content or use of this manual may be directed to: Commercial Aviation Services Boeing Commercial Airplanes P. O. Box 3707, M/C 20–89 Seattle, Washington 98124–2207 USA Attention: Senior Manager, Flight Technical Integration & Data Note: There are no plans for a future revision of this manual. Warnings, Cautions and Notes The following levels of written advisories are used throughout this manual: WARNING: An operating procedure, technique, etc., which may result in personal injury or loss of life if not carefully followed. CAUTION: An operating procedure, technique, etc., which may result in damage to equipment if not carefully followed. Note: An operating procedure, etc., considered essential to emphasize. Information contained in notes may also be safety related. January 15, 2004 747-400 Flight Attendant Manual Preface - Introduction Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 0.2.3 Page Numbering The FAM uses a decimal page numbering system. The page number is divided into three fields; chapter, section, and page. An example of a page number for the galleys chapter follows: chapter 6, section 10, page 3. Example Page Number Page Identification Each page is identified by a customer document number and a page date. The customer document number is composed of the general 747 FAM number, D6-30151–, and is followed by the customer identification. The page date is the date of publication of the manual or the most recent revision date. Example Page Identification Flight Attendant Manual Configuration Customer airplane configuration determines the data provided in this manual. The Boeing Company keeps a list of each airplane configuration as it is built and modified through the Service Bulletin process. The FAM does not reflect customer originated modifications without special contract provisions. 6.10.3 Page Number Chapter (Galleys) Section (Systems Description) D611W302-TBC Customer Identification 777 Flight Attendant Manual Number January 15, 2004 747-400 Flight Attendant Manual Preface - Introduction Copyright © The Boeing Company. See title page for details. 0.2.4 D6-30151-TBC (pax) Intentionally Blank January 15, 2004 747-400 Flight Attendant Manual Preface Chapter 0 Revision Record Section 4 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 0.4.1 0.4 Preface-Revision Record Revision Transmittal Letter To: All holders of The Boeing Company 747 flight attendant Manual, Boeing Document Number D6-30151-TBC (pax). Subject: Flight Attendant Manual Revision. This revision reflects the most current information available to The Boeing Company 45 days before the subject revision date. The following revision highlights explain changes in this revision. General information below explains the use of revision bars to identify new or revised information. Revision Record General The Boeing Company issues flight attendant manual revisions to provide new or revised procedures and information. Formal revisions also incorporate appropriate information from previously issued flight attendant manuals. The revision date is the approximate date the manual is mailed to the customer. Formal revisions include a Transmittal Letter, a new Revision Record, Revision Highlights, and a current List of Effective Pages. Use the information on the new Revision Record and List of Effective Pages to verify the flight attendant manual content. Pages containing revised technical material have revision bars associated with the changed text or illustration. Editorial revisions (for example, spelling corrections) may have revision bars with no associated highlight. The record above should be completed by the person incorporating the revision into the manual. No. Revision Date Date Filed No. Revision Date Date Filed 00 September 27, 2002 01 August 26, 2003 02 January 15, 2004 January 15, 2004 747-400 Flight Attendant Manual Preface - Revision Record Copyright © The Boeing Company. See title page for details. 0.4.2 D6-30151-TBC (pax) Filing Instructions Consult the List of Effective Pages (0.5). Pages identified with an asterisk (*) are either replacement pages or new (original) issue pages. Remove corresponding old pages and replace or add new pages. Remove pages that are marked DELETED; there are no replacement pages for deleted pages. Revision Highlights This section (0.4) replaces the existing section 0.4 in your manual. Be careful when inserting changes not to throw away pages from the manual that are not replaced. Using the List of Effective Pages (0.5) can help determine the correct content of the manual. Throughout the manual, airplane effectivity may be updated to reflect coverage as listed on the Preface - Model Identification page, or to show service bulletin airplane effectivity. Highlights are not supplied. This manual is published from a database; the text and illustrations are marked with configuration information. Occasionally, because the editors rearrange the database markers, or mark items with configuration information due to the addition of new database content, some customers may receive revision bars on content that appears to be unchanged. Pages may also be republished without revision bars due to slight changes in the flow of the document. Chapter 0 - Preface Section 2 - Introduction 0.2.1 - Title change of manual. Chapter 1 - Airplane Description Section 10 - Introduction Overview 1.10.1 - Chapter revised for cross-model standardization. Passenger and Attendant Seating 1.10.8 - Added warning concerning turbulent air operations. January 15, 2004 747-400 Flight Attendant Manual Preface List of Effective Pages Chapter 0 Section 5 * = Revised, Added, or Deleted Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 0.5.1 0.5 Preface-List of Effective Pages Page Date FAM * Title Page January 15, 2004 * Copyright January 15, 2004 0.0.1-2 June 1, 2001 * 0.1.1-2 January 15, 2004 * 0.1.1-2 January 15, 2004 * 0.2.1-4 January 15, 2004 * 0.4.1-2 January 15, 2004 * 0.5.1-2 January 15, 2004 Airplane Description (tab) * 1.TOC.0.1-2 January 15, 2004 * 1.10.1-2 January 15, 2004 1.10.3 June 1, 2001 * 1.10.4-16 January 15, 2004 Control Panels (tab) * 2.TOC.0.1-2 January 15, 2004 * 2.10.1-20 January 15, 2004 * 2.20.1-2 January 15, 2004 Cabin Management System (tab) * 2A.TOC.0.1-2 January 15, 2004 * 2A.10.1-8 January 15, 2004 * 2A.15.1-10 January 15, 2004 * 2A.20.1-4 January 15, 2004 * 2A.25.1-4 January 15, 2004 * 2A.26.1-2 January 15, 2004 * 2A.30.1-6 January 15, 2004 * 2A.40.1-2 January 15, 2004 Lighting (tab) * 3.TOC.0.1-2 January 15, 2004 3.10.1 June 1, 2001 * 3.10.2-7 January 15, 2004 3.10.8-10 June 1, 2001 * 3.10.11-12 January 15, 2004 * 3.10.13-14 Deleted Communications (tab) * 4.TOC.0.1-2 January 15, 2004 4.10.1-2 June 1, 2001 * 4.20.1-6 January 15, 2004 * 4.21.1-6 January 15, 2004 * 4.22.1-6 January 15, 2004 * 4.23.1-2 January 15, 2004 * 4.24.1-4 January 15, 2004 * 4.30.1-4 January 15, 2004 * 4.40.1-4 January 15, 2004 Lavatories (tab) * 5.TOC.0.1-2 January 15, 2004 5.10.1 June 1, 2001 * 5.10.2-12 January 15, 2004 * 5.10.13-14 Deleted 5.20.1 June 1, 2001 * 5.20.2-9 January 15, 2004 5.20.10 June 1, 2001 Page Date January 15, 2004 747-400 Flight Attendant Manual Preface - List of Effective Pages * = Revised, Added, or Deleted Copyright © The Boeing Company. See title page for details. 0.5.2 D6-30151-TBC (pax) Galleys (tab) * 6.TOC.0.1-2 January 15, 2004 * 6.10.1 January 15, 2004 6.10.2-4 June 1, 2001 * 6.10.5-12 January 15, 2004 6.20.1 June 1, 2001 * 6.20.2-6 January 15, 2004 Doors, Slides and Emergency Exits (tab) * 7.TOC.0.1-2 January 15, 2004 * 7.10.1 January 15, 2004 7.10.2 June 1, 2001 * 7.20.1-18 January 15, 2004 * 7.30.1-14 January 15, 2004 * 7.40.1-12 January 15, 2004 * 7.50.1-6 January 15, 2004 Emergency Equipment (tab) * 8.TOC.0.1-2 January 15, 2004 * 8.10.1-18 January 15, 2004 Non-Normal Situation Guidelines (tab) * 9.TOC.0.1-2 January 15, 2004 * 9.10.1-12 January 15, 2004 * 9.20.1-14 January 15, 2004 * 9.30.1-12 January 15, 2004 Miscellaneous (tab) * 10.TOC.0.1-2 January 15, 2004 10.10.1-2 June 1, 2001 Page Date Crew Rest (tab) * 11.TOC.0.1-2 January 15, 2004 * 11.10.1 January 15, 2004 11.10.2 June 1, 2001 * 11.10.3-10 January 15, 2004 * 11.20.1-2 January 15, 2004 11.20.3-12 June 1, 2001 * 11.30.1-12 January 15, 2004 (blank tab)
作者:
帅哥
时间:
2008-12-28 03:09:47
June 1, 2001 Page Date January 15, 2004 747-400 Flight Attendant Manual Airplane Description Chapter 1 Table of Contents Section 0 FCOM Template 12/12/98 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 1.TOC.0.1 1.0 Airplane Description-Table of Contents System Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.1 Overview . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.1 Airplane Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.1 Principal Dimensions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.2 Airplane Systems General . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.3 Auxiliary Power Unit (APU) . . . . . . . . . . . . . . . . . . . . . . . 1.10.3 Electrical Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.3 Air Conditioning and Pressurization . . . . . . . . . . . . . . . . . 1.10.3 Passenger Cabin . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.5 Cabin Management System . . . . . . . . . . . . . . . . . . . . . . . . 1.10.5 Cabin Doors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.5 Galleys . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.6 Food Cart Lift . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.6 Lavatories . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.6 Closets and Partitions . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.6 Crew Rest Area . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.7 Emergency Equipment Stowage . . . . . . . . . . . . . . . . . . . . 1.10.7 Passenger Overhead Stowage Bins . . . . . . . . . . . . . . . . . . 1.10.7 Passenger and Attendant Seating . . . . . . . . . . . . . . . . . . . . 1.10.8 Passenger and Attendant Seating Layout . . . . . . . . . . . . . 1.10.9 Passenger Service Units . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.11 Emergency Oxygen . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.11 Therapeutic Oxygen . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.11 Flight Deck Door . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.12 Flight Deck Security Door . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.12 Normal Flight Deck Access . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.14 Flight Deck Emergency Access Panel . . . . . . . . . . . . . . . 1.10.14 January 15, 2004 747-400 Flight Attendant Manual Copyright © The Boeing Company. See title page for details. 1.TOC.0.2 D6-30151-TBC (pax) Airplane Description - Table of Contents Intentionally Blank January 15, 2004 747-400 Flight Attendant Manual Airplane Description Chapter 1 Introduction Section 10 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 1.10.1 1.10 Airplane Description-Introduction Overview This chapter provides a general description of the airplane, principal dimensions, and passenger cabin. Airplane Description [Typical] [Typical] [Typical] [Typical] [Typical] Airplane model: 747-400 passenger Engines: General Electric CF6-80C2, rated at 62,100 pounds of thrust each Maximum takeoff weight (typical): 870,000 pounds (394,621 kilograms) Crew: Captain First Officer Observers (up to 2) Passenger: Flight Attendants: Upper Deck (up to 3) Main Deck (up to 18) Passenger seating capacity : 377 total: 12 First Class - Main Deck 32 Business Class - Upper Deck 24 Business Class - Main Deck 309 Economy Class - Main Deck Fuel capacity: 53,864 gallons (203,897 liters) Maximum operating altitude: 45,100 feet Maximum operating speed: 500 knots (0.83 Mach) January 15, 2004 747-400 Flight Attendant Manual Airplane Description - Introduction Copyright © The Boeing Company. See title page for details. 1.10.2 D6-30151-TBC (pax) [Typical] Principal Dimensions Passenger Range: 8,200 nautical miles 9,438 statue miles 15,186 kilometers 72' 9" 114' 5.5" 231' 10" 225' 2" 12' 7" 36' 1" 213' 0" 89' 5.5" 32' 5.5" 25' 0" 62' 6.5" 22.2m 34.9m 70.7m 68.5m 13.8m 11.0m 64.9m 27.26m 9.89m 7.6m 19.06m January 15, 2004 747-400 Flight Attendant Manual Airplane Description - Introduction Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 1.10.3 Airplane Systems General Auxiliary Power Unit (APU) An APU is mounted in the tail of the airplane. The APU is a gas turbine engine capable of operating both in the air and on the ground. On the ground, the APU provides the electrical power and pneumatic air necessary to operate the airplane systems if external ground services are not available. In flight, the APU is capable of serving as a back-up for the engine pneumatic air system at or below 15,000 feet. Electrical Power The electrical power system supplies 115 volt, 400 cycle AC and 28 volt DC electrical power to the airplane. On the ground, power can also be provided by the APU or by external power carts. If the electrical system loses one or more generators, electrical power to one or more galleys is removed automatically. Air Conditioning and Pressurization Normally, the pneumatic air for air conditioning and pressurization is supplied by the engines. The APU can also be used to supply bleed air. Temperature is controlled separately for the flight deck and for the passenger cabin. Cabin temperature is controlled automatically to maintain between 65 and 85 degrees F (18 to 29 degrees C) as selected by the flight crew. Temperature is controlled separately for the flight deck and for the passenger cabin. Flight attendants can control cabin temperatures manually for the upper deck and the five main deck passenger zones. Gasper air distribution outlets are provided for the main deck and upper deck passenger cabin. The cabin pressure is controlled automatically to provide a programmed cabin altitude. June 1, 2001 747-400 Flight Attendant Manual Airplane Description - Introduction Copyright © The Boeing Company. See title page for details. 1.10.4 D6-30151-TBC (pax) Intentionally Blank January 15, 2004 747-400 Flight Attendant Manual Airplane Description - Introduction Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 1.10.5 Passenger Cabin Cabin Management System The Advanced Cabin Entertainment/Service System (ACESS) is designed to control and monitor many cabin and passenger functions. Control panels for the ACESS are located at designated attendant stations. ACESS includes: the passenger services system, cabin lighting system, cabin interphone system, passenger address system, passenger entertainment system, and the cabin configuration system. The cabin configuration system consists of pre-programmed software with computer logic to automatically control system functions. It also defines and identifies passenger areas. See Chapter 2A, Cabin Management. The passenger services system includes the reading lights, call lights, passenger information signs, and chime functions. See Chapter 2A, Cabin Management, Chapter 3, Lighting, and Chapter 4, Communications, for detailed information. The cabin lighting system includes ceiling lights, sidewall wash lights, and night lights. See Chapter 3, Lighting. The cabin interphone system includes calls from the flight deck-to-attendants, attendant-to-attendant and the passenger address announcements. See Chapter 4, Communications. The passenger address system includes flight deck announcements, flight attendant announcements, pre-recorded announcements, entertainment and boarding music, and audio for the video system. See Chapter 2A, Cabin Management, and Chapter 4, Communications. The passenger entertainment system includes the video system, passenger address configuration, and entertainment audio. See Chapter 2A, Cabin Management. Cabin Doors The main passenger cabin is served by four entry doors, numbered 1L, 2L, 4L and 5L, located on the left side of the airplane. Service doors, numbered 1R, 2R, 4R and 5R, are located on the right side of the airplane. Doors 3L and 3R are overwing exits and are only used during an emergency. There are two upper deck doors which serve as emergency exits from the upper deck. See Chapter 7, Doors, Slides and Emergency Exits, for detailed information. January 15, 2004 747-400 Flight Attendant Manual Airplane Description - Introduction Copyright © The Boeing Company. See title page for details. 1.10.6 D6-30151-TBC (pax) Galleys The galleys have provisions for storing and preparing food and beverages. Removable containers, which insert and latch into the galley walls, are used for replenishment of supplies, food, beverages, and waste storage. The galleys are equipped with electrical power and water services. See Chapter 6, Galleys, for detailed information. Food Cart Lift An electrically powered food cart lift is installed for food service between the main and upper decks. The lift is located at the aft end of the upper deck passenger compartment and is capable of lifting a 250 pound (114 kilogram) food cart. Control panels are provided on both the main and upper decks adjacent to the lift. See Chapter 6, Galleys, for detailed information. Lavatories The airplane is equipped with lavatories on the main deck and upper deck. Each lavatory contains a toilet, wash basin, mirror, and all the necessary vanity items and disposal units. Some of the lavatories have baby care stations and handicap provisions. The lavatories contain two oxygen masks which deploy automatically during cabin depressurization. Ventilation is provided for each lavatory and air exhausts through overboard vents. See Chapter 5, Lavatories, for detailed information. Closets and Partitions [Typical] There is large coat closet is located in the forward (nose) section of the airplane. and a closet located on the upper deck. A closet is also located near doors 5L and 5R. Closets vary in size and can include coat rods or stowage shelves. Partitions, lavatories, and galleys are used to separate class seating. Some partitions have literature pockets and bassinet fittings installed. January 15, 2004 747-400 Flight Attendant Manual Airplane Description - Introduction Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 1.10.7 Crew Rest Area A cabin crew rest compartment is installed at Door 5 above the life raft support beam and the aft lavatories. Access is through a stairwell. The crew rest area can accommodate up to eight crew members. Oxygen, lighting, air conditioning, and emergency equipment are available. The door 5 overhead crew rest area is not certified for use during takeoff and landing. See Chapter 11, Crew Rest, for detailed information on the door 5 overhead crew rest compartment. A flight crew rest area is located on the forward left side of the upper deck and is accessible only from the flight deck. The crew rest area has two bunks and a wall mounted seat (for in-flight use only). Oxygen, lighting, air conditioning, interphone handset, and emergency equipment are available. The flight crew rest area is not certified for use during taxi, takeoff, or landing. Emergency Equipment Stowage Emergency equipment such as megaphones may be stored in the overhead bins. Additional stowage compartments for emergency equipment and other crew-related equipment are at or near the attendant stations. These stowage compartments may be floor or ceiling mounted units. See Chapter 8, Emergency Equipment, for locations and detailed information. Passenger Overhead Stowage Bins Overhead stowage bins running the length of the cabin over both the side and the center seats accommodate hats, coats, blankets, pillows, and most carry-on baggage. Emergency equipment may also be stored in the bins. Each bin has a placard stating its maximum weight capacity. January 15, 2004 747-400 Flight Attendant Manual Airplane Description - Introduction Copyright © The Boeing Company. See title page for details. 1.10.8 D6-30151-TBC (pax) Passenger and Attendant Seating Passenger Seating Accommodations are provided for each passenger class. A passenger control unit (PCU) is provided in each seat arm rest. Passengers use the PCU to make entertainment selections, turn the reading light on or off, or call for passenger service. Flight Attendant Stations Flight attendant stations are located at each door and include an attendant switch panel, service unit, attendant work lights, handset, and seats. Designated emergency equipment and a service unit containing oxygen masks are located at each flight attendant station. For details, refer to Chapter 8, Emergency Equipment. Flight Attendant Seating The flight attendant seats automatically return to the stowed position when unoccupied. A combination seat belt/shoulder harness and a padded head rest are installed in the seat. The harness functions as an inertia restraint device and retracts into a stowed position when not in use. The buckle has a release plate that must be moved through 90 degrees for release to occur. WARNING: Under turbulent air conditions or conditions where rapid airplane movement is expected, failure to firmly connect and properly adjust the flight attendant seat belt and shoulder harness (where available) may result in personal injury. Note: Flight attendants should use caution when standing or moving about the cabin during airplane taxi operations due to possible large or sudden airplane movements. January 15, 2004 747-400 Flight Attendant Manual Airplane Description - Introduction Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 1.10.9 Passenger and Attendant Seating Layout Upper Deck [Typical] A=Attendant Seat (3) • = Handset (2) AA• • A January 15, 2004 747-400 Flight Attendant Manual Airplane Description - Introduction Copyright © The Boeing Company. See title page for details. 1.10.10 D6-30151-TBC (pax) Main Deck [Typical] ** ** AA• AA• AA• AA• AA• AA• • AA• AA• A• A• A=Attendant Seat (18) • = Handset (11) January 15, 2004 747-400 Flight Attendant Manual Airplane Description - Introduction Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 1.10.11 Passenger Service Units The passenger service units are located immediately below the overhead stowage bins. Each unit has reading lights, controlled by a switch in the passenger seat arm rest, an attendant call light, and a seat locator sign. Emergency Oxygen Passenger oxygen masks are located in overhead modular compartments for both the outboard and center seating sections. One mask is supplied for each passenger seat and two for each lavatory. An extra mask is located in both the center and outboard passenger seat units. The system activates automatically if cabin altitude exceeds approximately 14,000 feet. If a group of masks fails to drop, the mask compartment can be released manually. Masks automatically drop from stowage and a continuous flow of oxygen is initiated when a mask is pulled. Pulling on one mask causes oxygen flow to all masks in that unit. The system can be manually activated by the flight crew at any altitude by pushing the passenger oxygen switch on the flight deck. Two oxygen masks are located in a compartment above each flight attendant station. See Chapter 8, Emergency Equipment System Description, for detailed information. Therapeutic Oxygen [Option: Theraputic Oxygen installed] The therapeutic oxygen system is an integral part of the passenger oxygen system. The therapeutic oxygen outlets are capable of providing oxygen to therapeutic masks without actuating all passenger masks. The therapeutic oxygen system can be activated at any altitude during normal flight by placing the Therapeutic Oxygen switch to the ON position. Prior to activation, at least one therapeutic oxygen mask must be plugged into an outlet. Therapeutic oxygen also activates automatically whenever the passenger oxygen system automatically activates. Passengers receive therapeutic oxygen through therapeutic masks plugged into the outlet on the PSUs. No oxygen flows from therapeutic oxygen outlets when masks are not plugged in. Oxygen flow can be reset by selecting the Therapeutic Oxygen switch to RESET position after all therapeutic masks are unplugged from the system. January 15, 2004 747-400 Flight Attendant Manual Airplane Description - Introduction Copyright © The Boeing Company. See title page for details. 1.10.12 D6-30151-TBC (pax) Flight Deck Door [Flight Deck Security Door: not installed] The flight deck door opens into the flight deck. When the door is closed, a viewing lens in the door allows observation of the passenger cabin. An electric lock latch mechanism, controlled by the flight deck door switch, allows the flight deck door to be locked. The door can be opened any time from the flight deck side. When the door is locked, a key is required to open the door from the passenger cabin side. The door unlocks with the loss of electric power. A break–away panel in the base of the door allows the door to open if the bottom of the door is jammed. A door latch mechanism allows the locked door to be forced open without permanent damage to the lock. Application of sufficient force opens the locked door in either direction. An angled door jam forces the door open into the flight deck in case of surrounding bulkhead deformation. CAUTION: Forcing the door open into the passenger cabin causes permanent damage.
作者:
帅哥
时间:
2008-12-28 03:10:01
Flight Deck Security Door [Flight Deck Security Door: installed] A lockable flight deck security door is installed to resist forcible entry by unauthorized personnel. In addition, the door meets the requirements for resistance to ballistic penetration and intruder entrance. The door opens into the flight deck. A viewing lens in the door allows observation of the passenger cabin. The door can be manually opened from the flight deck by turning the door handle. Entry to the flight deck is monitored by the flight crew. In the case of flight crew incapacitation, flight deck access may be gained through the use of the emergency access panel located on the right-side wall. January 15, 2004 747-400 Flight Attendant Manual Airplane Description - Introduction Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 1.10.13 1 Flight Deck Emergency Access Panel 2 Deadbolt Key Lock Note: The door incorporates a deadbolt with a key lock. Locking the deadbolt on the flight deck side prevents the key from unlocking the door on the passenger cabin side. 3 Door Handle FWD 1 2 5 3 4 ENT 1 2 3 Typical January 15, 2004 747-400 Flight Attendant Manual Airplane Description - Introduction Copyright © The Boeing Company. See title page for details. 1.10.14 D6-30151-TBC (pax) Normal Flight Deck Access Access to the flight deck is by permission of the flight crew. Doorbell Mode [Airline programmable option] If the doorbell mode is activated, an entry request to the flight deck is made by pressing "1" and then "ENT" on the emergency access panel on the right side of the door. A chime will sound on the flight deck and the flight crew may, at their discretion, authorize flight deck access. Flight Deck Emergency Access Panel A flight deck emergency access panel is located on the passenger side door post. The emergency access panel includes a six button keypad for entering the numeric access code along with red, amber, and green lights. The red light illuminates to indicate the door is locked. When the correct emergency access code is entered, the amber light illuminates. The green light illuminates to indicate the door is unlocked. The emergency access code is used to gain access to the flight deck in case of emergency or flight crew incapacitation. January 15, 2004 747-400 Flight Attendant Manual Airplane Description - Introduction Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 1.10.15 1 Keypad Push - enters 3 to 8 digit numeric access code. Entry of correct emergency access code sounds flight deck chime. 2 Access Lights Red (illuminated) - door locked. Amber (illuminated) - correct emergency access code entered. Green (illuminated) - door unlocked. 1 2 5 3 4 ENT 1 2 January 15, 2004 747-400 Flight Attendant Manual Airplane Description - Introduction Copyright © The Boeing Company. See title page for details. 1.10.16 D6-30151-TBC (pax) Normal Operation If emergency access to the flight deck is required, entry of the correct code causes: • a flight deck chime to sound • initiates the auto-unlock sequence Note: The illumination of the amber light on the access panel indicates that the correct emergency access code has been entered and the door is programmed to automatically unlock after a time delay. Note: If the flight crew decides to deny entry, the door remains locked and prevents further keypad entry for several minutes. Note: If the correct emergency access code is entered and the flight crew takes no action, the door unlocks for a short time after the expiration of a time delay. • the green indicator light on the emergency access panel illuminates when the door is unlocked January 15, 2004 747-400 Flight Attendant Manual Control Panels Chapter 2 Table of Contents Section 0 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 2.TOC.0.1 2.0 Control Panels-Table of Contents Overview . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.10.1 Attendant Switch Panels . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.10.1 Control Panels . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.10.2 Door 1L . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.10.2 Door 1R . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.10.3 Door 2L . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.10.4 Door 2R . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.10.6 Door 3L . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.10.8 Door 3R . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.10.9 Door 4L . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.10.10 Door 4R . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.10.11 Door 5L . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.10.12 Door 5R . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.10.13 Upper Deck Galley . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.10.14 Upper Deck Doors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.10.15 Cart Lift . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.10.16 Passenger Control Unit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.20.1 January 15, 2004 747-400 Flight Attendant Manual Copyright © The Boeing Company. See title page for details. 2.TOC.0.2 D6-30151-TBC (pax) Control Panels - Table of Contents Intentionally Blank January 15, 2004 747-400 Flight Attendant Manual Control Panels Chapter 2 Attendant Switch Panels Section 10 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 2.10.1 2.10 Control Panels-Attendant Switch Panels [Options shown: Emergency evacuation system, pre-recorded announcement system and boarding music system installed] Overview This chapter provides a general description of the various control panels located throughout the passenger cabin. The circled number adjacent to the panel refers to the chapter where a description and specific information may be found. Attendant Switch Panels An attendant switch panel (ASP) is installed at each attendant station. The ASP may be used to: • initiate passenger evacuation • silence the evacuation horn • turn on emergency lights • test emergency lights • turn on or off work lights. January 15, 2004 747-400 Flight Attendant Manual Control Panels - Attendant Switch Panels Copyright © The Boeing Company. See title page for details. 2.10.2 D6-30151-TBC (pax) Control Panels Door 1L [Typical; Option: Emergency evacuation system installed] SHUTOFF HORN EVACUATE COMMAND 8 4 3 January 15, 2004 747-400 Flight Attendant Manual Control Panels - Attendant Switch Panels Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 2.10.3 Door 1R [Typical; Option: Emergency evacuation system installed] HORN EVACUATE SHUTOFF COMMAND 8 4 3 January 15, 2004 747-400 Flight Attendant Manual Control Panels - Attendant Switch Panels Copyright © The Boeing Company. See title page for details. 2.10.4 D6-30151-TBC (pax) Door 2L [Typical; Option: Emergency evacuation system installed] SHUTOFF HORN EVACUATE COMMAND 4 8 3 2A January 15, 2004 747-400 Flight Attendant Manual Control Panels - Attendant Switch Panels Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 2.10.5 [Typical; Option: Pre-recorded announcemnt machine and boarding music installed] 1 4 3 2 1 CH VOL OFF 2 RSV NEXT CONT CANCL START PWR READY RSV ON ANNCMT ANNOUNCEMENT BGM 2 3 4 5 6 7 8 9 0 1 2A 2A January 15, 2004 747-400 Flight Attendant Manual Control Panels - Attendant Switch Panels Copyright © The Boeing Company. See title page for details. 2.10.6 D6-30151-TBC (pax) Door 2R [Typical; Option: Emergency evacuation system installed] SHUTOFF EVACUATE HORN COMMAND 2A 8 4 3 2A January 15, 2004 747-400 Flight Attendant Manual Control Panels - Attendant Switch Panels Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 2.10.7 [Typical] 2A January 15, 2004 747-400 Flight Attendant Manual Control Panels - Attendant Switch Panels Copyright © The Boeing Company. See title page for details. 2.10.8 D6-30151-TBC (pax) Door 3L [Typical; Option: Emergency evacuation system installed] HORN EVACUATE SHUTOFF COMMAND 8 3 4 January 15, 2004 747-400 Flight Attendant Manual Control Panels - Attendant Switch Panels Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 2.10.9 Door 3R [Typical; Option: Emergency evacuation system installed] HORN EVACUATE SHUTOFF COMMAND 8 3 4 January 15, 2004 747-400 Flight Attendant Manual Control Panels - Attendant Switch Panels Copyright © The Boeing Company. See title page for details. 2.10.10 D6-30151-TBC (pax) Door 4L [Typical; Option: Emergency evacuation system installed] HORN EVACUATE SHUTOFF COMMAND 8 2A 4 3 January 15, 2004 747-400 Flight Attendant Manual Control Panels - Attendant Switch Panels Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 2.10.11 Door 4R [Typical; Option: Emergency evacuation system installed] HORN SHUTOFF EVACUATE COMMAND 8 3 January 15, 2004 747-400 Flight Attendant Manual Control Panels - Attendant Switch Panels Copyright © The Boeing Company. See title page for details. 2.10.12 D6-30151-TBC (pax) Door 5L [Typical; Option: Emergency evacuation system installed] HORN EVACUATE SHUTOFF COMMAND 3 8 4 January 15, 2004 747-400 Flight Attendant Manual Control Panels - Attendant Switch Panels Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 2.10.13 Door 5R [Typical; Option: Emergency evacuation system installed] HORN EVACUATE SHUTOFF COMMAND 3 8 4 January 15, 2004 747-400 Flight Attendant Manual Control Panels - Attendant Switch Panels Copyright © The Boeing Company. See title page for details. 2.10.14 D6-30151-TBC (pax) Upper Deck Galley [Typical] 2A 4 January 15, 2004 747-400 Flight Attendant Manual Control Panels - Attendant Switch Panels Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 2.10.15 Upper Deck Doors [Option: Emergency evacuation system installed] HORN SHUTOFF EVACUATE 8 January 15, 2004 747-400 Flight Attendant Manual Control Panels - Attendant Switch Panels Copyright © The Boeing Company. See title page for details. 2.10.16 D6-30151-TBC (pax) Cart Lift Main Deck [Send only panel] CART LIFT READY DOWN READY UP OVERRIDE RESET POWER OFF TRANSIT IN M/D DOOR U/D DOOR NORMAL OPERATION UNSAFE/OPEN EMERGENCY STOP 6 January 15, 2004 747-400 Flight Attendant Manual Control Panels - Attendant Switch Panels Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 2.10.17 [Call/Send panel] CART LIFT EMERGENCY STOP READY DOWN READY UP OVERRIDE RESET POWER OFF TRANSIT IN UNSAFE U/DOOR NORMAL OPERATION 6 January 15, 2004 747-400 Flight Attendant Manual Control Panels - Attendant Switch Panels Copyright © The Boeing Company. See title page for details. 2.10.18 D6-30151-TBC (pax) Upper Deck [Send only panel] [Call/Send panel] NORMAL OPERATION U/DOOR UNSAFE RESET STOP EMERGENCY NORMAL OPERATION IN TRANSIT OVERRIDE UP READY DOWN READY C A R T L I F T UNSAFE/OPEN EMERGENCY STOP POWER OFF RESET M/D DOOR U/D DOOR 6 NORMAL OPERATION U/DOOR UNSAFE RESET POWER OFF RESET IN TRANSIT OVERRIDE UP READY DOWN READY STOP EMERGENCY C A R T L I F T 6
作者:
帅哥
时间:
2008-12-28 03:10:14
January 15, 2004 747-400 Flight Attendant Manual Control Panels - Attendant Switch Panels Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 2.10.19 Upper Deck Power Control DISCONNECT UPPER DECK CART LIFT POWER SWITCH RELEASE CONNECT MOTOR 1 MOTOR 2 HEAT PUSH TO RESET NORMAL OVERRIDE OVER OVER HEAT DISCONNECT UPPER DECK CART LIFT POWER SWITCH RELEASE CONNECT MOTOR 1 MOTOR 2 PUSH TO RESET NORMAL OVERRIDE HEAT OVER OVER HEAT 6 January 15, 2004 747-400 Flight Attendant Manual Control Panels - Attendant Switch Panels Copyright © The Boeing Company. See title page for details. 2.10.20 D6-30151-TBC (pax) Intentionally Blank January 15, 2004 747-400 Flight Attendant Manual Control Panels Chapter 2 Inflight Entertainment System Section 20 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 2.20.1 2.20 Control Panels-Inflight Entertainment System Passenger Control Unit There is a passenger control unit (PCU) located in the arm rest of each passenger seat. Passengers may use the PCU to make passenger entertainment selections, turn the reading light on or off, or call for passenger service. [Typical] VOLUME 4 January 15, 2004 747-400 Flight Attendant Manual Control Panels - Inflight Entertainment System Copyright © The Boeing Company. See title page for details. 2.20.2 D6-30151-TBC (pax) Intentionally Blank January 15, 2004 747-400 Flight Attendant Manual Cabin Management System Chapter 2A Table of Contents Section 0 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 2A.TOC.0.1 2A.0 Cabin Management System-Table of Contents Cabin Services Module Overview . . . . . . . . . . . . . . . . . . . . 2A.10.1 Cabin Services Module (CSM) . . . . . . . . . . . . . . . . . . . . 2A.10.2 Cabin Services Module Operations . . . . . . . . . . . . . . . . . . . 2A.10.4 Cabin Lighting Control . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.10.4 Reading Lights Control . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.10.4 Attendant Calls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.10.5 Passenger Entertainment System . . . . . . . . . . . . . . . . . . . . . 2A.10.6 Audio Entertainment System Operation . . . . . . . . . . . . . 2A.10.8 Passenger Service System . . . . . . . . . . . . . . . . . . . . . . . . 2A.10.8 Cabin Configuration Module Overview . . . . . . . . . . . . . . . . 2A.15.1 Cabin Configuration Module (CCTM) . . . . . . . . . . . . . . 2A.15.2 Cabin Configuration/Test Module Operations . . . . . . . . . . . 2A.15.8 Set the CCTM for Flight . . . . . . . . . . . . . . . . . . . . . . . . . 2A.15.8 Set Passenger Address Volume . . . . . . . . . . . . . . . . . . . . 2A.15.8 Change/Set No Smoking Areas . . . . . . . . . . . . . . . . . . . . 2A.15.9 Temperature Control Overview . . . . . . . . . . . . . . . . . . . . . . 2A.20.1 Cabin Temperature Control System . . . . . . . . . . . . . . . . 2A.20.1 Cabin Temperature Control Module . . . . . . . . . . . . . . . . 2A.20.2 System Operation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.20.4 Increase Target Temperature . . . . . . . . . . . . . . . . . . . . . . 2A.20.4 Decrease Target Temperature . . . . . . . . . . . . . . . . . . . . . 2A.20.4 Reset Target Temperature . . . . . . . . . . . . . . . . . . . . . . . . 2A.20.4 Door 5 Overhead Crew Rest Area Temperature Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.20.4 Lavatory Operation/Waste Quantity Overview . . . . . . . . . . 2A.25.1 Lavatory Operation/Waste Tank Module . . . . . . . . . . . . . 2A.25.2 Lavatory Operation/Waste Tank Operation . . . . . . . . . . . 2A.25.3 Potable Water Module Overview . . . . . . . . . . . . . . . . . . . . . 2A.26.1 Potable Water Module . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.26.1 Pre-recorded Announcement and Boarding Music System Overview . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.30.1 Pre-recorded Announcement System . . . . . . . . . . . . . . . 2A.30.2 January 15, 2004 747-400 Flight Attendant Manual Copyright © The Boeing Company. See title page for details. 2A.TOC.0.2 D6-30151-TBC (pax) Cabin Management System - Table of Contents Pre-recorded Announcement System Operation . . . . . . 2A.30.4 Boarding Music System . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.30.5 Boarding Music System Operation . . . . . . . . . . . . . . . . 2A.30.6 Cabin Management Non-normal Operations . . . . . . . . . . . 2A.40.1 Cabin Configuration/Test Module . . . . . . . . . . . . . . . . . 2A.40.1 January 15, 2004 747-400 Flight Attendant Manual Cabin Management Chapter 2A Cabin Services Module Section 10 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 2A.10.1 2A.10 Cabin Management-Cabin Services Module Cabin Services Module Overview Flight attendants use the Cabin Services Module (CSM) to control cabin lighting, passenger reading lights, area attendant call reset (passenger-to-attendant and lavatory-to-attendant reset), entertainment audio power and seat unit/reading light power. The passenger cabin is divided into seating areas. [Typical] CSMs are located at designated attendant stations at door 2L and the upper deck galley. January 15, 2004 747-400 Flight Attendant Manual Cabin Management - Cabin Services Module Copyright © The Boeing Company. See title page for details. 2A.10.2 D6-30151-TBC (pax) Cabin Services Module (CSM) 1 Area Description [Typical] Displays the selected area (Door 2L only): • FIRST CLASS • ECONOMY CLASS • ALL AREAS. Note: Display blanks after a period of inactivity. 1 2 3 4 5 7 6 January 15, 2004 747-400 Flight Attendant Manual Cabin Management - Cabin Services Module Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 2A.10.3 2 CABIN LIGHTING Switches Touch sensitive. Push - • configures lighting for selected passenger area • select light intensity for selected area by pushing NIGHT, LOW, MEDIUM, or HIGH switch. 3 READING LIGHTS Switches Touch sensitive. ON - illuminates all passenger service unit (PSU) reading lights in the selected area. NORMAL - allows passengers to control the PSU reading lights in the selected area. OFF - removes all electrical power from the reading lights in the selected area. 4 ATTENDANT CALL RESET Switch Touch sensitive. Push - extinguishes all passenger and lavatory call lights in the selected passenger area. 5 AREA SELECT Switch Push - pages through passenger areas controlled by panel. Note: If only one area is controlled by the CSM, pushing the AREA SELECT switch will not change the display. If the CSM controls more than one area, pushing the AREA SELECT switch will scroll through all areas controlled by that CSM, starting with ALL AREAS and then displaying the individually controlled areas. 6 Status Light (typical) Illuminated (white) - touch sensitive switch has been activated. 7 ATTENDANT CALL Light Illuminated (white). • active passenger call in displayed area • extinguishes when call is no longer active/reset. January 15, 2004 747-400 Flight Attendant Manual Cabin Management - Cabin Services Module Copyright © The Boeing Company. See title page for details. 2A.10.4 D6-30151-TBC (pax) Cabin Services Module Operations Cabin Lighting Control The ceiling, sidewall wash, and night lights are controlled by CSMs located through out the main deck cabin and the upper deck galley. Lighting can be selected for each separate area to conform with the desired activity. Each seating area can have a different lighting intensity or they can all have the same intensity level. To determine the cabin lighting intensity for each seating area, push the AREA SELECT switch and observe the cabin lighting switches for the illuminated light in the upper left-hand corner. Set Cabin Lighting To set the cabin lighting for a specific area: • push the AREA SELECT switch to select the area to be controlled • push the desired cabin lighting intensity level (NIGHT, LOW, MEDIUM, HIGH) • verify that the selected light intensity switch status light illuminates. Reading Lights Control Passenger seat reading lights are normally controlled at the passenger seat; however, switches on the CSM can also be used to control the reading lights. The status of the reading lights is indicated by the status light in the upper left-hand corner of the switch. If the status light is illuminated on either the ON or OFF switches, the passengers do not have control of the passenger service unit reading lights in the area selected. Set Reading Lights To set the passenger reading lights: • push the AREA SELECT switch to select the area to be controlled • push - • ON to turn on all reading lights in the selected area • NORMAL to enable passenger control of the reading lights • OFF to turn off all reading lights in the selected area. • verify the selected reading light switch status light illuminates. January 15, 2004 747-400 Flight Attendant Manual Cabin Management - Cabin Services Module Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 2A.10.5 Attendant Calls Passenger-to-attendant and lavatory-to-attendant service calls for the selected seating area are indicated on the CSM by the illumination of the attendant call light. Attendant service calls may be cancelled from the CSM. View Attendant Call Area To view attendant calls for a specific area, push the CSM AREA SELECT switch until the desired area is displayed. The AREA SELECT switch is used to scroll through the seating areas to determine which area made the call. The attendant call light will illuminate when a seating area with an active call is displayed in CSM area description. Attendant Call Cancel/Reset To cancel or reset the attendant calls for a specific area: • push the AREA SELECT switch to scroll the seating areas • area making the call will cause the attendant call light to illuminate • push the ATTENDANT CALL RESET switch. Note: Pushing the ATTENDANT CALL RESET switch will cancel all passenger-to-attendant and lavatory-to-attendant calls for the area displayed in the area description. It will also extinguish the seat row call lights and lavatory call lights in the selected seating area. Note: If the ALL AREAS selection is made, then all seat row call lights and lavatory lights will be reset for all areas controlled by that CSM. January 15, 2004 747-400 Flight Attendant Manual Cabin Management - Cabin Services Module Copyright © The Boeing Company. See title page for details. 2A.10.6 D6-30151-TBC (pax) Passenger Entertainment System Passenger entertainment system controls include the control of the audio entertainment system and the passenger service system through out the airplane. The audio entertainment switches on the CSM control the playing of the audio system and allow the selection of audio programs at the passenger service unit (PSU). The passenger service system switches on the CSM control the electrical power for the operation of the PA speakers, passenger reading lights, and the PSU row call light. January 15, 2004 747-400 Flight Attendant Manual Cabin Management - Cabin Services Module Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 2A.10.7 1 AUDIO ENTERTAINMENT Switches Touch sensitive. ON - allows the playing of the audio system. OFF - removes power from the audio system. 2 PASSENGER SERVICE SYSTEM Switches Touch sensitive. ON - applies electrical power to all overhead electrical units. OFF - removes electrical power from all overhead electrical units (inhibited in flight).
作者:
帅哥
时间:
2008-12-28 03:10:28
3 Status Light (typical) Illuminated - touch sensitive switch has been activated. 1 2 3 January 15, 2004 747-400 Flight Attendant Manual Cabin Management - Cabin Services Module Copyright © The Boeing Company. See title page for details. 2A.10.8 D6-30151-TBC (pax) Audio Entertainment System Operation Start Passenger Entertainment Audio To turn the inflight audio on, push: • the Audio Entertainment ON switch • verify that the status light in the upper left-hand corner of the ON switch illuminates. Stop Passenger Entertainment Audio To turn the inflight audio off, push: • the Audio Entertainment OFF switch • verify that the status light in the upper left-hand corner of the switch illuminates. Passenger Service System The passenger service units (PSUs) are powered before flight by pushing the passenger services system ON switch and observing that the ON light illuminates. The passenger service system switches are maintenance switches that control electrical power to the passenger reading lights, PA speakers, and PSU Row Call Light. During preflight, verify that the passenger services system ON light is illuminated. The OFF Switch is inhibited when the airplane is in flight. If OFF is indicated, the passengers will have no reading lights or PA speakers at their seats. When pushing the ON switch, note that the ON switch light illuminates in the upper left-hand corner and the OFF switch light is extinguished. PSU Power Preflight Prior to flight, verify that the passenger services system is ON and the status light is illuminated. This ensures normal system operation. The OFF switch is inhibited when the airplane is in flight. Note: If the passenger services system OFF switch is selected and the status light is illuminated, the passenger reading lights and PA system speakers will not operate. January 15, 2004 747-400 Flight Attendant Manual Cabin Management Chapter 2A Cabin Configuration/Test Module Section 15 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 2A.15.1 2A.15 Cabin Management-Cabin Configuration/Test Module Cabin Configuration Module Overview The Cabin Configuration/Test Module (CCTM) is the flight attendant's interface to the Advanced Cabin Entertainment/Service System (ACESS). It contains a four line display and switches to perform a variety of tasks. All operations associated with configuration database download, system self-tests, passenger address speaker volume control, and alternate system switching are initiated from the CCTM. The CCTM is located at the door 2R attendant station. January 15, 2004 747-400 Flight Attendant Manual Cabin Management - Cabin Configuration/Test Module Copyright © The Boeing Company. See title page for details. 2A.15.2 D6-30151-TBC (pax) Cabin Configuration Module (CCTM) 1 CABIN CONFIGURATION Display Displays: • up to four lines of text: • top line identifies menu mode • bottom three lines display the configuration of the mode selected. • a caret (>) symbol indicates programmable parameters • an up arrow indicates that the up arrow switch is functional • an down arrow indicates that the down arrow switch is functional. 1 4 5 2 3 6 January 15, 2004 747-400 Flight Attendant Manual Cabin Management - Cabin Configuration/Test Module Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 2A.15.3 2 Down Arrow Switch Touch sensitive. Push - • scrolls the lines of the display up one line each time the arrow switch is pushed • decreases the programmable values when a function select switch is active. 3 Up Arrow Switch Touch sensitive. Push - • scrolls the lines of the display down one line each time the arrow switch is pushed • increases the programmable values when a function select switch is active. 4 ENTER Switch Touch sensitive. Push - • when a “>” is displayed to the left of an area description, changes the display to an expanded description of the area Note: After selecting ENTER, a“>” displayed to the left of a discription indicates that line is changeable. • enters programmable row number or passenger address volume values displayed into system memory • moves the “>” to the next changeable line. 5 CLEAR Switch Touch sensitive. Push - • resets the passenger address volume to “0” in the selected speaker zone when the passenger address function is active • resets the row number to the minimum when the no smoking function is selected. 6 Status Light (typical) Illuminated (white) - touch sensitive switch has been activated. January 15, 2004 747-400 Flight Attendant Manual Cabin Management - Cabin Configuration/Test Module Copyright © The Boeing Company. See title page for details. 2A.15.4 D6-30151-TBC (pax) 1 PROGRAM Switch Maintenance use only. 2 TEST Switch Maintenance use only. 4 5 2 3 1 January 15, 2004 747-400 Flight Attendant Manual Cabin Management - Cabin Configuration/Test Module Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 2A.15.5 3 No Smoking Switch Touch sensitive. Push - displays the seat area description in the display to preview or change the smoking areas. Note: The seat area rows are preset to match the cabin configuration.
作者:
帅哥
时间:
2008-12-28 03:10:38
4 NORMAL Switch Touch sensitive. Push - displays the cabin configuration in the display. 5 Passenger Address Volume Switch Touch sensitive. Push - displays the speaker zone description for passenger address volume preview or volume change. Note: The maximum value is 15. The minimum value is 0. Area Description: January 15, 2004 747-400 Flight Attendant Manual Cabin Management - Cabin Configuration/Test Module Copyright © The Boeing Company. See title page for details. 2A.15.6 D6-30151-TBC (pax) 1 TEST MODE Switch Maintenance use only. 5 4 3 1 2 January 15, 2004 747-400 Flight Attendant Manual Cabin Management - Cabin Configuration/Test Module Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 2A.15.7 2 PASSENGER ADDRESS Switch Illuminated - confirms switch selection. Push - shifts control of the passenger address system to the alternate controller if a failure occurs with the primary controller. 3 CABIN INTERPHONE Switch Illuminated - confirms switch selection. Push - shifts control of the cabin interphone system to the alternate controller if a failure occurs with the primary controller. 4 PASSENGER SERVICES Switch Illuminated - confirms switch selection. Push - shifts control of the passenger services entertainment system to the alternate controller if a failure occurs with the primary controller. 5 CABIN SERVICES Switch Illuminated - confirms switch selection. Push - • all Cabin Services Modules are re-configured to control all areas of the cabin • a malfunctioning Cabin Services Module is not removed from the system. January 15, 2004 747-400 Flight Attendant Manual Cabin Management - Cabin Configuration/Test Module Copyright © The Boeing Company. See title page for details. 2A.15.8 D6-30151-TBC (pax) Cabin Configuration/Test Module Operations Set the CCTM for Flight During preflight: • set the PA volume levels as desired • set the no smoking areas as desired • verify the NORMAL switch status light is illuminated • check all (5) ALTERNATE SYSTEMS switches extinguished. Note: The TEST MODE switch status light must be extinguished for normal systems operation. If illuminated, push the switch to extinguish the status light. Set Passenger Address Volume To change the PA volume: • push the PA volume switch • observe PA VOLUME CONTROL displays in the cabin configuration display. • push the up or down arrow switch (as required) to scroll through the passenger address speaker zone menu • to select the displayed speaker zone, push the ENTER switch • observe SPKR ZONE DESC appears in the display • observe “>” displayed next to CURRENT VALUE • push the up or down arrow switch as required • PA speaker volume can be increased by pushing the up arrow to have a higher number in the display • PA speaker volume can be decreased by pushing the down arrow to have a lower number in the display • push the ENTER switch when the desired PA volume is next to the arrow pointer in the display • observe SPKR ZONE DESC re-appears in the display • repeat the steps, as required, to set the PA. speaker volume in the areas desired • push the NORMAL Switch • system returns to the NORMAL mode • NORMAL mode status light illuminates • ACESS CONFIGURATION INFORMATION is displayed Note: Remain in the NORMAL mode to prevent inadvertent inputs into the PA volume function. January 15, 2004 747-400 Flight Attendant Manual Cabin Management - Cabin Configuration/Test Module Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 2A.15.9 Change/Set No Smoking Areas To set/change no smoking areas: • push the no smoking function switch • observe SET SMOKING AREAS displays in the cabin configuration display. • push the up or down arrow switch (as required) to scroll through the passenger seating menu • push the ENTER switch when the desired seating area is next to the arrow pointer in the display • observe “>” to the left of SEAT AREA DESCRIPTION appears in the display • observe current smoking row definition • push the up or down arrow switch as required, to set the START SMOKING row number • push the ENTER switch • observe “>” to the left of STOP SMOKING appears in the display • push the up or down arrow switch as required, to set the STOP SMOKING row number • push the ENTER switch • observe SET SMOKING AREAS re-appears in the display • repeat the steps, as required, to set all no smoking areas • push the NORMAL Switch • system returns to the NORMAL mode • NORMAL mode status light illuminates • ACESS CONFIGURATION INFORMATION is displayed Note: Remain in the NORMAL mode to prevent inadvertent inputs into the no smoking function. January 15, 2004 747-400 Flight Attendant Manual Cabin Management - Cabin Configuration/Test Module Copyright © The Boeing Company. See title page for details. 2A.15.10 D6-30151-TBC (pax) Intentionally Blank January 15, 2004 747-400 Flight Attendant Manual Cabin Management Chapter 2A Cabin Temperature Section 20 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 2A.20.1 2A.20 Cabin Management-Cabin Temperature [Option: °F or °C; Option: Overhead door 5 crew rest] Temperature Control Overview The cabin temperature control module is located at door 2R. Cabin Temperature Control System Air moves from the passenger cabin to the lower deck, where it is either exhausted overboard or drawn into the recirculation system. Hot trim air from the bleed air system is added to the pack conditioned air to control the temperature in each zone. Each trim air system supplies three zone supply ducts, with the left trim air system also supplying the flight deck. The cabin temperature controllers regulate the temperature by controlling the addition of hot trim air to the cabin temperature zones. The flight crew sets the master passenger cabin target temperature reference to between 65 and 85 degrees F (18 and 29 degrees C) on the flight deck. The cabin attendants can use the cabin temperature control module to adjust the zone target temperature in any passenger zone (+/-10 degrees F, within the limits of 65 to 85 degrees F (+/- 6 degrees C, within the limits of 18 to 29 degrees C)). With the loss of inputs from the flight deck or cabin temperature controllers, the packs maintain a cabin target temperature of 75 degrees F (24 degrees C). The cabin temperature controllers automatically compensate for temperature changes as cabin air humidity and passenger activity change during cruise and descent. The zone target temperature is automatically increased (approximately 1 degree per hour to a maximum of 4 degrees F (approximately 1 degree per hour to a maximum of 4 degrees C)) during cruise so the flight attendants do not have to manually increase the target temperature. The zone target temperature is automatically decreased (approximately 4 degrees F (approximately 2 degrees C) slowly during descent until all automatic system corrections are removed. Note: Cabin temperature control is enabled at the beginning of cruise and disabled at the beginning of descent. January 15, 2004 747-400 Flight Attendant Manual Cabin Management - Cabin Temperature Copyright © The Boeing Company. See title page for details. 2A.20.2 D6-30151-TBC (pax) Cabin Temperature Control Module [Option – °F] [Option – °C] ZONE A 1 2 3 4 7 6 5 ZONE A 1 2 3 4 7 6 5 January 15, 2004 747-400 Flight Attendant Manual Cabin Management - Cabin Temperature Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 2A.20.3 1 ACTUAL Temperature Display Displays the actual temperature of the selected zone. 2 ZONE Display Displays the selected main deck or upper deck zone. 3 TARGET Temperature Display Displays the target temperature of the selected zone. Note: Passenger comfort temperature corrections are automatically made to the target temperature at the beginning of cruise. 4 WARMER Switch Push - increases the target temperature one degree C each time the switch is pushed. Note: Maximum target temperature selectable is 85 degrees F (29 degrees C). 5 COOLER Switch Push - increases the target temperature one degree C each time the switch is pushed. Note: Minimum target temperature selectable is 65 degrees F (18 degrees C). 6 ZONE SELECT Switch Push - displays the selected zone in the ZONE display. Note: Selectable cabin zones are: A, B, C, D, E, and U (upper deck). 7 RESET Switch Push and hold - resets the target temperature in all zones to the temperature selected by the flight deck temperature control selector. January 15, 2004 747-400 Flight Attendant Manual Cabin Management - Cabin Temperature Copyright © The Boeing Company. See title page for details. 2A.20.4 D6-30151-TBC (pax)
作者:
帅哥
时间:
2008-12-28 03:10:48
System Operation Increase Target Temperature To increase the temperature: • push the ZONE SELECT switch to select the desired area/zone • observe the actual temperature • use the WARMER switch to increase the target temperature. Each push of the WARMER switch increases the target temperature by 1 degree F or C. Note: Do not expect an immediate change in the temperature. Note: Maximum selectable target temperature is 85 degrees F (29 degrees C). Decrease Target Temperature To decrease the temperature: • push the ZONE SELECT switch to select the desired area/zone • observe the actual temperature • push the COOLER switch to decrease the target temperature. Each push of the COOLER switch decreases the target temperature by 1 degree F or C. Note: Do not expect an immediate change in the temperature. Note: Minimum selectable target temperature is 65 degrees F (18 degrees C). Reset Target Temperature To reset all passenger zone temperatures to the default (flight crew set) level, push and momentarily hold the RESET switch. Door 5 Overhead Crew Rest Area Temperature Control [Option: Overhead door 5 crew rest] The door 5 overhead crew rest area temperature is controlled manually by the heater controls in the compartment. See Chapter 11, Crew Rest, for detailed information. January 15, 2004 747-400 Flight Attendant Manual Cabin Management Chapter 2A Lavatory Operation/Waste Tank Section 25 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 2A.25.1 2A.25 Cabin Management-Lavatory Operation/Waste Tank Lavatory Operation/Waste Quantity Overview [Typical] The Lavatory Operation/Waste Quantity module is located at Door 2R. At the top of the module are four placards which list all lavatories and their respective waste tank. The placard includes all lavatories in all zones. The placards list the lavatories connected to each waste tank. The identifiers listed on the placards correspond to the lavatory locations shown in this section. January 15, 2004 747-400 Flight Attendant Manual Cabin Management - Lavatory Operation/Waste Tank Copyright © The Boeing Company. See title page for details. 2A.25.2 D6-30151-TBC (pax)
作者:
帅哥
时间:
2008-12-28 03:10:57
Lavatory Operation/Waste Tank Module [Typical] 1 LAVATORY OPERATION Placard Display Lists the lavatories and its respective waste tank. 2 Lavatory Inoperative (LAVS INOP) Switches Maintenance use only. Illuminated (white) - waste tank is full. The flush system for that system is automatically inhibited for the associated lavatories. 5 3 2 1 4 January 15, 2004 747-400 Flight Attendant Manual Cabin Management - Lavatory Operation/Waste Tank Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 2A.25.3 3 Waste TANK SELECT Selector OFF - waste tank display is off. FWD L (forward left) / AFT L (aft left) / FWD R (forward right) / AFT R (aft right) - selects the respect waste tank for display. 4 Waste Tank Quantity Guide Bar Provides guide for tank quantity and fill indication. 5 Waste Tank Quantity Indicator Displays the current waste tank quantity: • green - tank is up to 1/4 full • yellow - tank is between 1/4 and almost full • red - tank is full.
作者:
帅哥
时间:
2008-12-28 03:11:06
Lavatory Operation/Waste Tank Operation Each waste tank may be checked for its current fill status by selecting the appropriate tank with the TANK SELECT selector. A waste tank with little or no pre-charge will indicate in the first quarter of the green band (“E” to halfway). An indication within the yellow or red band indicates that the waste tank requires servicing. When a waste tank becomes full during flight, the corresponding LAVS INOP light illuminates and the flush system for that tank and the associated lavatories is shutdown. Lavatory Operation/Waste Tank Preflight During preflight, the normal indication for an unused tank is the indicator illuminated in the first half (from “E” to halfway) of the green band. This indicates the selected waste tank has the appropriate pre-charge of disinfectant/deodizer solution. January 15, 2004 747-400 Flight Attendant Manual Cabin Management - Lavatory Operation/Waste Tank Copyright © The Boeing Company. See title page for details. 2A.25.4 D6-30151-TBC (pax) Intentionally Blank January 15, 2004 747-400 Flight Attendant Manual Cabin Management Chapter 2A Potable Water Section 26 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 2A.26.1 2A.26 Cabin Management-Potable Water Potable Water Module Overview The potable water quantity indicator is located at Door 2R. It is used to monitor the quantity of potable water remaining. A full potable water tank contains approximately 420 gallons (1600 liters) of water. Potable Water Module 1 WATER QUANTITY Indicator Indicates quantity of water remaining. Segments extinguish from right to left as water quantity decreases. 1 January 15, 2004 747-400 Flight Attendant Manual Cabin Management - Potable Water Copyright © The Boeing Company. See title page for details. 2A.26.2 D6-30151-TBC (pax) Intentionally Blank January 15, 2004 747-400 Flight Attendant Manual Cabin Management Chapter 2A Pre-recorded Announcement / Boarding Music Section 30 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 2A.30.1 2A.30 Cabin Management-Pre-recorded Announcement / Boarding Music [Option shown: Pre-recorded announcement system and boarding music system installed]
作者:
帅哥
时间:
2008-12-28 03:11:15
Pre-recorded Announcement and Boarding Music System Overview The pre-recorded announcement system can select up to 126 different pre-recorded announcements for broadcast over the passenger address system. Up to three announcements can be pre-programmed for automatic playback. An emergency announcement is automatically actuated if the airplane is depressurized above 10,000 feet. The emergency announcement is not selectable at the panel. There are four channels of boarding music. The playback functions are in the following priority: automatic emergency message playback tape message playback, music playback. A lower priority playback cannot override a higher priority playback function. A higher playback function will, when activated, override a lower priority function in progress by interrupting the message. The interrupted function will not be restored when the higher priority function is complete, except when the boarding music is interrupted by the tape message playback function. January 15, 2004 747-400 Flight Attendant Manual Cabin Management - Pre-recorded Announcement / Boarding Music Copyright © The Boeing Company. See title page for details. 2A.30.2 D6-30151-TBC (pax) Pre-recorded Announcement System 1 Numeric Display Displays the selected tape segment numbers next to the ON ANNCMT line, the NEXT line, the RSV1, and the RSV2 lines. 2 NEXT Switch Light illuminates prior to selecting a tape segment and extinguishes after tape segment is programmed and displayed in the numeric display. For an incorrect entry, push the NEXT switch to delete the number shown in the numeric display. The correct number can be reselected. 3 Numeric Keys Push - selects the pre-recorded tape segment. 1 4 3 2 1 CH VOL OFF 2 RSV NEXT CONT CANCL START PWR READY RSV ON ANNCMT ANNOUNCEMENT BGM 2 3 4 5 6 7 8 9 0 1 1 3 4 6 5 7 2 8 9 10 January 15, 2004 747-400 Flight Attendant Manual Cabin Management - Pre-recorded Announcement / Boarding Music Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 2A.30.3 4 Continue (CONT) Switch Push - plays all selected tape segments displayed in the numeric display. Light is illuminated while tape segments are playing.
作者:
帅哥
时间:
2008-12-28 03:11:26
5 Cancel (CANCL) Switch Push - stops the tape. 6 START Switch Push - plays the tape segment number displayed in the NEXT line. The address number displayed in the NEXT line is moved to the ON ANNCMT display line. Address numbers in the RSV2 and RSV2 displays are moved up to the next higher status line. 7 Power (PWR) Switch Push - turns system power on or off. 8 RSV2 Switch Light illuminates prior to selecting a tape segment and extinguishes after tape segment is programmed and displayed in the numeric display. Push - to remove the tape segment shown on numeric display. The correct segment number can then be entered. 9 RSV1 Switch Light illuminates prior to selecting a tape segment and extinguishes after tape segment is programmed and displayed in the numeric display. Push - to remove the tape segment shown on numeric display. The correct segment number can then be entered. 10 READY Light Illuminates when a tape segment is ready to be played. January 15, 2004 747-400 Flight Attendant Manual Cabin Management - Pre-recorded Announcement / Boarding Music Copyright © The Boeing Company. See title page for details. 2A.30.4 D6-30151-TBC (pax) Pre-recorded Announcement System Operation To Play A Tape Segment To program the pre-recorded announcement system: • push the NEXT switch (light illuminates in the switch) • enter the selected number code • number code appears to the left of the NEXT switch (light in NEXT switch extinguishes) Note: The RSV1 and RSV2 lines are programmed in the same manner providing a maximum of three consecutive announcements. • the READY light illuminates when the tape segment is ready to be played To play programmed tape segments: • push the CONT switch to play all programmed tape segments • the tape segment number being played will move up to the ON ANNCMT line • the continue switch light illuminates while the tape segments are playing. To play only the tape segment displayed in the NEXT line: • push START • the segment displayed in the NEXT line will move up to ON ANNCMT line • all other tape segments will move up one line • the start switch light will illuminate while the segment is being played. Stop Or Cancel A Tape Segment To stop or cancel a tape segment, push the CANC switch. January 15, 2004 747-400 Flight Attendant Manual Cabin Management - Pre-recorded Announcement / Boarding Music Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 2A.30.5
作者:
帅哥
时间:
2008-12-28 03:11:38
Boarding Music System 1 Volume (VOL) Selector Rotate - sets the volume for the selected boarding music channel. OFF - boarding music is discontinued. 2 Channel (CH) Selector Rotate - selects the boarding music channel. 1 4 3 2 1 CH VOL OFF 2 RSV NEXT CONT CANCL START PWR READY RSV ON ANNCMT ANNOUNCEMENT BGM 2 3 4 5 6 7 8 9 0 1 1 2 January 15, 2004 747-400 Flight Attendant Manual Cabin Management - Pre-recorded Announcement / Boarding Music Copyright © The Boeing Company. See title page for details. 2A.30.6 D6-30151-TBC (pax) Boarding Music System Operation To turn on the boarding music system: • rotate the CH selector to the desired channel • rotate the VOL selector to the desired volume. Note: Ensure that the volume selector is placed in the OFF position prior to takeoff. If the volume selector is not in the OFF position, the inflight entertainment system audio and passenger address announcements will be inhibited during flight. January 15, 2004 747-400 Flight Attendant Manual Cabin Management Chapter 2A Non-Normal Operations Section 40 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 2A.40.1 2A.40 Cabin Management-Non-Normal Operations Cabin Management Non-normal Operations Cabin Configuration/Test Module Cabin Interphone System If the cabin interphone system malfunctions, push the Cabin Configuration Test Module (CCTM) CABIN INTERPHONE switch to select the alternate cabin interphone system. The switch illuminates to indicate the alternate cabin interphone system is selected. Cabin Services System The Cabin Services Modules (CSMs) are configured to control specific seating areas for lighting, passenger reading lights, and attendant call reset. Pushing the CCTM CABIN SERVICES switch (switch light illuminates when pushed) will cause all operational CSMs to have control of all seating areas (main and upper deck). To return the CSMs to their predefined areas of control, push the illuminated CABIN SERVICES switch on the CCTM (light extinguishes in switch when pushed). Cabin Configuration/Test Module (CCTM) Cabin Interphone Switch Cabin Services Switch Passenger Address Switch Passenger Services Switch January 15, 2004 747-400 Flight Attendant Manual Cabin Management - Non-Normal Operations Copyright © The Boeing Company. See title page for details.
作者:
帅哥
时间:
2008-12-28 03:11:50
2A.40.2 D6-30151-TBC (pax) Passenger Services System If passenger services (entertainment or call), cabin lighting, and passenger information signs malfunction, push the CCTM PASSENGER SERVICES switch to select the alternate passenger service system. The switch illuminates to indicate the alternate passenger services system is selected. Passenger Address System If the passenger services (entertainment or call), cabin lighting, and passenger information signs systems malfunctions, push the PASSENGER SERVICES switch on the CCTM to select the alternate passenger service system. The switch illuminates to indicate the alternate passenger services system has been selected. Note: Ensure the boarding music selector is placed in the OFF position prior to takeoff. Leaving the boarding music selector in an ON position will prevent the passengers from receiving the entertainment audio during flight. January 15, 2004 747-400 Flight Attendant Manual Lighting Chapter 3 Table of Contents Section 0 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 3.TOC.0.1 3.0 Lighting-Table of Contents Lighting Overview . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.10.1 Cabin Lighting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.10.1 Closet Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.10.1 Galley Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.10.1 Lavatory Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.10.1 Reading Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.10.2 Work Lights And Threshold Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.10.2 Miscellaneous Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.10.2 Light Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.10.3 Emergency Lighting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.10.8 Emergency Lights - Interior . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.10.8 Flashlights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.10.11 Emergency Lights - Exterior . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.10.12 Passenger Configuration . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.10.12 January 15, 2004 747-400 Flight Attendant Manual Copyright © The Boeing Company. See title page for details. 3.TOC.0.2 D6-30151-TBC (pax) Lighting - Table of Contents Intentionally Blank January 15, 2004 747-400 Flight Attendant Manual Lighting Chapter 3 Introduction Section 10 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 3.10.1 3.10 Lighting-Introduction Lighting Overview This chapter provides a description of the passenger cabin lighting, and interior and exterior emergency lighting. Cabin Lighting Cabin lighting is provided by white incandescent and fluorescent lights. General cabin illumination includes ceiling, side wall wash, and night lights. These are supplemented by reading, lavatory, work, threshold, and closet lights. If a cabin decompression occurs, all fluorescent lights illuminate and the normal lighting controls at the flight attendant stations are overridden. Cabin lighting is controlled by the Cabin Services Module (CSM) located at designated attendant stations at door 2L and the upper deck galley. See Chapter 2A, Cabin Management, for detailed information on CSM lighting operations. If all main electrical power is lost, the night and supplementary night lights are automatically turned on. Closet Lights A light is provided in each coat closet when normal cabin lighting provides insufficient illumination. Galley Lights The lighting in each galley is controlled by a dimmer switch which provides for high intensity work lighting and low intensity night lighting. Lavatory Lights Lavatories are illuminated by fluorescent lighting. With the airplane on the ground and the ground service bus powered, the lights illuminate bright regardless of the door position. In flight, the lights illuminate dim when the door is unlocked and bright when the door is locked. June 1, 2001 747-400 Flight Attendant Manual Lighting - Introduction Copyright © The Boeing Company. See title page for details. 3.10.2 D6-30151-TBC (pax) Reading Lights The reading lights are located in the passenger service unit (PSU) and provide light from above the passenger seats. They can be operated from the individual passenger control unit (PCU) or the CSM. The reading lights are controlled by the Cabin Services Module (CSM) located at designated attendant stations at door 2L and the upper deck galley. See Chapter 2A, Cabin Management, for detailed information on CSM lighting operations. Work Lights And Threshold Lights Each flight attendant station on the main deck is provided with a work light. Two threshold lights are located at each main deck door. These lights are controlled by switches on the flight attendant panels at each door. Miscellaneous Lights Controls for the overstair light to the upper deck and lights for flight deck access are located at door 2L while the control for the bar light is located at door 1L. January 15, 2004 747-400 Flight Attendant Manual Lighting - Introduction Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 3.10.3 Light Controls OFF BRIGHT INTENSITY BAR LIGHT LIGHTS/CHIME WORK LIGHT 1 2 5 Door 1L CHIME OFF LIGHTS/CHIME THRESHOLD LIGHT WORK LIGHT 1 2 Door 1R January 15, 2004 747-400 Flight Attendant Manual Lighting - Introduction Copyright © The Boeing Company. See title page for details. 3.10.4 D6-30151-TBC (pax) GROUND SERVICE OVER STAIR LIGHT FLIGHT DECK ACCESS CHIME OFF AFT CHIME OFF FORWARD LIGHTS/CHIME WORK LIGHT THRESHOLD LIGHT 1 2 4 3 Door 2L CHIME OFF AFT CHIME OFF FORWARD LIGHTS/CHIME WORK LIGHT THRESHOLD LIGHT 1 2 Door 2R January 15, 2004 747-400 Flight Attendant Manual Lighting - Introduction Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 3.10.5 Door 3L LIGHTS WORK LIGHT THRESHOLD LIGHT 1 2 LIGHTS THRESHOLD LIGHT WORK LIGHTS 1 2 Door 3R January 15, 2004 747-400 Flight Attendant Manual Lighting - Introduction Copyright © The Boeing Company. See title page for details. 3.10.6 D6-30151-TBC (pax) CHIME OFF AFT CHIME OFF FORWARD LIGHTS/CHIME WORK LIGHT THRESHOLD LIGHT 1 2 Door 4L CHIME OFF AFT CHIME OFF FORWARD LIGHTS/CHIME WORK LIGHT THRESHOLD LIGHT 1 2 Door 4R CHIME OFF AFT CHIME OFF FORWARD LIGHTS/CHIME WORK LIGHT THRESHOLD LIGHT 1 2 Door 5L/R January 15, 2004 747-400 Flight Attendant Manual Lighting - Introduction Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 3.10.7 1 WORK LIGHT Switch Illuminated - confirms switch selection. Push - turns associated area work light on or off. 2 THRESHOLD Switch Illuminated - confirms light switch selection. Push - turns associated door threshold light on or off. 3 FLIGHT DECK ACCESS Light Switch Illuminated - confirms light switch selection. Push - • turns the following lights on or off: • ceiling light above door 2L • door 1L work light • two lights in main equipment center • two upper deck ceiling lights, one at the top of the stairway, one at the forward lavatory (inhibited in flight). 4 OVER STAIR LIGHT Switch Illuminated - confirms switch selection. Push - illuminates the overstair side lights for stairway from the main deck to the upper deck. 5 BAR LIGHT Switch Rotate - controls the intensity of the bar unit lighting. Note: There are no light control switches on the upper deck. Upper deck lighting is controlled through the cabin services module (CSM). See Chapter 2A, Cabin Services Module. January 15, 2004 747-400 Flight Attendant Manual Lighting - Introduction Copyright © The Boeing Company. See title page for details. 3.10.8 D6-30151-TBC (pax) Emergency Lighting The emergency lighting system is powered by remote batteries. It provides power for direction to exit locations and illuminates the egress paths inside and outside the airplane. Emergency Lights - Interior 1 Emergency Lights (EMER LIGHTS) Switch Guarded. Illuminated - confirms switch selection. Push -illuminates all emergency lights regardless of the position of the flight deck emergency lights switch. Note: EMER LIGHTS switch is located at door 2L handset cradle only. Door 2L Handset Cradle EMER ACCESS DIRECT ON LIGHTS ___________________ ___________________ ___________________ ___________________ ___________________ ___________________ ___________________ ___________________ ___________________ 24 23 22 21 15 14 13 12 11 DOOR 4 RIGHT DOOR 3 RIGHT DOOR 2 RIGHT DOOR 1 RIGHT DOOR 5 LEFT DOOR 4 LEFT DOOR 3 LEFT DOOR 2 LEFT DOOR 1 LEFT 1 June 1, 2001 747-400 Flight Attendant Manual Lighting - Introduction Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 3.10.9 Emergency Lighting Interior emergency lighting consists of door, aisle, cross-aisle, escape path, and exit lights, and luminescent exit signs. The emergency lighting system is controlled by the emergency lights switch on the flight deck. The switch can be used to manually activate the system or arm the system for automatic operation. Automatic operation occurs if DC power fails or is turned off when the system is armed. In this position, all interior and exterior emergency lights illuminate automatically if there is a total loss of electrical power. The emergency lighting system can also be controlled by the EMER LIGHTS switch on the door 2L handset cradle. When the emergency lights switch on the flight deck is armed, and the door mode select lever is in the armed position, moving the door handle to the open position causes the exterior fuselage light and the interior emergency lights at that door to illuminate. June 1, 2001 747-400 Flight Attendant Manual Lighting - Introduction Copyright © The Boeing Company. See title page for details. 3.10.10 D6-30151-TBC (pax) Emergency Exit Signs Exit signs and emergency area lights indicate all passenger cabin routes. All emergency lights and EXIT signs are powered by remote batteries and are controlled by the emergency lights switches. 1 Emergency Door Light 2 EXIT Signs 3 Emergency Cross Aisle Light 4 Emergency Aisle Lights 5 Emergency Escape Path Lights 3 5 1 2 4 June 1, 2001 747-400 Flight Attendant Manual Lighting - Introduction Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 3.10.11 Escape Path Lighting Escape path lighting consists of floor mounted locator lights located in the aisles, cross-aisles, and on the stairway. Aft pointing arrows are located in both the upper deck track and the main deck Zone A track to assist in emergency evacuation. A lighted exit indicator is located near the floor by each door and emergency exit. When illuminated, escape path lighting provides visual guidance for emergency evacuation if all sources of lighting more than four feet (1.2 meters) above the aisle floor are obscured by smoke. Battery powered exit lights are located at each cabin exit. Flashlights Flashlights are stowed throughout the airplane. These high intensity flashlights illuminate automatically when they are removed from the stowage brackets. A battery indicator light flashes every three to four seconds to indicate adequate power. The light can be extinguished only by replacing the flashlight back into the stowage bracket. The batteries cannot be recharged. See Chapter 8, Emergency Equipment, for specific locations. EMERGENCY USE ONLY Seal Condition Light Viewport January 15, 2004 747-400 Flight Attendant Manual Lighting - Introduction Copyright © The Boeing Company. See title page for details. 3.10.12 D6-30151-TBC (pax) Emergency Lights - Exterior Exterior emergency lighting consists lights that are provided at all main deck, overwing emergency exit, and upper deck doors. The exterior emergency lights illuminate the areas at the base of the escape slides. The overwing exit also illuminates the exit ramp. Passenger Configuration January 15, 2004 747-400 Flight Attendant Manual Communications Chapter 4 Table of Contents Section 0 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 4.TOC.0.1 4.0 Communications-Table of Contents Communications Overview . . . . . . . . . . . . . . . . . . . . . . . . . . 4.10.1 Cabin Interphone System Overview . . . . . . . . . . . . . . . . . . . . 4.20.1 Call Light Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.20.1 Cabin Interphone Directory And Handset . . . . . . . . . . . . . . . 4.20.2 Cabin Interphone Calls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.20.4 Call Types . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.20.4 Cabin Interphone Calls . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.20.6 Passenger Address System . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.21.1 Passenger Address Priorities . . . . . . . . . . . . . . . . . . . . . . . 4.21.1 Handset . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.21.2 Passenger Address Announcements . . . . . . . . . . . . . . . . . 4.21.5 Passenger Call System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.22.1 Area Chime Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.22.3 Attendant Switch Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.22.3 Area Chime Control Operations . . . . . . . . . . . . . . . . . . . . 4.22.5 Lavatory Call System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.23.1 Passenger Signs System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.24.1 Passenger Signs Overview . . . . . . . . . . . . . . . . . . . . . . . . 4.24.1 Automatic Passenger Sign Operation . . . . . . . . . . . . . . . . 4.24.2 Inflight Entertainment System Overview . . . . . . . . . . . . . . . . 4.30.1 Passenger Control Unit (PCU) . . . . . . . . . . . . . . . . . . . . . 4.30.2 Communications Non-Normal Operations . . . . . . . . . . . . . . . 4.40.1 Cabin Interphone System . . . . . . . . . . . . . . . . . . . . . . . . . 4.40.1 Cabin Services System . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.40.1 Passenger Services System . . . . . . . . . . . . . . . . . . . . . . . . 4.40.2 Passenger Address System . . . . . . . . . . . . . . . . . . . . . . . . 4.40.2 In-flight Entertainment (IFE) System Smoke or Fire . . . . 4.40.2
作者:
帅哥
时间:
2008-12-28 03:12:05
January 15, 2004 747-400 Flight Attendant Manual Copyright © The Boeing Company. See title page for details. 4.TOC.0.2 D6-30151-TBC (pax) Communications - Table of Contents Intentionally Blank January 15, 2004 747-400 Flight Attendant Manual Communications Chapter 4 Introduction Section 10 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 4.10.1 4.10 Communications-Introduction Communications Overview This chapter provides a description of the airplane communications systems used by the flight attendants. These systems include: • cabin interphone system • passenger address system • passenger call system • lavatory call system • passenger signs. Also, included in this chapter is information on the passenger entertainment system. June 1, 2001 747-400 Flight Attendant Manual Communications - Introduction Copyright © The Boeing Company. See title page for details. 4.10.2 D6-30151-TBC (pax) Intentionally Blank June 1, 2001 747-400 Flight Attendant Manual Communications Chapter 4 Cabin Interphone Section 20 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 4.20.1 4.20 Communications-Cabin Interphone Cabin Interphone System Overview The cabin interphone system is a phone network with stations on the flight deck and at the attendant stations. [Typical] There are 11 handsets on the main deck: • 1 at each attendant station at doors 1, 2, 3, 4, and 5 • 1 in the door 2 galley at the cart lift. [Typical] There are 2 handsets on the upper deck: • 1 at the upper deck right door flight attendant station • 1 at the aft galley cart lift. [Option: Overhead door 5 crew rest installed] There is also one handset installed in the door 5 overhead attendant rest area. The cabin interphone system can be used to make: • flight deck-to-attendant calls • attendant-to-flight deck calls • attendant-to-attendant calls • passenger address announcements. The cabin interphone handset is used to initiate and receive calls. Call Light Panel The pink cabin interphone crew call lights and attendant station chime annunciations are used as call indicators at the receiving location. The cabin interphone crew call light extinguishes when the receiving station handset is removed from the cradle. Attendant Station Call Light Panel (typical) Crew Call Light (pink) January 15, 2004 747-400 Flight Attendant Manual Communications - Cabin Interphone Copyright © The Boeing Company. See title page for details. 4.20.2 D6-30151-TBC (pax) Cabin Interphone Directory And Handset [Typical] R T 3 T P T T P P 6 5 4 2 1 ___________________ 26 UD DOOR ___________________ 21 DOOR 1 RIGHT 6P CABIN READY PP ___________________ ___________________ PILOT ALERT 33 ___________________ PRIORITY PILOT ___________________ 55 54 56 ___________________ ___________________ 42 41 4P 46 43 52 ___________________ ___________________ ___________________ ___________________ ___________________ ___________________ PA FIRST CL ATT ALL CALL UPPER DECK GAL ALL CALL MAIN DECK GAL PA PRIORITY ALL PA ALL AREAS PA UPPER DECK PA ECONOMY CL 32 31 ___________________ ___________________ PRIORITY CABIN PILOT DOOR 5 RIGHT ___________________ ___________________ ___________________ ___________________ ___________________ ___________________ ___________________ ___________________ ___________________ 25 24 23 22 15 14 13 12 11 DOOR 4 RIGHT DOOR 3 RIGHT DOOR 2 RIGHT DOOR 5 LEFT DOOR 4 LEFT DOOR 3 LEFT DOOR 2 LEFT DOOR 1 LEFT 2 3 1 January 15, 2004 747-400 Flight Attendant Manual Communications - Cabin Interphone Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 4.20.3 1 Reset (R) Switch Momentary switch. Push - • cancels incorrectly selected dial code • ends the call. 2 Dial Buttons Push - enter the two digit dial code for the desired station or PA area. 3 Push-To-Talk (PTT) Switch Push - connects handset to dialed interphone area. January 15, 2004 747-400 Flight Attendant Manual Communications - Cabin Interphone Copyright © The Boeing Company. See title page for details. 4.20.4 D6-30151-TBC (pax) Cabin Interphone Calls Cabin interphone calls are initiated by removing the handset from the handset cradle (dial tone is heard) and dialing the two-digit code for the desired location or type of call. The calling station hears a ring signal until the handset is picked up. If the called station is already in use, the caller receives a normal busy signal. If the caller has dialed a non-existent two-digit code, or is dropped from a call already in progress, the caller receives a rapid busy signal. When an attendant station receives a call, the passenger address system (PAS) sounds a chime, and the pink station cabin interphone crew call light illuminates. Interphone calls are prioritized in the following order: Pilot Alert, Priority Pilot and Priority Cabin, All Call, Attendant All Call, and Station-to-Station calls. Call Types Pilot Alert Pilot Alert is used to notify the flight crew about an emergency. The Pilot Alert call is not inhibited at any time. The dial code for PILOT ALERT, PP, on the handset: • annunciates the call on the flight deck by sounding a single HI/LO chime. Note: Pilot alert calls take priority over all other calls to the flight deck. A lower priority call in progress is automatically disconnected. If more than one pilot alert call is initiated, all applicable callers are connected via a party line. Priority Pilot Priority Pilot is a private line between one designated cabin station (primary) and the flight deck. This is accomplished by either station dialing the PRIORITY PILOT code 33. The primary cabin station is normally at Door 1L. Any other station trying to dial code 33 will receive a rapid busy signal (connection not available). Priority Cabin Call Priority Cabin is a private line between two designated cabin stations (primary and secondary). This is accomplished by either station dialing the PRIORITY CABIN dial code 32. The secondary cabin station is normally at Door 4L. The primary station, normally at Door 1L, can call the flight deck or secondary station. The flight deck and secondary station cannot call each other. All three stations can be on the priority line at the same time, when the calls are initiated from the primary station. Any other station trying to dial either code 32 will receive a rapid busy signal (connection not available). January 15, 2004 747-400 Flight Attendant Manual Communications - Cabin Interphone Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 4.20.5 Pilot A normal two way call to the flight deck may be made by any station. Dialing the PILOT two digit code, 31: • annunciates the call on the flight deck by sounding 2 HI/LO chimes. All Call The All Call selection includes the flight deck and all designated flight attendant stations. Dialing 55, the two digit code for ALL CALL: • annunciates the call by three HI/LO chimes and a flashing cabin crew call light • connects each handset to the call as the handset is removed from the cradle. Attendant All Call Dialing the two digit code for attendant all call (ATT ALL CALL), 54, functions the same as an ALL CALL but does not include the flight deck. ATT ALL CALL calls: • are annunciated by a single HI/LO chime and a flashing cabin crew call light • connects each handset to the call as it is removed from the handset cradle. Cabin Ready Cabin Ready is used to notify the flight crew that the cabin is secured and ready for taxi. Dialing CABIN READY, 6P, on the handset: • sounds a single HI/LO chime on the flight deck • caller hears a rapid beep, beep and then a dial tone. Station-to-Station Calls Station-to-station calls are normal, non-priority/routing, two way calls between stations; for example, attendant-to-pilot, pilot-to-attendant, or attendant to attendant. Any station can make a call to any other station using the two digit dial code. Station-to-station calls: • are annunciated by a single HI/LO chime and a steady master call light. Once a station-to-station call is made, one or two more stations may be added to the connection. Party Line Calls The cabin interphone system has four party lines. Four stations can participate in a party line call. January 15, 2004 747-400 Flight Attendant Manual Communications - Cabin Interphone Copyright © The Boeing Company. See title page for details. 4.20.6 D6-30151-TBC (pax) Cabin Interphone Calls Normal Interphone Calls To place a cabin interphone call: • remove handset from the cradle (listen for dial tone) • enter the two digit code for the desired station. When the call is completed: • return the handset to cradle. Party Line Calls To place a party line interphone call: • remove handset from the cradle (listen for dial tone) • enter the two digit code for the first desired station • when the other station has answered, the caller then dials the two-digit code for the next (third) station to be added • ring will sound five times. If the called station has not answered by the fifth ring, the cabin interphone system will automatically cancel the call to the third station (stations one and two will still be on the line). • if a fourth station is desired, follow the same procedure as calling the third station. When the call is completed: • return the handset to cradle. Call Transfer When on a station-to-station call, to transfer the call to another station, dial the two-digit code for the desired station. When that station answers, replace the handset in the handset cradle or press the “R” (reset) key on the handset. Remote Answer Calls made to one station may be answered at a different station. To accomplish this, dial the two-digit code for the called station. This resets the other handset location to receive new calls. January 15, 2004 747-400 Flight Attendant Manual Communications Chapter 4 Passenger Address System Section 21 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 4.21.1 4.21 Communications-Passenger Address System [Option shown: Direct access switch door 2L installed] Passenger Address System The passenger address (PA) system is used for making flight deck, attendant, and prerecorded announcements to the passenger cabin. Entertainment audio and boarding music can also be sent through the PA system. Flight attendants can make PA announcements using the cabin interphone handsets. Those announcements can be sent through the cabin interphone system or directly to all cabin areas using the Direct Access switch located on the interphone handset cradle. The handset cradles located at doors 1L, 2L, and 4L have Direct Access switches. Passenger address announcements are made by selecting the desired area on the handset and pushing the Push-to-Talk (PTT) switch on the handset. Direct access announcements are initiated by pushing the PA direct access switch on the handset cradle. Passenger Address Priorities Passenger address announcements are prioritized in the following order: • flight deck • direct access • priority announcements • normal announcements • pre-recorded announcements • video system audio • boarding music A higher priority announcement overrides a lower priority announcement. When the cabin interphone system is used to make PA announcements and a higher priority announcement is initiated, the cabin interphone system resets and a dial tone is heard in the handset. There is a flight deck indication when the PA system is in use in the passenger cabin. January 15, 2004 747-400 Flight Attendant Manual Communications - Passenger Address System Copyright © The Boeing Company. See title page for details. 4.21.2 D6-30151-TBC (pax) Handset Door 1L, Door 4L [Typical] R T 3 T P T T P P 6 5 4 2 1 ACCESS DIRECT ON ___________________ ___________________ T S E R W E R C 5 R D 61 6P CABIN READY PP ___________________ ___________________ PILOT ALERT 33 ___________________ PRIORITY PILOT ___________________ 55 54 56 ___________________ ___________________ 42 41 4P 46 44 43 52 ___________________ ___________ CL________ ___________________ ___________________ ___________________ ___________________ ___________________ PA FIRST CL ATT ALL CALL UPPER DECK GAL ALL CALL MAIN DECK GALLEY PA PRIORITY PA ALL PA UPPER DECK PA ECONOMY CL PA BUSINESS 32 31 ___________________ ___________________ PRIORITY CABIN PILOT DOOR U/D RIGHT DOOR 5 RIGHT ___________________ ___________________ ___________________ ___________________ ___________________ ___________________ ___________________ ___________________ ___________________ ___________________ 26 25 24 23 22 21 15 14 13 12 11 DOOR 4 RIGHT DOOR 3 RIGHT DOOR 2 RIGHT DOOR 1 RIGHT DOOR 5 LEFT DOOR 4 LEFT DOOR 3 LEFT DOOR 2 LEFT DOOR 1 LEFT 1 2 3 1 Handset Handset Cradle January 15, 2004 747-400 Flight Attendant Manual Communications - Passenger Address System Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 4.21.3 Door 2L [Option: Direct access switch door 2L installed] 1 Direct Access Switch Push - • makes a PA to passenger cabin announcement sent to all areas of cabin • overrides all PA announcements except for flight deck announcements. R T 3 T P T T P P 6 5 4 2 1 EMER ACCESS DIRECT ON LIGHTS ___________________ ___________________ T S E R W E R C 5 R D 61 6P CABIN READY PP ___________________ ___________________ PILOT ALERT 33 ___________________ PRIORITY PILOT ___________________ 55 54 56 ___________________ ___________________ 42 4P 46 44 43 52 _________________34 ___________________ ___________________ ___________________ ___________________ ___________________ ___________________ BUSINESS CTR ATT ALL CALL UPPER DECK GAL ALL CALL MID GALLEY PA PRIORITY PA ALL AREAS PA UPPER DECK PA ECONOMY PA BUSINESS 32 31 ___________________ ___________________ PRIORITY CABIN FLIGHT DECK DOOR U/D RIGHT DOOR 5 RIGHT ___________________ ___________________ ___________________ ___________________ ___________________ ___________________ ___________________ ___________________ ___________________ ___________________ 26 25 24 23 22 21 15 14 13 12 11 DOOR 4 RIGHT DOOR 3 RIGHT DOOR 2 RIGHT DOOR 1 RIGHT DOOR 5 LEFT DOOR 4 LEFT DOOR 3 LEFT DOOR 2 LEFT DOOR 1 LEFT 41 ___________________ PA FIRST CLASS ___________________ P3 PILOT CRW RST 4 3 1 Handset Handset Cradle January 15, 2004 747-400 Flight Attendant Manual Communications - Passenger Address System Copyright © The Boeing Company. See title page for details. 4.21.4 D6-30151-TBC (pax) 2 Reset (R) Switch Momentary switch. Push - • cancels incorrectly selected dial code • ends the PA call. 3 Dial Buttons Push - enter the two digit dial code for the desired station or PA area. 4 Reset (R) Switch Momentary switch. Push - • cancels incorrectly selected dial code • ends the PA call. January 15, 2004 747-400 Flight Attendant Manual Communications - Passenger Address System Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 4.21.5 Passenger Address Announcements Direct Access Announcements [Option: Direct access switch door 2L installed] Direct access announcements can be initiated only at interphone handsets with a direct access switch, located at doors 1L, 2L, and 4L. Direct access announcements are sent to all areas of the passenger cabin and override all PA announcements except an announcement from the flight deck. To initiate a direct access announcement: • remove handset from the cradle • push the Direct Access switch located on the cradle • observe white light illuminates in switch indicating selection • push and hold the handset Push-to-Talk (PTT) switch • make the announcement • hang up phone to reset the system • observe white light in switch extinguishes. Note: If a flight deck announcement is in progress, the caller receives a busy signal. Note: Direct Access switch located at door 1L, 2L, and door 4L only. January 15, 2004 747-400 Flight Attendant Manual Communications - Passenger Address System Copyright © The Boeing Company. See title page for details. 4.21.6 D6-30151-TBC (pax) Priority Announcements A priority announcement overrides all other PA announcements being made through the cabin interphone system, except for the flight deck and direct access announcements. To make a priority announcement: • remove handset from the cradle (listen for dial tone) • enter the two digit code, 4P, for PA PRIORITY • push the handset PTT switch • make the announcement • replace the handset. Note: If a flight deck, direct access or another PA priority announcement is in progress, the caller receives a busy signal. Normal Announcements To make an announcement: • remove handset from the cradle (listen for dial tone) • enter the two digit code for the desired PA area • 41, PA FIRST CL, for first class • 42, PA BUSINESS CL, for business class • 43, PA ECONOMY CL, for economy class • 44, PA UPPER DECK, for the upper deck • 46, PA ALL, for all areas. Note: If making an announcement in multiple areas, select the two digit codes for the desired additional PA areas. • push and hold the handset Push-to-Talk switch • make the announcement • push the Reset switch. Note: If a flight deck, direct access, or a priority announcement is in progress, the caller receives a busy signal. January 15, 2004 747-400 Flight Attendant Manual Communications Chapter 4 Passenger Call System Section 22 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 4.22.1 4.22 Communications-Passenger Call System Passenger Call System A call from the passenger seating area is made by activating the Attendant Call switch located in each passenger seat arm rest. Pushing the Attendant Call switch: • illuminates the passenger service unit (PSU) white Row Call Light in the PSU above the seat row VOLUME Attendant Call Switch Attendant Call Reset Switch PSU Row Call Light (white) January 15, 2004 747-400 Flight Attendant Manual Communications - Passenger Call System Copyright © The Boeing Company. See title page for details. 4.22.2 D6-30151-TBC (pax) • illuminates the blue passenger call light at the attendant station being called • illuminates the attendant call light on the Cabin Services Module (CSM) for the appropriate displayed area, and • sounds a single HI chime at the attendant station being called. The PSU row call light is extinguished when any attendant call reset switch in that PSU row is pushed. The blue attendant station Attendant Call light extinguishes when all activated attendant call reset switches for that area have been reset. Pushing the Attendant Call RESET switch on the Cabin Services Module, (CSM) extinguishes all call lights in the displayed area; this includes all Passenger Call Lights and all Lavatory Call Lights. See Chapter 2A, Cabin Management. Passenger Call Light (blue) Light Panel (typical) RESET ATTENDANT CALL Cabin Services Module (typical) Passenger Call Light (white) January 15, 2004 747-400 Flight Attendant Manual Communications - Passenger Call System Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 4.22.3 Area Chime Control Passenger seat area passenger-to-attendant call chimes are controlled by the respective flight attendant panel. Attendant Switch Panel WORK LIGHT THRESHOLD LIGHT CHIME OFF LIGHTS/CHIME 1 Door 1L/1R LIGHTS/CHIME WORK LIGHT THRESHOLD LIGHT CHIME OFF AFT CHIME OFF FORWARD 2 3 Door 2R January 15, 2004 747-400 Flight Attendant Manual Communications - Passenger Call System Copyright © The Boeing Company. See title page for details. 4.22.4 D6-30151-TBC (pax) 1 CHIME OFF Switch Illuminated - confirms switch selection. Push - inhibits the passenger-to-attendant call chime on the upper deck.. 2 CHIME OFF AFT Switch Illuminated - confirms switch selection. Push - • inhibits the passenger-to-attendant call chime in the aft portion of the area controlled by the panel • controls the chime on the side of the cabin where the panel is located. 3 CHIME OFF FORWARD Switch Illuminated - confirms light switch selection. Push - • inhibits the passenger-to-attendant call chime in the forward portion of the area controlled by the panel • controls the chime on the side of the cabin where the panel is located. LIGHTS/CHIME WORK LIGHT THRESHOLD LIGHT CHIME OFF AFT CHIME OFF FORWARD 2 3 Door 4L/4R January 15, 2004 747-400 Flight Attendant Manual Communications - Passenger Call System Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 4.22.5 Area Chime Control Operations Disable/Enable Chimes To disable the passenger-to-attendant chimes for the area controlled by the respective attendant switch panel: • push the appropriate CHIME OFF switch • verify that the white light illuminates in the switch. To enable the passenger-to-attendant chimes for the area controlled by the respective attendant switch panel: • push the appropriate CHIME OFF switch • verify that the white light extinguishes in the switch Note: The CHIME OFF AFT and the CHIME OFF FORWARD switches control the associated aft/forward chimes on the side of the cabin where the panel is located. January 15, 2004 747-400 Flight Attendant Manual Communications - Passenger Call System Copyright © The Boeing Company. See title page for details.
作者:
帅哥
时间:
2008-12-28 03:12:20
4.22.6 D6-30151-TBC (pax) Intentionally Blank January 15, 2004 747-400 Flight Attendant Manual Communications Chapter 4 Lavatory Call Section 23 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 4.23.1 4.23 Communications-Lavatory Call Lavatory Call System A call from the lavatory is made by pushing the Attendant Call switch located on the front side of the lavatory sink cabinet. Pushing the Attendant Call switch: • illuminates the switch to confirm selection • illuminates the lavatory call light/reset switch located on the outside wall over the door of the calling lavatory • illuminates the amber lavatory call light at the attendant station being called • sounds a single HI chime at the attendant station being called • illuminates the attendant call light at the Cabin Services Module (CSM) for the appropriate area displayed In lavatory Attendant Call Switch Lavatory Call Light (amber) Attendant Station Call Light Panel (typical) January 15, 2004 747-400 Flight Attendant Manual Communications - Lavatory Call Copyright © The Boeing Company. See title page for details. 4.23.2 D6-30151-TBC (pax) The lavatory call light is extinguished by pushing the lavatory call light/reset switch over the lavatory door. The amber lavatory call light extinguishes when all lavatory call light/reset switches for that area are reset. Lavatory calls can also be reset from the CSM attendant call RESET switch for that area. January 15, 2004 747-400 Flight Attendant Manual Communications Chapter 4 Passenger Signs Section 24 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 4.24.1 4.24 Communications-Passenger Signs [Option shown: No smoking signs normal operation; Option: No smoking signs always on] Passenger Signs System Passenger Signs Overview NO SMOKING and FASTEN SEAT BELT signs are located on the cabin overhead and in the passenger service unit (PSU). The signs are visible to all passengers. The signs are controlled from the flight deck either manually or automatically. On the ground, all signs are illuminated. A single LO chime sounds over the passenger address system each time any of the passenger signs illuminate or extinguish. Lavatory Fwd Occupied Lavatory Aft Occupied Lavatory Fwd Occupied Cabin Overhead (typical) January 15, 2004 747-400 Flight Attendant Manual Communications - Passenger Signs Copyright © The Boeing Company. See title page for details. 4.24.2 D6-30151-TBC (pax) A RETURN TO SEAT sign is located in each lavatory and visible only when illuminated. The RETURN TO SEAT signs illuminate when the FASTEN SEAT BELT signs are illuminated. Note: All signs, except the Return to Seat signs in the lavatories, illuminate automatically if the cabin altitude is greater than 10,000 feet or if the passenger cabin oxygen system is deployed. Automatic Passenger Sign Operation Takeoff And Landing After takeoff with the passenger signs in the automatic mode, the FASTEN SEAT BELT and RETURN TO SEAT signs extinguish when the landing gear and flaps are up. The NO SMOKING signs extinguish when the landing gear are up. After takeoff with the passenger signs in the automatic mode, the FASTEN SEAT BELT and RETURN TO SEAT signs extinguish when the landing gear and flaps are up. The NO SMOKING signs extinguish when the landing gear are up.. During descent for landing, the FASTEN SEAT BELT and RETURN TO SEAT signs illuminate when the airplane gear and flaps are lowered or below 10,300 feet. The NO SMOKING signs illuminate when the landing gear are lowered. When the cabin signs illuminate or extinguish, a LO chime sounds over the PA system. Loss of Cabin Pressure And Oxygen Deployment The NO SMOKING and FASTEN SEAT BELT signs illuminate automatically if the cabin altitude exceeds 10,000 feet or if the passenger cabin oxygen system is manually or automatically deployed. The RETURN TO SEAT signs illuminate with the FASTEN SEAT BELT signs. In Lavatory January 15, 2004 747-400 Flight Attendant Manual Communications - Passenger Signs Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 4.24.3 The NO SMOKING and FASTEN SEAT BELT signs illuminate automatically if the cabin altitude exceeds 10,000 feet or if the passenger cabin oxygen system is manually or automatically deployed. The RETURN TO SEAT signs illuminate with the FASTEN SEAT BELT signs. Note: The RETURN TO SEAT sign in the lavatories will not illuminate if passenger cabin oxygen has been deployed. January 15, 2004 747-400 Flight Attendant Manual Communications - Passenger Signs Copyright © The Boeing Company. See title page for details. 4.24.4 D6-30151-TBC (pax) Intentionally Blank January 15, 2004 747-400 Flight Attendant Manual Communications Chapter 4 Inflight Entertainment System Section 30 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 4.30.1 4.30 Communications-Inflight Entertainment System Inflight Entertainment System Overview The passenger entertainment system includes a multi-channel selection of music and video system audio. The audio entertainment switches on the Cabin Services Modules (CSMs) control the playing of the audio system. See Chapter 2A, Cabin Management, Section 10 Cabin Services Module. The passenger service system switches provide electrical power for operation of the overhead electrical units which contain the PA speakers, passenger reading lights, and the passenger service unit (PSU) Row Call Light. The passenger service system switches are located on the CSM. The video entertainment system includes video monitors, video projectors, and screens. An individual video system (IVS) is installed in the airplane which is capable of providing audio and video from the tape cassettes. The audio can be distributed through individual passenger headsets or through the passenger address system overhead speakers. Passenger address announcements from the flight deck or a flight attendant handset automatically override the audio entertainment program. When the announcement is complete, the program resumes. Each passenger seat contains a passenger control unit (PCU). Passengers use the PCU to select various in-flight entertainment system functions, turn the reading lights on or off, or call for passenger service. A headset may be plugged in to listen to the audio on the selected channel. The PCU includes switches for channel selection and audio volume. See the inflight entertainment vendor’s operating manuals for detailed information. January 15, 2004 747-400 Flight Attendant Manual Communications - Inflight Entertainment System Copyright © The Boeing Company. See title page for details. 4.30.2 D6-30151-TBC (pax) Passenger Control Unit (PCU) [Typical] 1 Headphone Jack Headset plug-in. 2 Reading Light Switch Push - turns on or off the reading light for that seat. 3 Channel Up/Down Arrow Switch Push - channel displayed changed sequentially up/down each time switch is pushed. VOLUME 3 4 2 5 1 7 6 January 15, 2004 747-400 Flight Attendant Manual Communications - Inflight Entertainment System Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 4.30.3 4 Attendant Call Reset Switch Push - • extinguishes the PSU Row Call light • resets the attendant call function for that seat row. 5 Attendant Call Switch Push - • illuminates the white PSU Row Call light • illuminates the blue passenger call light at the flight attendant station being called (unless already illuminated by another call from that area) • sounds a chime at the flight attendant station being called (unless inhibited) • illuminates the Attendant Call Light at the Cabin Services Module for the respective seat area (unless illuminated by another call in that area). 6 Volume Up/Down Arrow Switch Push - incrementally increase/decreases volume each time switch is pushed. 7 Channel Select Display Displays the audio program channel selected. January 15, 2004 747-400 Flight Attendant Manual Communications - Inflight Entertainment System Copyright © The Boeing Company. See title page for details. 4.30.4 D6-30151-TBC (pax) Intentionally Blank January 15, 2004 747-400 Flight Attendant Manual Communications Chapter 4 Non-Normal Operations Section 40 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 4.40.1 4.40 Communications-Non-Normal Operations Communications Non-Normal Operations Cabin Interphone System If the cabin interphone system malfunctions, push the CABIN INTERPHONE switch on the Cabin Configuration Test Module (CCTM) to select the alternate cabin interphone system. The switch illuminates to indicate the alternate cabin interphone system is selected. Cabin Services System The Cabin Services Modules (CSMs) are configured to control specific seating areas for lighting, passenger reading lights, and attendant call reset. Pushing the CCTM CABIN SERVICES switch (switch light illuminates when pushed) will cause all operational CSMs to have control of all seating areas (main and upper deck). To return the CSMs to their predefined areas of control, push the illuminated CABIN SERVICES switch on the CCTM (light extinguishes in switch when pushed). Cabin Interphone Switch Passenger Address Switch Passenger Services Switch Cabin Services Switch Cabin Configuration/Test Module (CCTM) January 15, 2004 747-400 Flight Attendant Manual Communications - Non-Normal Operations Copyright © The Boeing Company. See title page for details. 4.40.2 D6-30151-TBC (pax) Passenger Services System If passenger services (entertainment or call), cabin lighting, and passenger information signs malfunction, push the PASSENGER SERVICES switch on the CCTM to select the alternate passenger service system. The switch illuminates to indicate the alternate passenger services system is selected. Passenger Address System If the passenger services (entertainment or call), cabin lighting, and passenger information signs systems malfunctions, push the CCTM PASSENGER SERVICES switch to select the alternate passenger service system. The switch illuminates to indicate the alternate passenger services system has been selected. Note: Ensure the boarding music selector is placed in the OFF position prior to takeoff. Leaving the boarding music selector in an ON position will prevent the passengers from receiving the entertainment audio during flight. In-flight Entertainment (IFE) System Smoke or Fire [Option shown: Video Control Center (VCC); Option: Purser Work Station] In the event of smoke or fire caused by any of the in-flight entertainment system (IFE) components, all electrical power should be removed from the IFE system. In the event of smoke or fire caused by any of the in-flight entertainment system (IFE) components, all electrical power should be removed from the IFE system and passenger seats. There is one master IFE power switch and eight individual passenger zone switches. Passenger zone switches are: • IFE Zone A • IFE Zone B • IFE Zone U/D • IFE Zone C • IFE Zone D (LHS) • IFE Zone D (RHS) • IFE Zone E (LHS) • IFE Zone E (RHS) Note: The IFE Master power switch will remove IFE, Airshow, and PC power from all passenger cabin zones while the individual power switches remove IFE, Airshow, and PC power to the respective zone only. January 15, 2004 747-400 Flight Attendant Manual Communications - Non-Normal Operations Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 4.40.3 Power is removed by moving the IFE ZONE Power switch, located in the Video Control Center (VCC), for the respective passenger zone to the OFF position. This removes all electrical power to that zone: • the in-seat audio/video system equipment • audio entertainment players • video entertainment players • overhead video system and displays/projectors • in-seat video displays/audio in the crew rest areas • integrated telephones • the passenger control units (PCUs) • the passenger seat • seat motor power (as applicable) • personal computer power outlet (as applicable) • in-flight passenger cabin telephones Note: If any IFE Master Power switch is placed in the OFF position, no passenger service functions (reading lights or attendant call) are available. Note: Moving the IFE Master power switch to the OFF position does not cause an EICAS message to be displayed on the flight deck. WARNING: Once power is removed from the IFE system or passenger IFE zone, do not turn the IFE power switch back on for the remainder of the flight. January 15, 2004 747-400 Flight Attendant Manual Communications - Non-Normal Operations Copyright © The Boeing Company. See title page for details. 4.40.4 D6-30151-TBC (pax) Intentionally Blank January 15, 2004 747-400 Flight Attendant Manual Lavatories Chapter 5 Table of Contents Section 0 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 5.TOC.0.1 5.0 Lavatories-Table of Contents Lavatories Overview . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.10.1 Lavatory Locations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.10.2 Upper Deck . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.10.2 Main Deck . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.10.3 Lavatory Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.10.4 Lavatory Layout . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.10.4 Lavatory Water System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.10.6 Water Supply Shutoff Valve Handle . . . . . . . . . . . . . . . . . 5.10.8 Lavatory Waste System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.10.9 Lavatory Fire Protection Systems . . . . . . . . . . . . . . . . . . . . . 5.10.10
作者:
帅哥
时间:
2008-12-28 03:12:34
Lavatory Smoke Detector . . . . . . . . . . . . . . . . . . . . . . . . 5.10.10 Lavatory Fire Extinguishing System . . . . . . . . . . . . . . . . 5.10.12 Lavatory Temperature Indicator . . . . . . . . . . . . . . . . . . . 5.10.12 Lavatory Non-Normals . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.20.1 Inoperative Toilet(s) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.20.1 Lavatory Sink Water Faucet Fails to Shut Off . . . . . . . . . 5.20.2 Toilet Flush Valve Fails to Reset . . . . . . . . . . . . . . . . . . . . 5.20.3 Toilet Flooding . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.20.4 Waste Tanks Improperly Serviced . . . . . . . . . . . . . . . . . . . 5.20.5 Lavatory Doors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.20.6 Bifold Door Unlocking/Locking . . . . . . . . . . . . . . . . . . . . 5.20.6 Bifold Door Removal . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.20.7 Panel Door Unlocking . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.20.9 January 15, 2004 747-400 Flight Attendant Manual Copyright © The Boeing Company. See title page for details. 5.TOC.0.2 D6-30151-TBC (pax) Lavatories - Table of Contents Intentionally Blank January 15, 2004 747-400 Flight Attendant Manual Lavatories Chapter 5 System Description Section 10 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 5.10.1 5.10 Lavatories-System Description [Options not shown: Bidet, upper deck lavatory door hooks] Lavatories Overview This chapter provides a description of the lavatories and their locations, water and waste systems, and lavatory smoke detection and fire protection systems. Lavatory controls and displays are located throughout the airplane. See Chapter 2A, Cabin Management, Lavatory Operation/Waste Tank. for information on the lavatory operation/waste quantity module displays. June 1, 2001 747-400 Flight Attendant Manual Lavatories - System Description Copyright © The Boeing Company. See title page for details. 5.10.2 D6-30151-TBC (pax) Lavatory Locations Upper Deck [Typical] On the upper deck, there are 2 lavatory compartments. The aft lavatory, 8U, contains a baby care station. D Baby Care Station Disabled Passenger H D Access 4U 8U January 15, 2004 747-400 Flight Attendant Manual Lavatories - System Description Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 5.10.3
作者:
帅哥
时间:
2008-12-28 03:12:47
Main Deck [Typical] On the main deck, there are 14 lavatories. Lavatory, BS6, located at door 2R, is equipped for handicapped passengers. All main deck lavatories contain baby care stations. H D D D D D D D D D D D D D D BS1A BS3 CC18 DC19 FC5 FC3 FC1 BS2A BS6 CC19 DC20 FC6 FC4 FC2 Baby Care Station Disabled Passenger H D Access January 15, 2004 747-400 Flight Attendant Manual Lavatories - System Description Copyright © The Boeing Company. See title page for details. 5.10.4 D6-30151-TBC (pax) Lavatory Description Lavatory Layout Each lavatory contains a toilet, wash basin, mirror, necessary vanity items, and disposal units. In addition, there is an attendant call switch, a loudspeaker for passenger address, a RETURN TO SEAT sign, a no smoking/fasten seat belts sign, a smoke detector/alarm, a waste compartment fire extinguishing system, a lockable door, and an overhead compartment containing two oxygen masks. Closing and latching the lavatory door causes the mirror light and a LAVATORY OCCUPIED sign to illuminate. Each toilet has a manual shutoff handle, located at the base of the toilet. If the flush valve fails in the open position, pulling the handle shuts off the toilet vacuum flush system. Passenger Service Unit (speaker & oxygen) Smoke Detector Flush Handle Water Heater (behind removeable panel) Manual Shutoff Handle Waste Compartment Fire Extinguisher (behind door) January 15, 2004 747-400 Flight Attendant Manual Lavatories - System Description Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 5.10.5 The lavatory door can be locked or unlocked from the outside by lifting the “LAVATORY” sign on the door and inserting a flat object into the VACANT/OCCUPIED indicator and sliding the lock left or right. Lock Slide Cover Plate January 15, 2004 747-400 Flight Attendant Manual Lavatories - System Description Copyright © The Boeing Company. See title page for details. 5.10.6 D6-30151-TBC (pax) Lavatory Water System The potable water system is supplied from four tanks located beneath the cabin floor. Water is supplied to the lavatory sinks and the toilet flush system. The tanks have a combined usable capacity of approximately 420 gallons (1600 liters). The tanks are normally pressurized with air from the airplane pneumatic system. When pneumatic pressure is not available, alternate pressurization is automatically provided by an electrically driven air compressor. Water is not available while the tanks are being serviced. Hot and cold water is available in the lavatories. The water heater is located below the lavatory sink. An ON-OFF Switch is located on the side near the top of the water heater. An amber light near the top of the heater is illuminated when the heater is operating. • low (approximately 105 degrees F / 41 degrees C) • medium (approximately 115 degrees F / approximately 46 degrees C) • high (approximately 125 degrees F / 52 degrees C). All lavatories have push button, time delay faucets. January 15, 2004 747-400 Flight Attendant Manual Lavatories - System Description Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 5.10.7 An amber indicator light located near the top of the heater is illuminated when the power switch is on and the heater is operating normally. An ON/OFF switch is located next to the amber light. Water is not available while the tanks are being serviced. Heater Switch Indicating Light Water Heater January 15, 2004 747-400 Flight Attendant Manual Lavatories - System Description Copyright © The Boeing Company. See title page for details. 5.10.8 D6-30151-TBC (pax) Water Supply Shutoff Valve Handle Each lavatory has a water shutoff valve handle which turns off water supplied to the water heater, lavatory sink, and toilet. The Water Supply Shutoff Valve handle has two positions, OPEN and CLOSE, and is located below the water heater. Access is through a removable panel next to the waste compartment door. OPEN CLOSE Water Supply Shutoff Valve handle Water Supply Shutoff Valve Water Heater January 15, 2004 747-400 Flight Attendant Manual Lavatories - System Description Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 5.10.9
作者:
帅哥
时间:
2008-12-28 03:13:02
Lavatory Waste System Waste water from the lavatory sinks is drained overboard through drain masts on the fuselage. Toilet waste is flushed into four waste holding tanks located in the bulk cargo area. The toilet waste is flushed into four waste holding tanks located below the main deck cabin, in the bulk cargo area. The two forward tanks have a capacity of 85 gallons (320 liters) each, for a total of 170 gallons (640 liters), and the two aft tanks have a capacity of 65 gallons (246 liters) each, for a total of 130 gallons (492 liters). The waste system uses a vacuum to collect the waste material and deposit it in the tanks. At altitudes above approximately 16,000 feet, the pressure difference between the cabin altitude and flight altitude moves the waste from the toilets to the tanks. Below 16,000 feet and on the ground, pushing the flush button on the toilet activates a vacuum system and the flush cycle. The flush cycle uses water from the potable water system, and lasts approximately six seconds. Once the flush handle is pushed, there is an automatic 15-second delay for a system reset before the next flush cycle can be initiated. This delay conserves water by preventing consecutive flushes if the flush handle is repeatedly pushed. Each tank system operates independently. The Waste Quantity Select switch on the Lavatory Operation/Waste Quantity Module, at the Door 2R attendant panel, can be used to check the waste quantity level of each tank. If a tank becomes full, the toilet flush system for that tank shuts down automatically. The flush system also shuts down automatically during ground servicing of the tanks. Lights on the Lavatory Operation/Waste Quantity Module illuminate to indicate flush system shutdown. Note: Toilet blockages can occur if large objects are flushed down the toilet. Items which commonly cause blockages are diapers, hand towels, cups, and large quantities of toilet paper. January 15, 2004 747-400 Flight Attendant Manual Lavatories - System Description Copyright © The Boeing Company. See title page for details. 5.10.10 D6-30151-TBC (pax) Lavatory Fire Protection Systems Lavatory Smoke Detector A smoke detector is mounted in each lavatory. When activated by either detecting smoke or pushing the self test switch, a horn sounds in the smoke detector and the red Alarm Indicator Light illuminates on the smoke detector. 1 Power Indicator Light Illuminated (green) - smoke detector has power and is operating. 2 Interrupt Switch Push - silences the horn and suppresses all alarm indications as long as the switch is pushed. 3 Self Test Switch Push - activates the smoke detector aural and visual alarms. Note: The system automatically resets when the test is concluded. 4 Alarm Indicator Light Illuminated (red) - presence of smoke has been detected 1 2 3 4 Lavatory Smoke Detector (typical) January 15, 2004 747-400 Flight Attendant Manual Lavatories - System Description Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 5.10.11 Lavatory Smoke Detector Operation When smoke is detected in a lavatory, the amber Lavatory Call indicator light/Reset switch, mounted on the exterior wall above the lavatory door, flashes and a chime sounds in the cabin near the associated lavatory. The lavatory call light at the associated lavatory flashes. The system can be reset by pushing the Lavatory Call indicator light/Reset switch. When the Lavatory Call indicator/reset switch is pushed: • the lavatory master call light extinguishes • the continuous chime is turned off • the smoke detector horn silences • the Lavatory Call indicator/reset switch extinguishes • a smoke alarm suppression cycle is initiated in the smoke detector Note: If there is still smoke in the lavatory, the red Alarm Indicator Light on the smoke detector remains illuminated. • a lavatory smoke alert message is displayed on the flight deck When the smoke clears, the red Alarm Indicator Light extinguishes, the suppression cycle ends, and the smoke detector is sensitive to smoke again. Continue to monitor the lavatory until the red Alarm Indicator Light extinguishes. Note: When the smoke detector has been activated by smoke, lingering smoke in the detector sensor may cause reactivation. Blowing air into the detector sensor (the small screen cutout on the side of the cube extending from the unit) may clear lingering smoke. January 15, 2004 747-400 Flight Attendant Manual Lavatories - System Description Copyright © The Boeing Company. See title page for details. 5.10.12 D6-30151-TBC (pax)
作者:
帅哥
时间:
2008-12-28 03:13:11
Lavatory Fire Extinguishing System An automatic fire extinguishing system is located beneath the sink in each lavatory. A fire extinguisher discharges a halon vapor through either one or both of the heat-activated nozzles. Both nozzles discharge toward the waste disposal container. The color of the nozzle tips change to an aluminum color if the extinguisher has discharged. Lavatory Temperature Indicator A temperature indicator is located inside the waste compartment below each sink, behind and above the waste container. Grey dots on the indicator turn black when exposed to high temperatures. If any dot has turned black or a nozzle tip has changed color, the extinguisher has discharged. CHECK THE FOUR GREY DOTS ON TEMPERATURE INDICATOR LOCATED ABOVE WASTE CONTAINER IF ANY GREY DOT HAS TURNED BLACK CHECK FOR FIRE DAMAGE REPLACE FIRE EXTINGUISHER REPLACE TEMPERATURE INDICATOR TEMPERATURE INDICATOR 250 230 200 180 TEMPERATURE INDICATOR January 15, 2004 747-400 Flight Attendant Manual Lavatories Chapter 5 Non-Normal Operations Section 20 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 5.20.1 5.20 Lavatories-Non-Normal Operations Lavatory Non-Normals Inoperative Toilet(s) If one of the toilets does not flush, use the the Lavatory Operation/Waste Quantity Module to check the status of the waste tank for that lavatory. If the waste tank is full, placard all lavatories connected to the full waste tank as inoperative. If the waste tank is not full, the affected lavatory should be placarded inoperative. If one or more of the toilets do not flush, check the placard on the Lavatory Operation/Waste Quantity Module at door 2R. Locate the LAVS INOP switch applicable for the inoperative toilet(s). If the light in the LAVS INOP switch is illuminated, the waste tank is full and the affected lavatories should be placarded as inoperative. If the LAVS INOP switch light is not illuminated, push and hold the LAVS INOP switch (may require holding switch for up to 30 seconds) until the LAVS INOP switch light illuminates. The vacuum flush system is now reset. If the toilet(s) still do not flush, the affected lavatory should be placarded as inoperative. See Chapter 2A, Cabin Management, Lavatory Operation/Waste Tank for further information. June 1, 2001 747-400 Flight Attendant Manual Lavatories - Non-Normal Operations Copyright © The Boeing Company. See title page for details. 5.20.2 D6-30151-TBC (pax) Lavatory Sink Water Faucet Fails to Shut Off If the sink water faucet buttons do not shut off the running water, the water system for that lavatory must be shut off. Remove the access panel on the vanity cabinet next to the waste compartment door by pulling the bottom edge of the panel out. Locate the Water Shutoff Valve Handle which is below the water heater. Turn the handle perpendicular to the water line (water pipe) to close the valve. The water system, which includes the sink and the toilet flush, is turned off for that lavatory. OPEN CLOSE Water Supply Shutoff Valve handle Water Supply Shutoff Valve Water Heater January 15, 2004 747-400 Flight Attendant Manual Lavatories - Non-Normal Operations Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 5.20.3 Placard the lavatory as inoperative. Toilet Flush Valve Fails to Reset A loud continuous air noise or sucking noise coming from the toilet is caused by the flush valve sticking in the open position. Flush the toilet to reset the flush valve. If the noise stops, the flush valve is reset and the toilet is operating normally. If the noise continues, close the toilet lid and pull the manual shutoff handle located at the base of the toilet out. This closes the flush valve and stops the noise. Placard the lavatory as inoperative. Flush Handle Manual Shutoff Handle January 15, 2004 747-400 Flight Attendant Manual Lavatories - Non-Normal Operations Copyright © The Boeing Company. See title page for details. 5.20.4 D6-30151-TBC (pax)
作者:
帅哥
时间:
2008-12-28 03:13:20
Toilet Flooding If a toilet floods due to the water rinse valve sticking open after flushing, immediately flush the toilet to evacuate excess water from the toilet bowl. If the toilet does not flush, refer to Inoperative Toilet(s). If the toilet flushes, but water continues to flow into the toilet bowl, flush the toilet once or twice more. If the water continues flowing, use the water supply shutoff valve to shut off the water for that lavatory. OPEN CLOSE Water Supply Shutoff Valve handle Water Supply Shutoff Valve Water Heater January 15, 2004 747-400 Flight Attendant Manual Lavatories - Non-Normal Operations Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 5.20.5 Remove the access panel on the vanity cabinet next to the waste compartment door by pulling the bottom edge of the panel out. Locate the Water Shutoff Valve Handle which is below the water heater. Turn the handle perpendicular to the water line (water pipe) to close the valve. The water system, which includes the sink and the toilet flush, is turned off for that lavatory. Placard the lavatory as inoperative. Waste Tanks Improperly Serviced Verification of waste tank servicing is accomplished prior to dispatch by viewing the Waste Quantity on Lavatory Operation/Waste Quantity Module. Rotate the Waste Quantity select switch through all four waste tank positions (FWD L, AFT L, FWD R, AFT R). The waste tank quantity level should be in the first half (from "E" to halfway) of the green color bar for an unused waste tank. A waste quantity indication in the yellow or red color band indicates an improperly serviced waste tank. Maintenance should be contacted to service any tanks not showing the proper indication. January 15, 2004 747-400 Flight Attendant Manual Lavatories - Non-Normal Operations Copyright © The Boeing Company. See title page for details. 5.20.6 D6-30151-TBC (pax) Lavatory Doors Bifold Door Unlocking/Locking The lavatory door can be locked or unlocked from the outside by: • lifting the metal flap above the VACANT/OCCUPIED indicator • moving the lock slide to left to lock the door • moving the lock slide to right to unlock the door Lock Slide Cover Plate January 15, 2004 747-400 Flight Attendant Manual Lavatories - Non-Normal Operations Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 5.20.7 Bifold Door Removal Occasionally the lavatory door may become blocked from the inside due to supplies falling out of the storage compartment onto the floor, or an incapacitated passenger lying on the floor. The following procedure allows the removal of the door and access to the lavatory compartment: • unlock the door • release the upper and lower hinge pins on the door • pull the top hinge pin down and over • lift the bottom hinge pin up and over • rotate the door hooks (as installed) up by pushing each button in and turning clockwise Lavatory Door Latch Hinge Pin Door Hook Push Buttons January 15, 2004 747-400 Flight Attendant Manual Lavatories - Non-Normal Operations Copyright © The Boeing Company. See title page for details. 5.20.8 D6-30151-TBC (pax) • pull the door out at the bottom • drop the door down and away from the lavatory January 15, 2004 747-400 Flight Attendant Manual Lavatories - Non-Normal Operations Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 5.20.9 Panel Door Unlocking Panel doors are generally associated with lavatories with handicapped facilities. If the panel door is locked and access must be gained: • slide a flat object (knife, credit card, fingernail) under the door latch receiver flap • pry the door latch receiver flap forward and outward • pull on door handle at same time as lifting on door latch receiver flap Door Latch Receiver Flap January 15, 2004 747-400 Flight Attendant Manual Lavatories - Non-Normal Operations Copyright © The Boeing Company. See title page for details.
作者:
帅哥
时间:
2008-12-28 03:13:29
5.20.10 D6-30151-TBC (pax) Intentionally Blank June 1, 2001 747-400 Flight Attendant Manual Galleys Chapter 6 Table of Contents Section 0 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 6.TOC.0.1 6.0 Galleys-Table of Contents Galley Overview . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.10.1 Galley Locations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.10.2 Upper Deck . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.10.2 Main Deck . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.10.3 Galley Electrical Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.10.4 Galley Water System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.10.4 Water Shutoff Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.10.4 Galley Waste System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.10.5 Food Cart Lift . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.10.6 Cart Lift Control Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.10.6 Galley Non-Normals . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.20.1 Floor Drains Flooding with Fluid Overflow . . . . . . . . . . . 6.20.1 Galley Sink Drain Blockages . . . . . . . . . . . . . . . . . . . . . . 6.20.1 Galley Emergency Power Off Switch . . . . . . . . . . . . . . . . 6.20.1 Galley Water Fails to Shut Off . . . . . . . . . . . . . . . . . . . . . 6.20.2 Cart Lift . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.20.2 January 15, 2004 747-400 Flight Attendant Manual Copyright © The Boeing Company. See title page for details. 6.TOC.0.2 D6-30151-TBC (pax) Galleys - Table of Contents Intentionally Blank January 15, 2004 747-400 Flight Attendant Manual Galleys Chapter 6 System Description Section 10 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 6.10.1 6.10 Galleys-System Description Galley Overview Individual galley modules may contain ovens, waste containers, coffee makers, refrigeration units, storage/servicing carts, sinks and stowage space to aid in food preparation and dispensing. Galleys are equipped with electrical power and water systems. Lighting controls are located on the galley electric panel. A galley vent system keeps the air fresh. Service carts are restrained for takeoff and landing. There are stowage areas for extra carts located at various galleys. The number of food carts shall not exceed the number of inflight cart restraints available. January 15, 2004 747-400 Flight Attendant Manual Galleys - System Description Copyright © The Boeing Company. See title page for details. 6.10.2 D6-30151-TBC (pax) Galley Locations Upper Deck [Typical] Upper Deck Galley Cart Lift June 1, 2001 747-400 Flight Attendant Manual Galleys - System Description Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 6.10.3 Main Deck [Typical] Galley 1 Galley 2 Galley 3 Galley 5 Galley 4B Cart Lift Galley 6 Bar Unit Galley 7 Galley 8 Galley 9 June 1, 2001 747-400 Flight Attendant Manual Galleys - System Description Copyright © The Boeing Company. See title page for details. 6.10.4 D6-30151-TBC (pax) Galley Electrical Power A Galley Emergency Power Off Switch is located in each galley. The switch is covered with a red guard. With the red guard closed, the switch is in the NORMAL (on) position. If there is an emergency, the red guard should be lifted and the toggle switch placed to the OFF position. This removes all electrical power to the galley. The Galley Emergency Power Off Switch should be used only during an emergency situation. Galley Water System Galley water is supplied from four potable water tanks. The tanks have a combined usable capacity of approximately 420 gallons (1600 liters). The tanks are normally pressurized with air from the airplane pneumatic system. When pneumatic pressure is not available, alternate pressurization is automatically provided by an electrically driven air compressor. Water is not available while the tanks are being serviced. Water Shutoff Valve Each galley that has running water is equipped with a water shutoff valve. Positioning the water shutoff valve to OFF turns off water to that galley. OFF ON Water Shutoff V
作者:
帅哥
时间:
2008-12-28 03:13:40
alve June 1, 2001 747-400 Flight Attendant Manual Galleys - System Description Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 6.10.5 Galley Waste System Galley sink waste water is drained overboard through heated drain masts. To prevent sink drain blockages do not put solid waste (coffee grounds, tea bags, fruit pulp, and so on) in the sink drain. Put solid waste in the galley waste bins. Mixtures, which can curdle and create a drain blockage, should be diluted with an equal amount of water. Solid waste is stored in removable waste bins within each galley. Do not remove the sink drain strainer. January 15, 2004 747-400 Flight Attendant Manual Galleys - System Description Copyright © The Boeing Company. See title page for details. 6.10.6 D6-30151-TBC (pax) Food Cart Lift An electrically powered food cart lift is installed for food service between the main and upper decks. Control panels are provided on both the main and upper decks adjacent to the lift. An interphone handset is located near each cart lift. Cart Lift Control Panel [Send only panel] [Call/Send panel] NORMAL OPERATION IN TRANSIT C A R T L I F T UNSAFE/OPEN EMERGENCY STOP POWER OFF RESET M/D DOOR U/D DOOR Upper Deck Only 1 2 3 4 5 6 7 NORMAL OPERATION U/DOOR UNSAFE RESET POWER OFF RESET IN TRANSIT STOP EMERGENCY C A R T L I F T Upper Deck Only 1 2 3 4 5 6 7 January 15, 2004 747-400 Flight Attendant Manual Galleys - System Description Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 6.10.7 [Send only panel] [Call/Send panel] 1 Up Arrow Switch Illuminated - the cart is located at the upper deck. Main deck: • Push - with the cart lift located at the main deck, pushing the up arrow raises the cart lift from the main deck to the upper deck. Note: The upper deck up arrow switch is inoperative. CART LIFT UP OVERRIDE RESET POWER OFF TRANSIT IN M/D DOOR U/D DOOR NORMAL OPERATION UNSAFE/OPEN EMERGENCY STOP Main Deck Only 1 2 3 4 5 6 7 CART LIFT EMERGENCY STOP OVERRIDE RESET POWER OFF TRANSIT IN UNSAFE U/DOOR NORMAL OPERATION Main Deck Only 1 2 3 4 5 6 7 January 15, 2004 747-400 Flight Attendant Manual Galleys - System Description Copyright © The Boeing Company. See title page for details. 6.10.8 D6-30151-TBC (pax) 2 INTRANSIT Light Illuminated - when the cart lift is in transit between the main deck and the upper deck. Note: When the cart lift is in transit, the UP/DOWN arrows will be extinguished. 3 Down Arrow Switch Illuminated - the cart is located at the main deck. Upper deck: • Push - with the cart lift located at the upper deck, pushing the down arrow lowers the cart lift from the upper deck to the main deck. Note: The main deck down arrow switch is inoperative.
作者:
帅哥
时间:
2008-12-28 03:14:12
747-400 Flight Attendant Manual The Boeing Company Copyright © 2001 The Boeing Company All Rights Reserved Document Number D6-30151-TBC (pax) 4 Emergency Stop RESET Light Illuminated (red) - the EMERGENCY STOP switch has been pushed. 5 Emergency Stop POWER OFF Light Illuminated (red) - illuminated on both main deck and upper deck cart lift control panels when power is removed from the cart lift. 6 EMERGENCY STOP Switch Push - • removes electrical power from the cart lift • restores electrical power to the cart lift if the emergency stop RESET light is illuminated. 7 Upper Deck (U/D) DOOR / Main Deck (M/D) DOOR Light Illuminated (amber) - upper deck/main deck cart lift door is not closed and latched. Note: If both the upper deck and main deck cart lift doors are open, U/D DOOR and M/D DOOR will be illuminated. January 15, 2004 747-400 Flight Attendant Manual Galleys - System Description Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 6.10.9 Intentionally Blank January 15, 2004 747-400 Flight Attendant Manual Galleys - System Description Copyright © The Boeing Company. See title page for details. 6.10.10 D6-30151-TBC (pax) [Send only panel] [Call/Send panel] OVERRIDE UP READY DOWN READY C A R T L I F T Upper Deck Only 1 2 3 4 5 6 OVERRIDE UP READY DOWN READY C A R T L I F T Upper Deck Only 1 2 3 4 5 6 January 15, 2004 747-400 Flight Attendant Manual Galleys - System Description Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 6.10.11 [Send only panel] [Call/Send panel] 1 OVERRIDE UP-READY Switch Push and hold - cart lift transits from the main deck to the upper deck when both the main deck and upper deck OVERRIDE UP-READY switches are pushed and held at the same time. The emergency stop switches and the safety interlocks are inhibited. 2 OVERRIDE UP Light Illuminated (white) - • override electrical power is available for cart lift operation • both main and upper deck panels OVERRIDE UP-READY switches are pushed simultaneously. READY DOWN READY UP OVERRIDE RESET Main Deck Only 4 5 6 1 2 3 4 5 6 READY DOWN READY UP OVERRIDE RESET Main Deck Only 1 2 3 4 5 6 January 15, 2004 747-400 Flight Attendant Manual Galleys - System Description Copyright © The Boeing Company. See title page for details. 6.10.12 D6-30151-TBC (pax) 3 OVERRIDE UP READY Light Illuminated (green) - • override electrical power is available for cart lift operation • on both main and upper deck panels when the OVERRIDE UP-READY switch is pushed only on one panel. 4 OVERRIDE DOWN-READY Switch Push and hold - cart lift transits from the upper deck to the main deck when both the main deck and upper deck OVERRIDE DOWN-READY switches are pushed and held at the same time. The emergency stop switches and the safety interlocks are inhibited. 5 OVERRIDE DOWN Light Illuminated (white) - • override electrical power is available for cart lift operation • both main and upper deck panels OVERRIDE DOWN-READY switches are pushed simultaneously. 6 OVERRIDE DOWN READY Light Illuminated (green) - • override electrical power is available for cart lift operation • on both main and upper deck panels when the OVERRIDE DOWN-READY switch is pushed only on one panel. January 15, 2004 747-400 Flight Attendant Manual Galleys Chapter 6 Non-Normal Operations Section 20 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 6.20.1 6.20 Galleys-Non-Normal Operations Galley Non-Normals Floor Drains Flooding with Fluid Overflow Flooding can occur in the floor drains located near the main deck entry doors, on the galley floor, or in the food cart lift well. The flooding at these drains is caused by a blockage in the normal drain system. If a drain is overflowing, do not pour any more fluids into a galley sink adjacent to a flooding floor drain. Fluids should be disposed of in another galley sink. Galley Sink Drain Blockages If a sink drain is blocked, or drainage is slow, no more fluids should be poured into the sink. Dispose of fluids in another galley sink. Galley Emergency Power Off Switch A galley Emergency (EMER) POWER OFF SWITCH is located in each galley. The switch is guarded. With the guard closed, the switch is in the NORM (on) position. If there is a non-normal condition, lift the guard and position the switch to OFF. This removes all electrical power to the galley. Galley electrical power should immediately be shut off for malfunctions such as fire, smoke, electrical arcing, and so on. Note: When placing the galley Emergency Power Off switch to the OFF position, notify the flight deck. OFF NORM EMER POWER OFF SWITCH June 1, 2001 747-400 Flight Attendant Manual Galleys - Non-Normal Operations Copyright © The Boeing Company. See title page for details. 6.20.2 D6-30151-TBC (pax) Galley Water Fails to Shut Off If the water cannot be turned off in any of the galley fixtures, such as the sink water faucet, coffee maker, or water boiler, the water system for that galley must be shut off. Locate the water shutoff valve for that galley and position the galley water shutoff valve to OFF. The water system for that galley is shutoff. See the galley vendor’s drawings for exact location. Cart Lift Lift Fails to Rise/Lower The cart lift override switches are used only when the normal operation of the lift fails and the procedures on the Cart Lift Motor Disconnect Panel have been accomplished. [Send only panel] OFF ON Water Shutoff Valve NORMAL OPERATION U/DOOR UNSAFE RESET STOP EMERGENCY NORMAL OPERATION IN TRANSIT OVERRIDE UP READY DOWN READY C A R T L I F T UNSAFE/OPEN EMERGENCY STOP POWER OFF RESET M/D DOOR U/D DOOR Upper Deck Only January 15, 2004 747-400 Flight Attendant Manual Galleys - Non-Normal Operations Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 6.20.3 [Call/Send panel] [Send only panel] NORMAL OPERATION U/DOOR UNSAFE RESET POWER OFF RESET IN TRANSIT OVERRIDE UP READY DOWN READY STOP EMERGENCY C A R T L I F T Upper Deck Only CART LIFT READY DOWN READY UP OVERRIDE RESET POWER OFF TRANSIT IN M/D DOOR U/D DOOR NORMAL OPERATION UNSAFE/OPEN EMERGENCY STOP Main Deck Only January 15, 2004 747-400 Flight Attendant Manual Galleys - Non-Normal Operations Copyright © The Boeing Company. See title page for details. 6.20.4 D6-30151-TBC (pax) [Call/Send panel] Verify the appropriate override READY light is illuminated. Pressing the respective override switch simultaneously on the main deck and the upper deck will raise or lower the cart lift. Note: The Cart Lift Motor Disconnect Panel must be in OVERRIDE before the cart lift override switches are operative. Note: The emergency stop POWER OFF light will be illuminated when the power is removed from the cart lift by the cart lift disconnect motor procedure. CART LIFT EMERGENCY STOP READY DOWN READY UP OVERRIDE RESET POWER OFF TRANSIT IN UNSAFE U/DOOR NORMAL OPERATION Main Deck Only January 15, 2004 747-400 Flight Attendant Manual Galleys - Non-Normal Operations Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 6.20.5 Cart Lift Motor Fails to Operate If the cart lift motor fails to operate properly, follow the printed instructions shown below the Cart Lift Motor Disconnect Panel. IF LIFT WILL NOT OPERATE CHECK THAT: BOTH LIFT DOORS ARE CLOSED; “UP”, “DOWN”, OR “IN-TRANSIT” LIGHT IS ILLUMINATED; & “STOP” LIGHT IS NOT ILLUMINATED. IF LIFT WILL STILL NOT OPERATE PUSH “STOP” SWITCH TO REMOVE POWER & CHECK FOR JAMMED LIFT CAR. OPEN DISCONNECT DOOR LIFT MOTOR DISCONNECT DOOR CAUTION: DO NOT CONNECT MOTORS WITH LIFT MOVING LATCH CLOSED DURING TAXI, TAKEOFF AND LANDING. Cart Lift Door Latch Lift Motor Disconnect Panel Cart Lift Placard Cart Lift Door Upper Deck Only January 15, 2004 747-400 Flight Attendant Manual Galleys - Non-Normal Operations Copyright © The Boeing Company. See title page for details. 6.20.6 D6-30151-TBC (pax) IF LIFT WILL NOT OPERATE CHECK THAT: BOTH LIFT DOORS ARE CLOSED; “UP”, “DOWN”, OR “IN-TRANSIT” LIGHT IS ILLUMINATED; & “STOP” LIGHT IS NOT ILLUMINATED. IF LIFT WILL STILL NOT OPERATE PUSH “STOP” SWITCH TO REMOVE POWER & CHECK FOR JAMMED LIFT CAR. OPEN DISCONNECT DOOR LIFT MOTOR DISCONNECT DOOR CAUTION: DO NOT CONNECT MOTORS WITH LIFT MOVING IF LIFT WILL NOT OPERATE CHECK THAT: BOTH LIFT DOORS ARE CLOSED; “UP”, “DOWN”, OR “IN-TRANSIT” LIGHT IS ILLUMINATED; & “STOP” LIGHT IS NOT ILLUMINATED. IF LIFT WILL STILL NOT OPERATE PUSH “STOP” SWITCH TO REMOVE POWER & CHECK FOR JAMMED LIFT CAR. OPEN DISCONNECT DOOR DISCONNECT UPPER DECK CART LIFT POWER SWITCH RELEASE CONNECT MOTOR 1 MOTOR 2 HEAT PUSH TO RESET NORMAL OVERRIDE OVER OVER HEAT Note: Cart lift motor disconnect panel shown with door in the open position. January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits Chapter 7 Table of Contents Section 0 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 7.TOC.0.1 7.0 Doors, Slides and Emergency Exits-Table of Contents Doors, Slides, And Emergency Exits Overview . . . . . . . . . . . 7.10.1 Overview . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.20.1 Main Deck Passenger Entry Doors . . . . . . . . . . . . . . . . . . 7.20.1 Passenger Entry Door Controls . . . . . . . . . . . . . . . . . . . . . 7.20.2 Door Mode Select Panel . . . . . . . . . . . . . . . . . . . . . . . . . . 7.20.4 Dedicated Assist Space . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.20.7 Evacuation Slide/Rafts . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.20.8 Slide/Raft Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.20.10 Evacuation Slide/Rafts - Slides . . . . . . . . . . . . . . . . . . . . 7.20.12 Evacuation Slide/Raft - Rafts . . . . . . . . . . . . . . . . . . . . . 7.20.13 Main Deck Entry Doors . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.20.14 Main Deck Passenger Entry Door Preflight . . . . . . . . . . 7.20.14 Main Deck Passenger Entry Door Normal Operation – Interior . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.20.15 Main Deck Passenger Entry Door Normal Operation - Exterior . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.20.16 Overwing Emergency Exit Overview . . . . . . . . . . . . . . . . . . . 7.30.1 Overwing Emergency Exit Controls . . . . . . . . . . . . . . . . . 7.30.2 Door Mode Select Panel . . . . . . . . . . . . . . . . . . . . . . . . . . 7.30.4 Dedicated Assist Space . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.30.7 Overwing Ramp/Slide . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.30.8 Overwing Ramp/Slide Manual Inflation Handle . . . . . . . . 7.30.9 Overwing Door Slide . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.30.10 Escape Strap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.30.11 Overwing Emergency Exit . . . . . . . . . . . . . . . . . . . . . . . . . . 7.30.12 Overwing Exit Preflight . . . . . . . . . . . . . . . . . . . . . . . . . 7.30.12 Overwing Emergency Exit Normal Operation . . . . . . . . 7.30.13 Upper Deck Doors Overview . . . . . . . . . . . . . . . . . . . . . . . . 7.40.1 Upper Deck Door Controls . . . . . . . . . . . . . . . . . . . . . . . . 7.40.2 Door Mode Select Panel . . . . . . . . . . . . . . . . . . . . . . . . . . 7.40.4 Door Ground Mode/Battery OK Panel . . . . . . . . . . . . . . . 7.40.6 Dedicated Assist Space . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.40.7 January 15, 2004 747-400 Flight Attendant Manual Copyright © The Boeing Company. See title page for details. 7.TOC.0.2 D6-30151-TBC (pax) Doors, Slides and Emergency Exits - Table of Contents Upper Deck Door Slide . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.40.8 Upper Deck Door Manual Inflation Handle . . . . . . . . . . . 7.40.9 Upper Deck Door Slides . . . . . . . . . . . . . . . . . . . . . . . . . 7.40.10 Upper Deck Door . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.40.11 Upper Deck Door Preflight . . . . . . . . . . . . . . . . . . . . . . . 7.40.11 Upper Deck Door Normal Operation . . . . . . . . . . . . . . . . 7.40.12 Doors, Slides and Emergency Exits Non-Normal Operations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.50.1 Passenger Entry Door Non-Normal Operation . . . . . . . . . 7.50.1 Overwing Exit Non-Normal Operation . . . . . . . . . . . . . . . 7.50.3 Upper Deck Doors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.50.5 Securing Main Deck Doors 1, 2, 4, or 5 In The Open Position . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.50.6 January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits Chapter 7 Introduction Section 10 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 7.10.1 7.10 Doors, Slides and Emergency Exits-Introduction Doors, Slides, And Emergency Exits Overview This chapter describes the passenger entry doors, overwing exits, upper deck doors, and evacuation slides and slide/rafts. It includes a description of door and emergency exit preflight, and normal and non-normal operation from inside and outside the airplane. There are eight identically operated main deck passenger entry doors, doors 1, 2, 4, and 5, which are paired along the airplane fuselage. They are used to enter and exit the airplane, and also serve as emergency exits. Additionally, there are two overwing emergency exit doors, door 3, and two upper deck doors which function as emergency exits only. The operation of the main deck passenger entry doors is discussed in Section 20, Passenger Entry Doors. The operation of the overwing emergency exits is discussed in Section 30, Overwing Emergency Exits. The operation of the upper deck doors is discussed in Section 40, Upper Deck Doors. Passenger evacuation and ditching guidelines are described in Chapter 9, Non-Normal Situation Guidelines. January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Introduction Copyright © The Boeing Company. See title page for details. 7.10.2 D6-30151-TBC (pax) Intentionally Blank June 1, 2001 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits Chapter 7 Passenger Entry Doors Section 20 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 7.20.1 7.20 Doors, Slides and Emergency Exits-Passenger Entry Doors [Option shown: AUTOMATIC/MANUAL; Option: ARM/DISARM, FLIGHT/PARK] Overview Main Deck Passenger Entry Doors The ten main deck passenger entry doors are used to enter and exit the airplane, and also serve as emergency exits. Doors on the left side of the airplane are identified as 1L, 2L, 4L, and 5L are generally used for passenger entry. Doors on the right side of the airplane are 1R, 2R, 4R, and 5R are generally used for the servicing of the airplane. The main deck passenger doors can be opened or closed manually from inside or outside the airplane. The doors are inward-outward opening, plug-type doors. When opened, the door first moves inward then swings outward and forward. Each door is held in the open position by a gust lock. The gust lock drops into a latch as the door nears its forward limit of travel. A window in each door allows observation outside the airplane. Rotation of the door operating handle forward to the CLOSED position automatically latches the door. A dual lane slide/raft is contained behind the door bustle of each passenger entry door on Doors 1, 2, 4, and 5. The slide/rafts are detachable from the doorsill and may be used as life rafts during ditching. January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Passenger Entry Doors Copyright © The Boeing Company. See title page for details. 7.20.2 D6-30151-TBC (pax) Passenger Entry Door Controls 1 Door Assist Handle Used to apply leverage needed to open and latch door if power assist system fails. 2 Door Mode Select Panel See following graphic. 3 Slide/Raft Gas Bottle Pressure Gage Indicates pressure in bottle used to inflate slide/raft. If the gage needle is outside the green zone, the system is unusable. 1 5 6 7 8 3 2 4 January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Passenger Entry Doors Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 7.20.3 4 Door Power Assist Gas Bottle Pressure Gage Behind access panel. Indicates pressure in bottle used to assist in door opening. If the gage needle is outside the green zone, the system is unusable. 5 Escape Slide Lamp Illuminates entire slide. 6 Viewing Window Allows observation outside the airplane. 7 Door Operating Handle Latches and unlatches the door for opening. To open the door – rotate in the direction of the arrow. To close the door – rotate in the opposite direction of the arrow. 8 Slide/Raft Bustle Bustle contains the slide/raft. Note: A warning strap is installed in the door sill, approximately halfway up on the left side of the door. It should be used when the door is open. To use the warning strap, pull the metal handle and attach it to the loop on the right side of the door sill. January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Passenger Entry Doors Copyright © The Boeing Company. See title page for details. 7.20.4 D6-30151-TBC (pax) Door Mode Select Panel 1 Door Mode Select Lever Used to select the required mode for flight, AUTOMATIC, or arrival, MANUAL. 2 Access Cover Open - allows access to the door mode select lever. Closed - allows verification of the door mode select lever position. AUTOMATIC MANUAL Door 3 2 4 1 5 January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Passenger Entry Doors Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 7.20.5 3 MANUAL Door is disarmed if the mode select lever knob is visible in the viewport. Moving the mode select lever to the MANUAL position disables automatic slide/raft deployment Note: Automatic deployment of the slide/raft is disabled when the exterior door operating handle is moved to the open position. Note: A lockout pin may be installed. The lockout pin prevents the movement of the mode select lever from the MANUAL position 4 Clear Plastic Viewport MANUAL - knob visible in viewport indicates door is in the disarmed mode. AUTOMATIC - knob visible in viewport indicates door is in the armed mode. 5 AUTOMATIC Door is armed if the mode select lever knob is visible in the viewport. When the door operating handle is moved to the OPEN position: • the door is powered open • the slide/raft automatically deploys. Note: If the door is opened from the outside, the mode select lever automatically moves to the MANUAL position. CAUTION: To ensure that the door is properly armed or disarmed, the door mode select lever knob must be visible in the viewport window. January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Passenger Entry Doors Copyright © The Boeing Company. See title page for details. 7.20.6 D6-30151-TBC (pax) Door Mode Select Lever Operation The mode select lever on each door controls the arming and disarming of: • the power assist system • the automatic deployment of the slide/raft Setting the mode select lever to MANUAL disarms the power assist system and the door can be opened normally without power assist and without deploying the slide/raft. Note: A lockout pin may be installed. The lockout pin prevents the movement of the mode select lever from the MANUAL position Setting the mode select lever to AUTOMATIC arms the power assist system and the rotation of the inside door operating handle to OPEN activates the power assist and automatically deploys and inflates the slide/raft. Rotating the door operating handle fully aft (OPEN) with the mode select lever in the AUTOMATIC position activates the power assist system and automatically deploys and inflates the slide/raft. In certain adverse airplane attitudes, an initial outward push on the door operating handle may be required to supplement the power assist system. When the door is closed using the exterior door operating handle, the door mode select lever remains in MANUAL and must be manually positioned to AUTOMATIC to provide normal power assist system operation and automatic slide deployment. When the mode select lever is in AUTOMATIC position and the door is opened using the exterior door handle, the mode select lever mechanically positions to MANUAL and the door may be opened without slide deployment. Note: The mode select lever cannot be moved from MANUAL to AUTOMATIC or AUTOMATIC to MANUAL unless the door is fully closed.
作者:
帅哥
时间:
2008-12-28 03:14:27
January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Passenger Entry Doors Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 7.20.7 Dedicated Assist Space Near each door are dedicated assist spaces. The dedicated assist spaces are located on either side of the door passageway. During an emergency evacuation, it is important that the flight attendants grasp the assist handle and place themselves in the dedicated assist space to ensure that they are not blocking the exit in any way. Blocking the exit prohibits dual lane flow onto the slides. Note: The use of the aft facing dedicated assist space allows continuous monitoring of the slide without interrupting passenger flow. Assist Handle Dedicated Assist Space (typical) January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Passenger Entry Doors Copyright © The Boeing Company. See title page for details. 7.20.8 D6-30151-TBC (pax) Evacuation Slide/Rafts Evacuation slide/raft and door opening systems are contained in each passenger entry door. A door bustle on the lower face of the door covers the slide/raft. When the mode select lever is in AUTOMATIC position and the door operating handle is rotated 180 degrees, the door automatically opens using the power assist system activates. The flight attendant must release the door operating handle and continue to assist the door opening motion by using the assist handles on the door and on the door surround panel until the door is in the full open and latched position. The door-mounted escape slide/raft automatically deploys and inflates. If the slide/raft does not inflate automatically, pulling the manual inflation handle inflates the slide/raft. Note: If an inflated slide/raft becomes deflated after deployment, it may be used as an apron slide. When the door is to be opened from the interior and slide deployment is not desired, the mode select lever must be in MANUAL position. Slide/raft January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Passenger Entry Doors Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 7.20.9 The slide/rafts are dual lane and can be released from the door sill to be used as life rafts after ditching. A knife is provided to cut the mooring line. Each slide/raft may contain: • a canopy • a survival kit • manual inflation provisions (hand pump) The canopy and survival kit are tethered to the slide/raft for easy retrieval following deployment. The canopy is constructed of lightweight fabric. The survival kit may contain: • a first aid kit • flares • a signal mirror • a survival manual • a flashlight • water • a bailing bucket • a sponge If the raft is not fully inflated, manual inflation valves can be used to inflate the raft using the hand pump. The inflation valves are self-closing upon removal of the hand pump. WARNING: In a ditching situation, deployment of both the door 3 ramp/slide and door 4 slide/raft on the same side of the airplane will cause interference with the normal operation of the door 4 slide/raft. The door 4 slide/raft may be unusable. January 15, 2004 747-400 Flight Attendant Manual
作者:
帅哥
时间:
2008-12-28 03:14:44
Doors, Slides and Emergency Exits - Passenger Entry Doors Copyright © The Boeing Company. See title page for details. 7.20.10 D6-30151-TBC (pax) Slide/Raft Controls 1 Slide/Raft Detachment Handle Lift flap, pull handle completely free to release slide/raft from girt bar. Note: For ditching use only. 2 Manual Inflation Handle If the passenger entry door slide/raft does not deploy and inflate automatically, pull the manual inflation handle to inflate the slide/raft. Note: Typical passenger entry door interior, looking out 1 2 January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Passenger Entry Doors Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 7.20.11 Intentionally Blank January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Passenger Entry Doors Copyright © The Boeing Company. See title page for details. 7.20.12 D6-30151-TBC (pax) Evacuation Slide/Rafts - Slides Evacuation Slide/Rafts Deployed 5 4 2 1 January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Passenger Entry Doors Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 7.20.13 Slide Length, Width, And Door Sill Height Note: See Section 7.30, Overwing Emergency Exits, for detailed information on door 3L and 3R overwing slides and Section 7.30, Upper Deck Doors, for detailed information on the upper deck doors. Evacuation Slide/Raft - Rafts Slide/Raft Capacity The following table shows the number of occupants allowed in each slide/raft. [Option: Life raft provisions] Overhead stowage provisions for additional life rafts are available above doors 5L and 5R. After removing the rafts, the stowage doors must be closed so they do not obstruct the passageway. Slide Location Slide Length (approximate) Slide Lane Width (approximate) Door Sill Height - All landing gear down (approximate) Door 1 L & R 29.8 ft. (9.1 m.) 80 in. (208 cm.) 15.6 ft. (4.7 m.) Door 2 L & R 30.9 ft. (9.4 m.) 80 in. (208 cm.) 15.8 ft. (4.8 m.) Door 4 L & R 29.8 ft. (9.1 m.) 80 in. (208 cm.) 16.5 ft. (5.0 m.) Door 5 L & R 32.3 ft. (9.9m.) 68 in. (173 cm.) 16.8 ft. (5.1 m.) Raft Location Normal Capacity Overload Capacity Door 1 L & R 60 75 Door 2 L & R 60 75 Door 4 L & R 60 75 Door 5 L & R 56 70 January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Passenger Entry Doors Copyright © The Boeing Company. See title page for details. 7.20.14 D6-30151-TBC (pax) Main Deck Entry Doors Main Deck Passenger Entry Door Preflight The main deck door slide/raft pressure gauge and the power assist pressure gauge must indicate in the green range. Slide/raft Gas Bottle Pressure Gage Door Power Assist Gas Bottle Pressure Gage Passenger Entry Door (typical) January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Passenger Entry Doors Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 7.20.15 Main Deck Passenger Entry Door Normal Operation – Interior Close Door To close the door: • raise the gust lock release handle to release the gust lock • pull the door toward you • close the door slowly and firmly • rotate the door operating handle to latch the door. WARNING: Avoid the path of the door operating handle whenever the door is closed. Rotate the handle slowly. ensure the opposite handle path is clear. Rapid and unexpected movement of the door operating handle could injure personnel on the opposite side of the door. WARNING: Keep hands and fingers well clear of door edges while closing door. Injury will result if hands or fingers are not clear of door edges. To arm the power assist system and slide/raft, position the mode select lever to AUTOMATIC. • Raising the door mode select panel access cover and moving the lever to AUTOMATIC engages the girt bar to the door sill for automatic deployment of slide/rafts when the door is opened from the inside. Open Door To disarm the power assist system and slide/raft automatic deployment position the mode select lever to MANUAL. • Raising the door mode select panel access cover and moving the lever to the MANUAL position disengages the girt bar from the door sill. To open the door: • disarm the door • rotate the door operating handle fully aft (OPEN) • push the door open until the gust lock engages WARNING: Avoid the path of the door operating handle whenever the door is closed. Rotate the handle slowly. ensure the opposite handle path is clear. Rapid and unexpected movement of the door operating handle could injure personnel on the opposite side of the door. January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Passenger Entry Doors Copyright © The Boeing Company. See title page for details. 7.20.16 D6-30151-TBC (pax) Main Deck Passenger Entry Door Normal Operation - Exterior Close Door To close the door: • raise the door hold-open release lever to release the gust lock • when the door reaches the “cocked” position, extend the exterior door operating handle • rotate the door operating handle to latch the door closed • after full rotation, release the door operating handle and push the handle to the stowed position WARNING: Keep hands and fingers clear of door edges while closing the door. CAUTION: The outside door handle is spring loaded to retract into the recess. Release handle carefully to avoid pinching fingers. WARNING: The inside door handle rotates as the outside handle is rotated. Rotate the outside handle slowly to avoid rapid or unexpected movement of the inside door handle, which could injure personnel inside the airplane. Note: When the door is closed using the exterior door operating handle, the door mode select lever remains in MANUAL and must be manually positioned to AUTOMATIC to provide normal power assist system operation and automatic slide deployment. January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Passenger Entry Doors Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 7.20.17 Open Door To open the door: • push in the door operating handle latch and pull the door operating handle fully outward from the recess (pulling the handle from the recess disarms the power assist system and disengages the girt bar from the door sill) • rotate the door handle (rotating the handle fully unlatches the door) • release the handle and rotate the door to the full open position (this engages the door gust lock) WARNING: The inside door operating handle rotates as the outside handle is rotated. Rotate the outside handle slowly to avoid rapid or unexpected movement of the inside door handle, which could injure personnel inside the airplane. CAUTION: The outside door handle is spring loaded to retract into the recess. Release handle carefully to avoid pinching fingers. Note: When the mode select lever is in AUTOMATIC position and the door is opened using the exterior door handle, the mode select lever mechanically positions to MANUAL and the door may be opened without slide/raft deployment. January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Passenger Entry Doors Copyright © The Boeing Company. See title page for details. 7.20.18 D6-30151-TBC (pax) Intentionally Blank January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits Chapter 7 Overwing Emergency Exits Section 30 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 7.30.1 7.30 Doors, Slides and Emergency Exits-Overwing Emergency Exits [Option shown: AUTOMATIC/MANUAL; Option: ARM/DISARM, FLIGHT/PARK]
作者:
帅哥
时间:
2008-12-28 03:14:53
Overwing Emergency Exit Overview The overwing emergency exits, doors 3L and 3R, are for emergency use only and are inward-outward opening, plug-type doors, identical in appearance and operation to the passenger entry doors. When opened, the door first moves inward then swings outward and forward. Each door is held in the open position by a gust lock.The gust lock drops into a latch as the door nears its forward limit of travel. A window in the door allows observation outside of the airplane. An overwing emergency exit ramp and slide are contained in the door 3L and 3R door bustle. Escape straps located at Door 3 can be attached to a fitting near the leading edge of the wing between the engines. The escape straps will aid personnel in maintaining footing while moving outboard on the wing during ditching. When the door mode select lever is in AUTOMATIC position and the door operating handle is rotated 180 degrees, the door begins to open and the power assist system activates. If the ramp/slide does not open automatically, pulling the manual inflation handle located in the door sill will inflate the ramp/slide. WARNING: Door 3 ramp/slides are not usable as life rafts and should not be deployed during a ditching situation. If door 3 is used as an alternate evacuation exit during ditching, the door mode select lever must be in MANUAL to allow the door to be opened without deploying the ramp/slide. Door 3 is not to be used as a primary exit during ditching operations. Deployment of both the door 3 ramp/slide and the door 4 slide/raft on the same side of the aircraft will cause interference with the normal operation of the door 4 slide/raft and the door 4 slide/raft may then be unusable. January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Overwing Emergency Exits Copyright © The Boeing Company. See title page for details. 7.30.2 D6-30151-TBC (pax)
作者:
帅哥
时间:
2008-12-28 03:15:02
Overwing Emergency Exit Controls 1 Door Assist Handle Used to apply leverage needed to open and latch door if power assist system fails. 2 Door Mode Select Panel See following graphic. 3 Ramp/Slide Gas Bottle Pressure Gage Indicates pressure in bottle used to inflate ramp/slide. If the gage needle is outside the green zone, the system is unusable. 1 5 6 7 8 3 2 4 January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Overwing Emergency Exits Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 7.30.3 4 Door Power Assist Gas Bottle Pressure Gage Indicates pressure in bottle used to assist in door opening. If the gage needle is outside the green zone, the system is unusable. 5 Escape Ramp Lamp Illuminates entire ramp. Exterior fuselage lights illuminate the rest of the slide. 6 Viewing Window Allows observation outside the airplane. 7 Door Operating Handle Latches and unlatches the door for opening. To open the door – rotate in the direction of the arrow. To close the door – rotate in the opposite direction of the arrow. 8 Ramp/Slide Bustle Bustle contains the overwing ramp and slide. January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Overwing Emergency Exits Copyright © The Boeing Company. See title page for details. 7.30.4 D6-30151-TBC (pax) Door Mode Select Panel 1 Door Mode Select Lever Used to select the required mode for flight, AUTOMATIC, or arrival, MANUAL. 2 Access Cover Open - allows access to the door mode select lever. Closed - allows verification of the door mode select lever position. AUTOMATIC MANUAL Door 3 2 4 1 5 January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Overwing Emergency Exits Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 7.30.5 3 MANUAL Door is disarmed if the mode select lever knob is visible in the viewport. Moving the door operating handle to the OPEN position disables automatic ramp/slide deployment Note: A lockout pin may be installed. The lockout pin prevents the movement of the mode select lever from the MANUAL position 4 Clear Plastic Viewport MANUAL - knob visible in viewport indicates door is in the disarmed mode. AUTOMATIC - knob visible in viewport indicates door is in the armed mode. 5 AUTOMATIC Door is armed if the mode select lever knob is visible in the viewport. When the door operating handle is moved to the OPEN position: • the door is powered open • the ramp/slide automatically deploys. Note: If the door is opened from the outside, the mode select lever automatically moves to the MANUAL position. CAUTION: To ensure that the door is properly armed or disarmed, the door mode select lever knob must be visible in the view port window. January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Overwing Emergency Exits Copyright © The Boeing Company. See title page for details. 7.30.6 D6-30151-TBC (pax) Door Mode Select Lever Operation The mode select lever on each door controls the arming and disarming of: • the power assist system • the ramp/slide Setting the mode select lever to MANUAL disarms the power assist system and the door can be opened normally without power assist and without deploying the ramp/slide. Note: A lockout pin may be installed. The lockout pin prevents the movement of the mode select lever from the MANUAL position Setting the mode select lever to AUTOMATIC arms the power assist system and the rotation of the inside door operating handle to OPEN activates the power assist and automatically deploys and inflates the ramp/slide. Rotating the door operating handle fully aft (OPEN) with the mode select lever in the AUTOMATIC position activates the power assist system and automatically deploys and inflates the ramp/slide. In certain adverse airplane attitudes, an initial outward push on the door operating handle may be required to supplement the power assist system.
作者:
帅哥
时间:
2008-12-28 03:15:13
CAUTION: To ensure that the door is properly armed or disarmed, the door mode select lever knob must be visible in the viewport. January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Overwing Emergency Exits Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 7.30.7 Dedicated Assist Space Near each door are dedicated assist spaces. The dedicated assist spaces are located on either side of the door passageway. During an emergency evacuation, it is important that the flight attendants grasp the assist handle and place themselves in the dedicated assist space to ensure that they are not blocking the exit in any way. Blocking the exit prohibits dual lane flow onto the slides. Note: The use of the aft facing dedicated assist space allows continuous monitoring of the slide without interrupting passenger flow. Assist Handle Dedicated Assist Space (typical) January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Overwing Emergency Exits Copyright © The Boeing Company. See title page for details. 7.30.8 D6-30151-TBC (pax) Overwing Ramp/Slide The overwing ramp/slide is used for emergency evacuation of the airplane during land passenger evacuation operations only. The overwing ramp/slide is installed in the door bustle. It is a dual lane slide that deploys automatically when the mode select lever is in the AUTOMATIC position and the door operating handle is rotated a full 180 degrees. Slide readiness is indicated by a deployment indicator at the end of the ramp: Note: Visibility of the deployment indicator is the cue to immediately initiate evacuation. CAUTION: Block the exit while the slide is inflating. Do not allow passengers onto the wing until the slide is fully inflated. Full inflation is indicated when barber pole is visible. When evacuating the airplane, passengers must step onto the ramp from the door sill. Exterior emergency lights are mounted on the airplane fuselage which illuminate the wing walkway. The overwing ramp/slide has lights built into the sliding lanes and at the toe end. Barber Pole January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Overwing Emergency Exits Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 7.30.9 Overwing Ramp/Slide Manual Inflation Handle The overwing ramp/slide should deploy and inflate automatically. In the unlikely event that manual inflation is required, a manual inflation handle is located in the lower portion of the door frame. Pulling the manual inflation handle will inflate the slide. January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Overwing Emergency Exits Copyright © The Boeing Company. See title page for details. 7.30.10 D6-30151-TBC (pax) Overwing Door Slide Overwing Ramp/Slides Deployed Overwing Ramp/Slide Length, Width, And Door Sill Height Slide Location Slide Length (approximate) Slide Width (approximate) Trailing Edge of Wing Height - All landing gear down (approximate) Door 3L & 3R 45.5 ft. (13.9 m.) 84 in. (213 cm.) 11.2 ft. (3.4 m.) 3 January 15, 2004
作者:
帅哥
时间:
2008-12-28 03:15:21
747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Overwing Emergency Exits Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 7.30.11 Escape Strap An emergency escape strap is located in the aft end of the overhead stowage bin forward of doors 3L and 3R. The escape strap is used to assist the movement of passengers onto the wing in the event of a water landing. The escape strap can be attached to a fitting on the top of the wing between the engines. Escape Strap Overwing Exit Door 3L (typical) January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Overwing Emergency Exits Copyright © The Boeing Company. See title page for details. 7.30.12 D6-30151-TBC (pax) Overwing Emergency Exit Overwing Exit Preflight The overwing emergency exit ramp/slide pressure gauge and the power assist pressure gauge must indicate in the green range. Ramp/Slide Gas Bottle Pressure Gage Door Power Assist Gas Bottle Pressure Gage Overwing Emergency Exit (typical) January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Overwing Emergency Exits Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 7.30.13 Overwing Emergency Exit Normal Operation Before opening the overwing emergency exit and automatically deploying the overwing ramp/slide: • assess the escape route conditions • observe cabin interior and airplane exterior conditions to identify usable escape exits • ensure the airplane has stopped and the engines are shut down • verify the mode select lever is positioned to AUTOMATIC Then: • rotate the door operating handle aft (OPEN) • push the door until power assist system engages or until the exit door is fully open WARNING: Release the door operating handle once power assist system engages to prevent being pulled from the airplane. • continue to assist the door opening motion by using the assist handles on the door and on the door surround panel until the door is in the full open and latched position • verify that the door-mounted escape ramp deploys and inflates as the door is opened. • verify the barber pole is visible (off-wing escape slide is properly deployed) Note: If power assist system does not activate, direct two able-bodied passengers to assist in pushing the door out and forward to the open position. January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Overwing Emergency Exits Copyright © The Boeing Company. See title page for details. 7.30.14 D6-30151-TBC (pax) Intentionally Blank January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits Chapter 7 Upper Deck Doors Section 40 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 7.40.1 7.40 Doors, Slides and Emergency Exits-Upper Deck Doors [Option shown: AUTOMATIC/MANUAL; Option: ARM/DISARM, FLIGHT/PARK]
作者:
帅哥
时间:
2008-12-28 03:15:30
Upper Deck Doors Overview Two upper deck doors with slides are installed for emergency evacuation from the upper deck. The upper deck slides cannot be used as life rafts. Each upper deck door has a mode select lever that functions similar to the main deck mode select lever in controlling automatic slide deployment. With the mode select lever in AUTOMATIC, opening the door automatically deploys the escape slide. If an upper deck door opens, but the automatic system fails to deploy the escape slide, the slide can be deployed by pushing it out the door. Due to the heavy weight of the slide, manual deployment could require more than one person to push the slide out the door. Door warning straps are installed at each of the two upper deck doors. In flight, a flight lock mechanism is automatically activated to hold the upper deck door operating handle in the closed position. The door power assist system automatically opens the upper deck door when the mode select lever is in AUTOMATIC and the door operating handle is moved to OPEN. WARNING: If the door does not open or the slide fails, use the other door. If both doors fail to open, move the passengers to the main deck. The upper deck doors cannot be opened manually. WARNING: Do not use the upper deck doors during ditching operations. The upper deck slides are used for escape only and cannot be used as rafts. Note: If automatic slide inflation fails, the slides have a manual inflation handle located on the right side of the slide apron. WARNING: Extreme caution should be used during manual deployment of the slide to prevent falling out the door. January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Upper Deck Doors Copyright © The Boeing Company. See title page for details. 7.40.2 D6-30151-TBC (pax) Upper Deck Door Controls FWD 1 2 3 6 4 5 Upper Deck Door (typical) January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Upper Deck Doors Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 7.40.3 1 Door Operating Gas Bottle Pressure Gage Indicates pressure in bottle used to open the door. If the gage needle is outside the green zone, the system is unusable. 2 Door Ground Mode/Battery OK Panel See following graphic. 3 Door Mode Select Panel See following graphic. 4 Door Operating Handle OPEN: • lift handle in the direction of the arrow • unlatches door and permits opening of door • automatically deploys slide when door mode select lever is in the AUTOMATIC mode. 5 Escape Slide Pack Slide rotates through door when door is opened with the door mode select lever on AUTOMATIC. 6 Evacuation System Panel Used for initiating passenger evacuation. January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Upper Deck Doors Copyright © The Boeing Company. See title page for details. 7.40.4 D6-30151-TBC (pax) Door Mode Select Panel 1 AUTOMATIC Door is armed if the mode select lever handle is visible in the viewport. Note: If the door is opened from the outside, the mode select lever automatically moves to the MANUAL position. 2 Door Mode Select Lever Used to select the required mode for flight, AUTOMATIC, or arrival, MANUAL. 3 Access Cover Lift to use door mode select lever. Note: Cover will not close unless the mode select lever is in the AUTOMATIC or MANUAL position. 4 Clear plastic viewport The door mode select lever must be visible in the clear plastic viewport to ensure that the door is properly armed or disarmed. AUTOMATIC 1 2 3 5 4 January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Upper Deck Doors Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 7.40.5 5 MANUAL Door is disarmed if the mode select lever handle is visible in the viewport. CAUTION: To ensure that the door is properly armed or disarmed, the door mode select lever must be visible in the clear plastic viewport. Note: A lockout pin may be installed. The lockout pin prevents the movement of the mode select lever from the MANUAL position.
作者:
帅哥
时间:
2008-12-28 03:15:44
Door Mode Select Lever Operation The mode select lever on each door controls the arming and disarming of: • the door power assist system • the automatic deployment of the escape slide. Setting the mode select lever to MANUAL disarms the door power assist system and the door can be opened normally without power assist and without deploying the slide. Setting the mode select lever to AUTOMATIC arms the door power assist system and the rotation of the inside door operating handle to OPEN activates the door power assist system and automatically deploys and inflates the slide. The door power assist system is sufficient to open the upper deck door even if the airplane is not level because of landing gear collapse or uneven terrain. CAUTION: To ensure that the door is properly armed or disarmed, the door mode select lever must be visible in the clear plastic viewport. January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Upper Deck Doors Copyright © The Boeing Company. See title page for details. 7.40.6 D6-30151-TBC (pax) Door Ground Mode/Battery OK Panel 1 DOOR Ground (GND) MODE Light Illuminated (blue) - on ground or in flight when the flight lock mechanism is not in the locked position. 2 BATTERY OK Test Switch/Light Push - Illuminated (green) - battery charge is sufficient for door operation. Note: Light must be pushed and held for 3 - 5 seconds before it will illuminate. In flight, the flight lock mechanism automatically activates to hold the upper deck door operating handle in the closed position. If a flight lock fails, the DOOR GND MODE light illuminates over the door and the flight crew receives an EICAS message. In this condition, flight attendants should monitor the door closely and coordinate with the flight crew to prevent accidental operation when cabin pressure is 3 PSI or LESS. When pushed and held for 3-5 seconds, the BATTERY OK Test Light illuminates. This indicates that battery power is satisfactory to activate the upper deck door power assist system. DOOR GND TEST HOLD 3 SEC BATTERY MODE BATTERY OK FWD 1 2 January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Upper Deck Doors Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 7.40.7 Dedicated Assist Space Near each door is a dedicated assist space. During an emergency evacuation, it is important that the flight attendants grasp the assist handle and place themselves in the dedicated assist space to ensure that they are not blocking the exit in any way. Blocking the exit prohibits dual lane flow onto the slide. FWD Assist Handle Dedicated Assist Space January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Upper Deck Doors Copyright © The Boeing Company. See title page for details. 7.40.8 D6-30151-TBC (pax) Upper Deck Door Slide The upper deck slide is used for emergency evacuation of the airplane during land passenger evacuation operations only. The upper deck door slide is a dual lane slide that deploys automatically when the mode select lever is in the AUTOMATIC position and the door operating handle is lifted to the full up position. CAUTION: Block the exit while the slide is inflating. Do not allow passengers onto the slide until the slide is fully inflated. Upper Deck Door (typical view from inside airplane) January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Upper Deck Doors Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 7.40.9 Upper Deck Door Manual Inflation Handle To manually inflate the slide, pull the Manual Inflation Handle located on the right side of the slide apron. WARNING: Extreme caution should be used during manual deployment of the slide to prevent falling out the door. Upper Deck Door (typical view from inside airplane) January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Upper Deck Doors Copyright © The Boeing Company. See title page for details. 7.40.10 D6-30151-TBC (pax) Upper Deck Door Slides Upper Deck Door Slides Deployed Upper Deck Door Slide Length, Width, And Door Sill Height Slide Location Slide Length (approximate) Slide Lane Width (approximate) Door Sill Height - All landing gear down (approximate) Upper Deck (UD) 46.5 ft. (14.0 m) 68 in. (173 cm.) 25.5 ft. (7.75 m.) UD January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Upper Deck Doors Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 7.40.11
作者:
帅哥
时间:
2008-12-28 03:15:54
Upper Deck Door Upper Deck Door Preflight Push and hold the BATTERY OK Test Switch for 3-5 seconds and observe that the BATTERY OK light illuminates. This verifies that battery power is adequate to activate the upper deck door power assist system. The door power assist system reservoir gage must indicate in the green zone. If the gage needle is outside of the green zone, the system is unusable. FWD Battery OK Light Door Operating Gas Bottle Pressure Gage Evacuation Command Switch Upper Deck Door (typical) January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Upper Deck Doors Copyright © The Boeing Company. See title page for details. 7.40.12 D6-30151-TBC (pax) Upper Deck Door Normal Operation Lifting the door operating handle fully up (OPEN) with the mode select lever in the AUTOMATIC position automatically opens the door, deploys and inflates the slide. In certain adverse airplane attitudes, an initial outward push on the door handle may be required. Open Door To open the upper deck door and automatically deploy the slide: • assess the escape route conditions • observe cabin interior and airplane exterior conditions to identify usable escape exits • ensure the airplane has stopped and the engines are shut down • verify the mode select lever is positioned to AUTOMATIC • lift the door operating handle up (OPEN) WARNING: The upper deck door opens outward rapidly. Release the door operating handle once the door starts moving to prevent being pulled or falling from the airplane. WARNING: Block the exit while the slide is inflating. Do not allow passengers onto the slide until the slide is fully inflated. January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits Chapter 7 Non-Normal Operations Section 50 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 7.50.1 7.50 Doors, Slides and Emergency Exits-Non-Normal Operations [Option shown: AUTOMATIC/MANUAL; Option: ARM/DISARM, FLIGHT/PARK] Doors, Slides and Emergency Exits Non-Normal Operations Passenger Entry Door Non-Normal Operation Rotating the door handle fully aft (OPEN) with the mode select lever in the AUTOMATIC position activates the power assist system and automatically deploys and inflates the slide/raft. In certain adverse airplane attitudes, an initial outward push on the door handle may be required to supplement power assist system. Passenger Entry Door Power Assist System Does Not Activate If power assist system does not activate when the door handle is moved to OPEN: • direct two able-bodied passengers to assist in first pulling the door inward and then pushing the door out and forward to the open position. • push until the door is fully open • verify that the slide/raft automatically deploys WARNING: If the power assist system engages as the door is being pushed open, release the door operating handle immediately to prevent being pulled from the airplane. Passenger Entry Door Slide/Raft Does Not Automatically Inflate If the slide/raft does not automatically inflate: • pull and discard the manual inflation handle located on the doorsill • observe the slide/raft inflates WARNING: If the slide/raft still does not inflate after both automatic and manual deployment attempts, do not use. Redirect passengers to the nearest usable exit. January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Non-Normal Operations Copyright © The Boeing Company. See title page for details. 7.50.2 D6-30151-TBC (pax) Passenger Entry Door Slide/Raft Becomes Deflated If the slide/raft becomes deflated and another exit with an inflated slide/raft or slide is not available, the deflated slide/raft may be used as an apron slide: • direct two able-bodied passengers to climb down the slide/raft using it as a rope • direct the two passengers to then use the red webbing along the sides of the slide/raft to hold it taut while the remaining passengers exit one at a time January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Non-Normal Operations Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 7.50.3 Overwing Exit Non-Normal Operation Overwing Exit Power Assist System Does Not Activate If the power assist system does not activate when the door handle is moved to OPEN: • direct two able-bodied passengers to assist in pulling the door inward and then pushing the door out and forward to the open position • push until the door is fully open • verify that the slide automatically deploys (barber pole visible) WARNING: If the power assist engages as the door is being pushed open, release the door operating handle immediately to prevent being pulled from the airplane. Overwing Exit Slide Does Not Automatically Inflate If the slide does not automatically inflate (barber pole not seen): • pull and discard the manual inflation handle located in the doorsill • observe barber pole to verify inflation WARNING: If the slide still does not inflate after both automatic and manual deployment attempts, do not use. Redirect passengers to the nearest usable exit. January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Non-Normal Operations Copyright © The Boeing Company. See title page for details. 7.50.4 D6-30151-TBC (pax) Overwing Exit Slide Deploys But Becomes Deflated If the slide deploys but becomes deflated and another exit with an inflated slide or slide/raft is not available, the deflated slide may be used as an apron slide: • direct two able-bodied passengers to climb down the slide/raft using it as a rope • direct these individuals to use the hand-holds provided on the slide to hold it taut while the remaining passengers exit one at a time Barber Pole January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Non-Normal Operations Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 7.50.5 Upper Deck Doors If the door does not open or the slide fails, use the other door. WARNING: If both upper deck doors fail to open, move passengers to the main deck. The upper deck doors cannot be manually opened. Door Opens But Slide Fails To Automatically Deploy If the upper deck opens, but the slide fails to automatically deploy, the slide may be deployed by pushing it out the door. Direct two able-bodied passengers to assist in pushing the slide out the door. WARNING: Extreme caution should be used during manual deployment of the slide to prevent falling from the airplane. Note: The slide weighs approximately 275 pounds (126 kilograms) and the pivot point of the slide is at the doorsill. Flight Lock Fails In flight, the flight lock mechanism automatically activates to hold the upper deck door operating handle in the CLOSE position. If a flight lock fails, the DOOR GND MODE light illuminates over the door and the flight crew receives an EICAS message. In this condition, flight attendants should monitor the door closely and coordinate with the flight crew to prevent accidental operation when cabin pressure is 3 PSI or LESS. This condition should be coordinated with the flight deck. DOOR GND BATTERY TEST HOLD OK MODE 3 SEC BATTERY Door Ground Mode Light FWD January 15, 2004 747-400 Flight Attendant Manual Doors, Slides and Emergency Exits - Non-Normal Operations Copyright © The Boeing Company. See title page for details. 7.50.6 D6-30151-TBC (pax) Securing Main Deck Doors 1, 2, 4, or 5 In The Open Position To accomplish the smoke removal procedure, main entry doors (as designated by the Captain) need to be secured in the partially open position as follows: • ditching straps forward of doors 3 left and right can be used to secure door 2 or 4 without detaching strap from its compartment • attach snap end of strap to door assist handle on AFT door frame, place door operating handle to vertical (12 o’clock position), secure handle with several loops, return strap through assist handle and tie as shown below • pressure on the door maintains tension on the strap so it may be left unattended Note: If strap is not available, use any satisfactory item in the same manner to secure the doors. Door Assist Handle Strap Door Operating Handle January 15, 2004 747-400 Flight Attendant Manual Emergency Equipment Chapter 8 Table of Contents Section 0 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 8.TOC.0.1 8.0 Emergency Equipment-Table of Contents Emergency Equipment Overview . . . . . . . . . . . . . . . . . . . . . . 8.10.1 Emergency Equipment Symbols . . . . . . . . . . . . . . . . . . . . . . . 8.10.3 Emergency Equipment Location . . . . . . . . . . . . . . . . . . . . . . 8.10.4 Passenger Airplane . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.10.4 System Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.10.7 Oxygen Systems . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.10.7 Passenger and Flight Attendant Oxygen . . . . . . . . . . . . . . 8.10.7 Decompression . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.10.7 Portable Oxygen . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.10.8 Protective Breathing Equipment (Smoke Hoods) . . . . . . . . . . 8.10.9 Fire Extinguishers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.10.10 Water Fire Extinguishers . . . . . . . . . . . . . . . . . . . . . . . . . 8.10.10 Halon Fire Extinguishers . . . . . . . . . . . . . . . . . . . . . . . . . 8.10.12 Emergency Locator Transmitter (ELT) . . . . . . . . . . . . . . . . . 8.10.14 Miscellaneous Emergency Equipment . . . . . . . . . . . . . . . . . 8.10.14 Escape Strap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.10.15 Smoke Barrier . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.10.16
作者:
帅哥
时间:
2008-12-28 03:16:05
January 15, 2004 747-400 Flight Attendant Manual Copyright © The Boeing Company. See title page for details. 8.TOC.0.2 D6-30151-TBC (pax) Emergency Equipment - Table of Contents Intentionally Blank January 15, 2004 747-400 Flight Attendant Manual Emergency Equipment Chapter 8 System Description Section 10 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 8.10.1 8.10 Emergency Equipment-System Description [Options shown: Emergency evacuation system installed, door 5 overhead crew rest installed] Emergency Equipment Overview This chapter describes the emergency equipment located throughout the airplane, including: • passenger cabin emergency equipment and location • passenger and flight attendant oxygen systems • protective breathing equipment • fire extinguishers • emergency locator transmitters (ELTs) January 15, 2004 747-400 Flight Attendant Manual Emergency Equipment - System Description Copyright © The Boeing Company. See title page for details. 8.10.2 D6-30151-TBC (pax) Intentionally Blank January 15, 2004 747 Flight Attendant Manual Emergency Equipment - System Description Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 8.10.3 Emergency Equipment Symbols EQUIPMENT PORTABLE BREATHING (PBE) HALON EXTINGUISHER EXTINGUISHER WATER O 2 H L A H OXYGEN PORTABLE 2 O O 2 OXYGEN PORTABLE SMOKE MASK MASK OXYGEN BOTTLE BOTTLE WITH EMERGENCY PROTECTIVE GLOVES LOCATOR TRANSMITTER FLASHLIGHT MEGAPHONE VEST LIFE KIT FIRST AID NOTE: Some symbols do not apply to all configurations. GOGGLES SMOKE WITH SLIDE EXIT PATH EXIT PATH WITH ESCAPE SLIDE/RAFT SIGNAL LIGHT AXE CRASH BARR SMOKE BARRIER SMOKE DEVICE EMERGENCY ESCAPE STOWAGE RAFT / LIFE January 15, 2004 747 Flight Attendant Manual Emergency Equipment - System Description Copyright © The Boeing Company. See title page for details. 8.10.4 D6-30151-TBC (pax) Emergency Equipment Location Passenger Airplane [Passenger typical] Flight Deck 2 O L A H At each crew station: (4) 1 January 15, 2004 747 Flight Attendant Manual Emergency Equipment - System Description Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 8.10.5 Upper Deck/Door 5 Overhead Crew Rest GAL GAL GAL Escape Hatch (on floor, 1 (2) (2) 2 O L A H O 2 H L A H O 2 H under bunk) Each attendant seat stowage: Under each seat: 1 Door 5 Overhead Crew Rest BARR SMOKE Flight Crew Rest January 15, 2004 747 Flight Attendant Manual Emergency Equipment - System Description Copyright © The Boeing Company. See title page for details. 8.10.6 D6-30151-TBC (pax) Main Deck Each attendant seat stowage: Under each seat: 1 1 As installed. (2) 2 O (2) 2 O 2 O L A H L A H L A H L A H (2) 2 O (2) 2 O (2) 2 O (2) 2 O O 2 H O 2 H (2) 2 O (2) 2 O O 2 H January 15, 2004 747-400 Flight Attendant Manual Emergency Equipment - System Description Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 8.10.7
作者:
帅哥
时间:
2008-12-28 03:16:26
Oxygen Systems [Typical] Two independent oxygen systems are provided, one for the flight crew and one for the passengers. Portable oxygen cylinders are located in the flight deck and passenger cabin for emergency use. Passenger and Flight Attendant Oxygen The passenger oxygen system is supplied by bottled gaseous oxygen. The oxygen bottles provide oxygen to the passenger, attendant stations, and lavatory service units. The passenger oxygen masks are located above the passenger seats in the passenger service units (PSUs). Each mask oxygen valve is held closed by a pin inserted into the valve. Pulling on the mask withdraws the pin, causing the mask oxygen valve to open and oxygen to flow to that mask. The masks automatically drop from the PSUs if cabin altitude exceeds approximately 14,000 feet. The passenger masks can be manually deployed from the flight deck. Note: If the masks fail to drop from a PSU, the cover of the oxygen compartment can be opened manually by releasing the door latch. The latch can be opened by inserting a hair pin or a thin rod into the hole of the compartment cover. Decompression If cabin altitude exceeds approximately 10,000 feet, the following automatic events take place: • cabin lights come on full bright • one LO chime sounds through out the cabin • NO SMOKING/FASTEN SEAT BELT signs illuminate and corresponding chimes sound. These events warn the flight attendants that a possible decompression is about to occur. Flight attendants must sit down, fasten their seat belts, and prepare to put oxygen masks on. [Option: Passenger only, overhead door 5 crew rest installed] Note: Flight attendant guidelines for decompression while occupying the door 5 crew rest area are contained in Chapter 11.20, Crew Rest, Non-Normal Situation Guidelines. January 15, 2004 747-400 Flight Attendant Manual Emergency Equipment - System Description Copyright © The Boeing Company. See title page for details. 8.10.8 D6-30151-TBC (pax) Portable Oxygen There are portable oxygen bottles stowed in various locations in the passenger cabin. The bottles are fitted with disposable mask and safety straps and are used for first aid purposes or as walk-around units. Portable Oxygen Bottle Preflight During the preflight of the portable oxygen bottle, check the following: • the ON-OFF valve is OFF • the Oxygen Pressure Gage is in the FULL range • the mask is attached to the bottle. Portable Oxygen Bottle Use To use the portable oxygen bottle: • use safety strap Note: Use extreme care while transporting portable oxygen bottle. • remove mask from plastic bag • open dust cover and attach the fitting • rotate the ON-OFF valve fully counter-clockwise • place mask over nose and mouth. 2000 FULL 1500 1000 500 0 PRESSURE Oxygen Pressure Gauge FULL range Oxygen Hi Outlet (4 liters per minute) Mask Safety strap ON-OFF Valve LO Outlet (2 liters per minute) January 15, 2004 747-400 Flight Attendant Manual Emergency Equipment - System Description Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 8.10.9 Protective Breathing Equipment (Smoke Hoods) Protective breathing equipment (PBE) is installed in the passenger cabin. The PBE provides an oxygen supply and smoke protection, and are to be used when fighting a fire. The smoke hood is placed over the head and, when activated by a starter lanyard, provides approximately 15 minutes of oxygen. Detailed operating instructions are placarded on the container. WARNING: Human hair is highly flammable. Hair that protrudes through the neck seal of the PBE could ignite if brought into direct contact with a flame. CAUTION: This device produces oxygen which vigorously accelerates combustion. Do not expose the device to direct flame or remove in the immediate vicinity of fire or flame. Due to oxygen saturation of the hair, do not smoke or become exposed to fire or flame immediately after removing. Speaking Diaphram Tension Strap Starter Lanyard Full Face Mask Hood 15 Minute Oxygen Generator January 15, 2004 747-400 Flight Attendant Manual Emergency Equipment - System Description Copyright © The Boeing Company. See title page for details. 8.10.10 D6-30151-TBC (pax) Fire Extinguishers Water and halon fire extinguishers are located throughout the passenger cabin and flight deck. Water Fire Extinguishers Water fire extinguishers contain a solution of water mixed with antifreeze. Water fire extinguishers are to be used on fabric or paper fires only. They are not to be used on electrical or grease fires. CAUTION: Antifreeze compound has been added to the water which makes it unfit for drinking. CAUTION: Do not use on electrical or grease type fires. January 15, 2004 747-400 Flight Attendant Manual Emergency Equipment - System Description Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 8.10.11 Water Fire Extinguisher Preflight Check that the safety wire and seal on the handle are intact. Water Fire Extinguisher Operation To use the water fire extinguisher: • remove it from stowage • turn handle clockwise as far as possible (charges bottle with CO2) • hold bottle upright • direct nozzle at base of fire • press trigger to discharge. CAUTION: Do not use on electrical or grease type fires. Water Fire Extinguisher Recharging To recharge the water fire extinguisher in flight: • unscrew top (the CO2 charge bleeds off) • refill with water • replace top • unscrew handle • replace CO2 cylinder • reinstall handle (the extinguisher now ready for use). Trigger Discharge Nozzle Turn to puncture CO2 cartridge January 15, 2004 747-400 Flight Attendant Manual Emergency Equipment - System Description Copyright © The Boeing Company. See title page for details. 8.10.12 D6-30151-TBC (pax) Halon Fire Extinguishers Halon fire extinguishers contain a liquefied gas agent under pressure. The extinguisher pressure indicator shows three pressure ranges: • acceptable • recharge • overcharged. A safety pin with a pull ring prevents accidental trigger movement. When released, the liquefied gas agent vaporizes and extinguishes the fire. The extinguisher is effective on all types of fires, but is used primarily on electrical, fuel, and grease fires. WARNING: If a halon fire extinguisher is to be discharged in the flight deck area, all flight crew members must wear oxygen masks and use 100% oxygen with emergency selected. CAUTION: For electrical fires, remove the power source as soon as possible. Avoid discharging directly on persons due to possibility of suffocating effects. Do not discharge too close to fire as the discharge stream may scatter the fire. As with any fire, keep away from the fuel source. Avoid breathing vapors, fumes and heated smoke as much as possible. January 15, 2004 747-400 Flight Attendant Manual Emergency Equipment - System Description Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 8.10.13 Halon Fire Extinguisher Preflight Check: • pressure gage is in the green band • the ring pin is in place through the handle and lever. Halon Fire Extinguisher Operation To use the Halon fire extinguisher: • pull ring pin from lever and handle • hold extinguisher upright with hand under handle and thumb on top of lever • from a distance of 6 to 10 feet, direct the nozzle towards the base of the fire source • squeeze the lever downward with thumb • spray at the base of the flame in quick side-to-side -motion. Note: The extinguisher stream will shoot over 10 foot distance. WARNING: If a halon fire extinguisher is to be discharged in the flight deck area, all flight crew members must wear oxygen masks and use 100% oxygen with emergency selected. CAUTION: For electrical fires, remove the power source as soon as possible. Avoid discharging directly on persons due to possibility of suffocating effects. Do not discharge too close to fire as the discharge stream may scatter the fire. As with any fire, keep away from the fuel source. Avoid breathing vapors, fumes and heated smoke as much as possible. Discharge Nozzle Lever Ring Pin Pressure Gauge Handle January 15, 2004 747-400 Flight Attendant Manual Emergency Equipment - System Description Copyright © The Boeing Company. See title page for details. 8.10.14 D6-30151-TBC (pax) Emergency Locator Transmitter (ELT) An ELT is installed forward of Door 5. The ELT activates by high deceleration forces or when the flight deck ELT switch is placed ON by the flight crew. The ELT can be deactivated by placing the ELT switch to RESET. [Typical] Two emergency locator transmitters are installed on the airplane: • one in the door 1L slide/raft • one in the door 4R slide/raft Miscellaneous Emergency Equipment Additional equipment is stowed at strategic locations throughout the airplane. This includes: • crash axe • megaphones • flashlights • first aid kits • smoke goggles • life vests at each crew member station and passenger seat [Option: Overhead door 5 crew rest installed] Emergency equipment located in the door 5 crew rest area includes: • portable oxygen bottles • additional emergency equipment as installed by the interior vendor January 15, 2004 747-400 Flight Attendant Manual Emergency Equipment - System Description Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 8.10.15 Escape Strap An emergency escape strap is located in the aft end of the overhead stowage bin forward of doors 3L and 3R. The escape strap is used to assist the movement of passengers onto the wing in the event of a water landing. The escape strap can be attached to a fitting on the top of the wing between the engines. Escape Strap Overwing Exit Door 3L (typical) January 15, 2004 747-400 Flight Attendant Manual Emergency Equipment - System Description Copyright © The Boeing Company. See title page for details. 8.10.16 D6-30151-TBC (pax) Smoke Barrier The smoke barrier can be used on the ground to prevent smoke migration by covering the stairwell between the main deck and the upper deck. To deploy the smoke barrier: • pull latch release • allows cover to fall free and expose the smoke barrier • insert fingers in barrier loops • pull barrier toward railing Cover Release Latch Smoke Barrier Smoke Barrier Ground use only Ground use only January 15, 2004 747-400 Flight Attendant Manual Emergency Equipment - System Description Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 8.10.17 • drape barrier over railing • engage snaps along top of stairwell and railing sides • press flap at bottom of barrier against carpet • ensures good contact between velcro flap and carpet CAUTION: The smoke barrier is for ground use only. Snaps Ground use only January 15, 2004 747-400 Flight Attendant Manual Emergency Equipment - System Description Copyright © The Boeing Company. See title page for details. 8.10.18 D6-30151-TBC (pax) Intentionally Blank January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines Chapter 9 Table of Contents Section 0 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 9.TOC.0.1 9.0 Non-Normal Situation Guidelines-Table of Contents Cabin Fire Fighting & Smoke Removal Overview . . . . . . . . 9.10.1 Fire Prevention . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.10.1 Cabin Fire Fighting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.10.2 Specific Cabin Fire Fighting . . . . . . . . . . . . . . . . . . . . . . . . . 9.10.4 Lavatory Fire . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.10.4 Closet Fire . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.10.5 Galley Fire . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.10.6 Door 5 Overhead Crew Rest . . . . . . . . . . . . . . . . . . . . . . . 9.10.6 In-flight Entertainment (IFE) System Smoke or Fire . . . . 9.10.6 Smoke/Fumes Removal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.10.8 Smoke Barrier . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.10.10 Land Evacuation Overview . . . . . . . . . . . . . . . . . . . . . . . . . . 9.20.1 Passenger Entry Doors and Upper Deck Doors . . . . . . . . 9.20.2 Overwing Emergency Exits . . . . . . . . . . . . . . . . . . . . . . . . 9.20.2 Emergency Evacuation Guidelines . . . . . . . . . . . . . . . . . . . . . 9.20.3 Initiate Evacuation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.20.3 Escape Slide Usability . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.20.4 If Exit Is Usable . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.20.10 If Exit Is Not Usable . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.20.12 Flight Attendants Not Assigned To An Exit . . . . . . . . . . 9.20.14 Ditching Overview . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.30.1 Ditching Guidelines . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.30.2 Initiate Ditching Evacuation . . . . . . . . . . . . . . . . . . . . . . . 9.30.2 Board Passengers Into The Passenger Entry Door Slide/Raft . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.30.6 Slide/Raft Portability . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.30.8 Slide/Raft Portability Procedures . . . . . . . . . . . . . . . . . . . 9.30.8 January 15, 2004 747-400 Flight Attendant Manual Copyright © The Boeing Company. See title page for details. 9.TOC.0.2 D6-30151-TBC (pax) Non-Normal Situation Guidelines - Table of Contents Intentionally Blank January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines Chapter 9 Cabin Fire Fighting & Smoke Removal Section 10 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 9.10.1 9.10 Non-Normal Situation Guidelines-Cabin Fire Fighting & Smoke Removal Option shown: AUTOMATIC/MANUAL, Option: ARM/DISARM, FLIGHT/PARK; Option shown: Overhead door 5 crew rest installed Cabin Fire Fighting & Smoke Removal Overview This section provides guidelines for fire prevention and cabin fire fighting. Fire Prevention The flight attendants practice fire prevention by watching for unsafe passenger actions, and the immediate elimination of potential fire hazards. In particular, attention should be directed to the lavatories. Make frequent checks of the lavatories to assure that no smoke is present and good housekeeping exists. Check trash containers for partly open flapper doors due to overfull or jammed conditions. These containers should also be inspected for discarded objects which could be hazardous, such as cologne bottles or spray cans. Put these objects into the galley trash container. Accumulated waste paper and other flammable trash sometimes exceed the capacity of passenger cabin storage units. Since this affects fire safety, place this trash in the galley trash container or other suitable container. Another area susceptible to fire is the passenger cabin lower sidewall. Flammable items over return air grills have ignited unobserved because the return airflow carried smoke and fumes away from the passengers. Maintain surveillance of floor areas, particularly in the smoking zones, to keep clothing, bags, papers, and so on, from being deposited where they may be a fire hazard. January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Cabin Fire Fighting & Smoke Copyright © The Boeing Company. See title page for details. 9.10.2 D6-30151-TBC (pax) Cabin Fire Fighting CAUTION: Put on heat resistant protective clothing. For protection from smoke inhalation, put on a smoke hood with oxygen or a portable oxygen bottle with smoke mask attached. Immediately attack the fire with the nearest appropriate type fire extinguisher. Direct the extinguishing agent at the base of the flames at the near edge and bottom of the fire first, and then progress forward and upward. Move the discharge nozzle slowly with a side-to-side sweeping motion. Immediately notify the flight deck. Request help from crew members. Continuous communication provides information essential for making safety-of-flight decisions. Remove electrical power from the affected area. Bring additional fire fighting equipment to the fire scene as necessary: • portable oxygen bottle with smoke mask attached and/or smoke hood with oxygen • crash axe • water fire extinguisher • halon fire extinguisher • flashlight Use the crash axe to obtain access, if necessary. Rapid access to the fire may require the destruction of cabin wall panels. The crash axe may also be required to obtain access of a suspected electrical fire behind a wall. If the fire is not immediately extinguished, remove all portable oxygen cylinders from the vicinity of the fire. Advise the passengers to stay seated or move them as required. January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Cabin Fire Fighting & Smoke Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 9.10.3 If the fire produces excessive smoke and fumes inside the cabin: • request smoke evacuation procedures from the flight deck • continuously observe passengers for signs of panic and take additional action if needed • relocate passengers away from the area of severe smoke and fumes • administer 100% oxygen using portable oxygen bottles to any passengers experiencing respiratory difficulties • instruct passengers to breathe through wet handkerchiefs or other appropriate materials. WARNING: Do not deploy passenger oxygen masks. Note: The oxygen system is for use only during a cabin pressure loss. Most oxygen mask air is cabin air drawn through the mask inhalation valve; smoke in the cabin would be inhaled. WARNING: Do not use passenger oxygen masks as smoke masks. When the fire is extinguished, a water fire extinguisher or other cooling liquid should be used to quench any smoldering embers and prevent re-ignition: • the stream from a water fire extinguisher is relatively narrow and should be carefully directed into each burning portion. A finger or thumb placed on the nozzle creates a wider spray pattern • all burned material should be thoroughly soaked with water and may need to be broken apart to completely extinguish the fire • to conserve the hand held fire extinguisher, water, coffee, carbonated beverages, and so on, can be poured onto the embers. Smoldering material may be soaked in a lavatory/galley sink or in a pot of coffee Inspect adjacent areas to ensure the fire has not spread. January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Cabin Fire Fighting & Smoke Copyright © The Boeing Company. See title page for details. 9.10.4 D6-30151-TBC (pax) Specific Cabin Fire Fighting Fires in the lavatories, closets, or galleys may present special difficulties. Lavatory Fire Feel the door. If the door is hot: • keep the door closed • use a crash axe to chop a small hole in the upper part of the door just big enough to receive a fire extinguisher nozzle • discharge the fire extinguishing agent, preferably halon, into the hole • discharge the extinguisher completely • if needed, discharge the remaining extinguishers into the same hole to build up and maintain a high concentration of extinguishing agent If the door is cool: • carefully open the door and locate the fire • discharge the hand held fire extinguisher onto the fire • thoroughly douse the affected area with water • if trapped towels or cups are burning in the waste chute or the waste container, discharge the extinguishing agent directly into the chute Supplies stored in dispensers are normally tightly packed and less likely to catch fire than loose paper items; however, these stored items can contribute to an existing fire. January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Cabin Fire Fighting & Smoke Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 9.10.5 Closet Fire Closets with Curtains • locate the source of the fire and apply extinguishing agent • remove the coats and other contents that are not burning to gain access to a fire in a remote area of the closet • check that flames have been extinguished and thoroughly douse the burned materials with water • monitor the closet to ensure the fire remains out Closets with Doors Feel the closet walls and door for hot spots. If the walls or door are hot: • keep the door closed • seal any space at the base of the closet door with blankets or heavy clothing • use a crash axe to chop a small hole in the upper part of the door just big enough to receive a fire extinguisher nozzle • discharge the fire extinguishing agent, preferably halon, into the hole • discharge the fire extinguishing agent, preferably halon • monitor the closet to ensure the fire remains out • if needed, discharge the remaining extinguishers into the same hole to build up and maintain a high concentration of extinguishing agent If the walls and door are cool: • carefully open the door and locate the fire • discharge the hand held fire extinguisher onto the fire • remove coats and other contents that are not burning to gain access to a fire in a remote area of the closet • thoroughly douse the burned materials with water • monitor the closet to ensure the fire remains out January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Cabin Fire Fighting & Smoke Copyright © The Boeing Company. See title page for details. 9.10.6 D6-30151-TBC (pax) Galley Fire Galley electrical power should immediately be shut off for malfunctions such as fire, smoke, electrical arcing, and so on. If there is a fire in the galley: • remove electrical power from the galley by placing the galley emergency power OFF switch to the OFF position. • inform the flight deck. • determine type of fire • extinguish the fire using the appropriate hand held fire extinguisher Door 5 Overhead Crew Rest [Option: Overhead door 5 crew rest installed] For overhead door 5 crew rest area fire fighting guidelines, see Chapter 11, Section 20, Crew Rest Non-Normal Situation Guidelines for information on overhead crew rest fire fighting. In-flight Entertainment (IFE) System Smoke or Fire [Option shown: Video Control Center (VCC); Option: Purser Work Station] In the event of smoke or fire caused by any of the in-flight entertainment system (IFE) components, all electrical power should be removed from the IFE system. In the event of smoke or fire caused by any of the in-flight entertainment system (IFE) components, all electrical power should be removed from the IFE system and passenger seats. There is one master IFE power switch and eight individual passenger zone switches. Passenger zone switches are: • IFE Zone A • IFE Zone B • IFE Zone U/D • IFE Zone C • IFE Zone D (LHS) • IFE Zone D (RHS) • IFE Zone E (LHS) • IFE Zone E (RHS) Note: The IFE Master power switch will remove IFE, Airshow, and PC power from all passenger cabin zones while the individual power switches remove IFE, Airshow, and PC power to the respective zone only. January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Cabin Fire Fighting & Smoke Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 9.10.7 Power is removed by moving the IFE ZONE Power switch, located in the Video Control Center (VCC), for the respective passenger zone to the OFF position. This removes all electrical power to that zone: • the in-seat audio/video system equipment • audio entertainment players • video entertainment players • overhead video system and displays/projectors • in-seat video displays/audio in the crew rest areas • integrated telephones • the passenger control units (PCUs) • the passenger seat • seat motor power (as applicable) • personal computer power outlet (as applicable) • in-flight passenger cabin telephones Note: If any IFE Master Power switch is placed in the OFF position, no passenger service functions (reading lights or attendant call) are available. Note: Moving the IFE Master power switch to the OFF position does not cause an EICAS message to be displayed on the flight deck. WARNING: Once power is removed from the IFE system or passenger IFE zone, do not turn the IFE power switch back on for the remainder of the flight. January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Cabin Fire Fighting & Smoke Copyright © The Boeing Company. See title page for details. 9.10.8 D6-30151-TBC (pax) Smoke/Fumes Removal The smoke/fumes removal procedure requires close coordination with the flight deck. To accomplish the smoke/fumes procedure: • verify flight deck door closed • establish communication with the flight deck • determine the origin of the smoke (in the forward or aft passenger cabin) • at Captain’s direction, open doors: • position door mode selector lever to MANUAL • rotate the door operating handle toward the OPEN position Note: If the smoke/fumes concentration is determined to be in the forward section of the cabin, a door 1 or a door 2 and a door 4 or a door 5 will be opened. Note: If the concentration of smoke/fumes is determined to be in the aft section of the cabin, only one door 2 will be opened. January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Cabin Fire Fighting & Smoke Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 9.10.9 • secure the door operating handle in the 12 o’clock position • ditching straps forward of doors 3 left and right can be used to secure door 2 or 4 without detaching strap from its compartment • attach snap end of strap to door assist handle on AFT door frame, place door operating handle to vertical (12 o’clock position), secure handle with several loops, return strap through assist handle and tie as shown below • pressure on the door maintains tension on the strap so it may be left unattended. Note: If strap is not available, use any satisfactory item in the same manner to secure the doors. When the smoke/fumes are evacuated, and at the Captain’s direction: • remove strap • rotate the door operating handle to the CLOSED position • position door mode selector lever to AUTOMATIC. Note: The forward door must be closed before closing the aft door. Door Assist Handle Strap Door Operating Handle January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Cabin Fire Fighting & Smoke Copyright © The Boeing Company. See title page for details. 9.10.10 D6-30151-TBC (pax) Smoke Barrier The smoke barrier can be used on the ground to prevent smoke migration by covering the stairwell between the main deck and the upper deck. To deploy the smoke barrier: • pull latch release • allows cover to fall free and expose the smoke barrier • insert fingers in barrier loops • pull barrier toward railing Cover Release Latch Smoke Barrier Smoke Barrier Ground use only Ground use only January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Cabin Fire Fighting & Smoke Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 9.10.11 • drape barrier over railing • engage snaps along top of stairwell and railing sides • press flap at bottom of barrier against carpet • ensures good contact between velcro flap and carpet CAUTION: The smoke barrier is for ground use only. Snaps Ground use only January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Cabin Fire Fighting & Smoke Copyright © The Boeing Company. See title page for details. 9.10.12 D6-30151-TBC (pax) Intentionally Blank January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines Chapter 9 Land Evacuation Section 20 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 9.20.1 9.20 Non-Normal Situation Guidelines-Land Evacuation Land Evacuation Overview This section provides flight attendants with recommended guidelines for emergency land evacuation. The flight attendant’s primary responsibility during an evacuation is to direct passenger evacuation at all exits. The goal is to ensure passengers and crew exit the airplane safely in a minimum amount of time. Under abnormal conditions, the airplane might settle in an unusual attitude after landing. The flight crew and flight attendants must be aware of outside conditions which may affect an orderly evacuation. The flight crew will notify the flight attendants of any additional conditions which might impact passenger evacuation. If the exit will not open, or a hazard exists, making the exit unsafe for use, take a position to prevent passengers from exiting. Forcefully inform the passengers that the exit will not be used and why. For example, “DOOR JAMMED” or “NO SLIDE”. Hold passengers in the immediate area until the nearest usable exit can be determined. Once determined, redirect the passengers to that usable exit. Use positive commands in a strong and forceful voice when directing the evacuation, such as: • “EVACUATE” • “RELEASE YOUR SEAT BELTS” • “GET OUT OF YOUR SEATS” • “COME THIS WAY” Note: Redirection means sending passengers past a usable/unusable exit toward a usable exit in order to maintain balanced flow to all usable exits. This will minimize the total evacuation time Flight attendants must monitor the progress of the evacuation and the condition of the slide at their assigned station. Should conditions change such that the safety at an exit is in doubt, discontinue evacuation at that exit and redirect the passengers to alternate doors. Note: It is not possible to cover all conceivable evacuation scenarios with one set of procedures. It is extremely important for flight attendants to assess each emergency situation and exercise their best judgment in how to evacuate the passengers safely in minimum time. January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Land Evacuation Copyright © The Boeing Company. See title page for details. 9.20.2 D6-30151-TBC (pax) Passenger Entry Doors and Upper Deck Doors After slide deployment, verify the slide is safe for use. Position yourself in the dedicated assist space forward or aft of the exit. Do not block the exit. Make physical and/or verbal contact as soon as possible with the passengers approaching the exit. The slides are dual lane. During an emergency it is very important to establish dual lane flow to ensure a timely evacuation. Use the command: “FORM TWO LINES”. Strong, loud, positive commands, such as: • “FORM TWO LINES” • “GO” • “JUMP” • “MOVE”. must be used. Overwing Emergency Exits At the overwing exits, verify the “barber pole” is visible. Position yourself in the aft facing assist space. Do not block the exit. Make physical and/or verbal contact as soon as possible with the passengers approaching the exit. Command the first passengers out of the overwing exit to: • “FORM TWO LINES” Continue to command the passengers at the overwing exits to “FORM TWO LINES” until flow has been established. Once flow to the slide is established, continue to use positive commands, such as: • “GO” • “MOVE”. January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Land Evacuation Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 9.20.3 Emergency Evacuation Guidelines Note: In the following guidelines, “adjacent exit” is defined as the exit forward or aft of the “assigned exit”. “Adjacent exit” is not used to refer to the exit across from the assigned exit. Maintain brace position until the airplane comes to a complete stop. Communicate with the flight deck. If time permits, use the PA to: • brief the passengers (exits, protective positions, and other information, as required) • assign helpers • order the removal of high heels and other restrictive articles
作者:
帅哥
时间:
2008-12-28 03:16:41
3 4 3 5 1 6 January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Land Evacuation Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 9.20.5 All Landing Gear Up Point Description Escape Slide Condition 1 Door 1L & 1R Usable 2 Upper Deck Door L & R Usable 3 Door 2L & 2R Usable 4 Door 3L & 3R Usable 5 Door 4L & 4R Usable 6 Door 5L & 5R Usable 3 4 2 5 1 6 January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Land Evacuation Copyright © The Boeing Company. See title page for details. 9.20.6 D6-30151-TBC (pax) Airplane Tips Tail Down Point Description Escape Slide Condition 1 Door 1L & 1R Not Usable 2 Upper Deck Door L & R Usable 3 Door 2L & 2R Usable 4 Door 3L & 3R Usable 5 Door 4L & 4R Usable 6 Door 5L & 5R Usable 3 4 2 5 1 6 January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Land Evacuation Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 9.20.7 Airplane Tips Nose Down Point Description Escape Slide Condition 1 Door 1L & 1R Usable 2 Upper Deck Door L & R Usable 3 Door 2L & 2R Usable 4 Door 3L & 3R Usable 5 Door 4L & 4R Usable 6 Door 5L & 5R Usable 1 2 3 4 2 5 1 6 January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Land Evacuation Copyright © The Boeing Company. See title page for details. 9.20.8 D6-30151-TBC (pax) Airplane Rolls On One Side
作者:
帅哥
时间:
2008-12-28 03:16:49
Point Description Escape Slide Condition 1 Door 1L & 1R Usable 2 Upper Deck Door L & R Usable 3 Door 2L & 2R Usable 4 Door 3L & 3R Usable 5 Door 4L & 4R Usable 6 Door 5L & 5R Usable Wing Down Configuration (typical) January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Land Evacuation Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 9.20.9 Intentionally Blank January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Land Evacuation Copyright © The Boeing Company. See title page for details. 9.20.10 D6-30151-TBC (pax) If Exit Is Usable • open the exit • pull the manual inflation handle (if required) • command passengers to stand back until the slide/raft or slide is fully deployed • be assertive (forceful) in your commands • Research has proven assertive action by cabin crew can accelerate passenger emergency evacuation rates. (It is extremely important that assertive actions be strongly emphasized in any flight attendant training program.) • assume a protective position in the dedicated assist space • all exits have dedicated assist space(s) forward and/or aft of the exit • Maintain your position in the assist space, keeping the exit path clear to prevent interfering with passenger evacuation. Note: When the assist space is against a vertical surface (such as a partition, lavatory, or galley) keeping your heels and upper back pressed against that surface helps to ensure that you stay clear of the exit path. • command passengers to form two lines and evacuate • dual lane flow of passengers (two passengers side by side) is required for the fastest evacuation. At usable exits, your primary duty is to maintain constant dual lane flow of passengers out that exit • continually assess conditions inside the aircraft and on the slide to ensure passenger flow is maintained • take appropriate action to assist hesitant passengers • do not touch passengers as they exit. If a passenger freezes, have passenger behind buckle balking passenger’s knees or place one hand on shoulder and other hand in small of back and simultaneously push downward and outward. • passengers who sit and delay at the top of the slide rather than jumping will slow the evacuation. Commanding the passenger behind such a “sitter” to push that person out onto the slide can prevent significant delays in an evacuation. • use sharp verbal commands. For hesitant passengers within your reach, push at waist level to move them out through the exit. Do not push at knee or shoulder level January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Land Evacuation Copyright © The Boeing Company. See title page for details.
作者:
帅哥
时间:
2008-12-28 03:16:57
D6-30151-TBC (pax) 9.20.11 • if there are no more passengers approaching your exit and the exit across from you (passenger flow has ceased) take appropriate actions to: • attract additional passengers to come toward your exit; use strong, loud, positive commands or, if necessary • move down the aisle toward an adjacent exit, if conditions permit, to gain the attention of an attendant to initiate the redirection of passengers toward your exit • continue to monitor and protect your exit Note: In mixed class airplane interiors, passenger densities in the forward zone of the cabin are lower than the middle and aft zones. Use of redirection to maintain flow at the forward doors becomes even more important in these airplanes Note: On two-aisle airplanes, if only one exit of any exit pair is unusable, use the aisle on the opposite side of the airplane from the usable exit for redirecting passengers to another exit. This will allow minimum disruption of flow at the usable exit. Total evacuation time is minimized when passengers clear all exits (passenger flow at all exits ceases) at the same time. Only by-pass the passengers that will be able to exit the airplane through an adjacent door sooner that the last passenger exits through the door closest to you. • exit the airplane following the last passenger, using the nearest exit. January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Land Evacuation Copyright © The Boeing Company. See title page for details. 9.20.12 D6-30151-TBC (pax) If Exit Is Not Usable • block the exit to prevent passenger evacuation, while commanding passengers that the exit is blocked • if your exit is not usable you must perform the duties of managing the cabin evacuation by: • first, establish passenger flow away from the unusable exit, and then • direct passenger flow to the usable exit(s) • assess usability of other exits across from and adjacent to yours • visually determine that passenger flow has been established through a usable exit before redirecting passenger flow • direct passengers to the nearest usable exit by issuing appropriate commands and using arms and hands to point passengers in direction of exit • when, in your best judgment, passenger flow is established away from an unusable exit and toward a usable exit, proceed to an appropriate location to best direct or redirect passengers to balance flow to adjacent usable exits • minimizing evacuation time requires maximizing utilization of all usable exits throughout an evacuation. Evacuation time will be minimized when passenger flow to all usable exits ends at the same time • maintain awareness of evacuation progress in adjacent cabin areas and at other usable exits and direct (or redirect) passengers as necessary to help maintain equal flow to each exit January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Land Evacuation Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 9.20.13
作者:
帅哥
时间:
2008-12-28 03:17:05
• if there are no passengers approaching your exit and a usable exit across from you (passenger flow has ceased), take appropriate actions to: • attract additional passengers to come toward the usable exit near you; use strong, loud, positive command, or if necessary, • move down the aisle toward an adjacent exit, if conditions permit, to gain the attention of an attendant to initiate the redirection of passengers toward the usable exit across from you • continue to monitor and protect your exit • in mixed class airplane interiors, passenger densities in the forward zone of the cabin are lower than the middle and aft zones. Use of exit by-pass to maintain flow at the forward doors becomes even more important in these airplanes • if you see no passengers (passenger flow has ceased) at an adjacent usable exit, and significant numbers of passengers remain in your exit area, redirect passengers toward the usable exit to maintain balanced exit utilization • when using exit redirection, avoid disrupting passenger flow to the usable exit near you. Redirect passengers singly or in small groups to maintain balanced flows Note: On two-aisle airplanes, if only one exit of any exit pair is unusable, use the aisle on the opposite side of the airplane from the usable exit for redirecting passengers to another exit. This will allow minimum disruption of flow at the usable exit. Total evacuation time is minimized when passengers clear all exits (passenger flow at all exits ceases) at the same time. Only by-pass the passengers that will be able to exit the airplane through an adjacent door sooner than the last passenger exits through the door closest to you. January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Land Evacuation Copyright © The Boeing Company. See title page for details. 9.20.14 D6-30151-TBC (pax)
作者:
帅哥
时间:
2008-12-28 03:17:13
Flight Attendants Not Assigned To An Exit The responsibility of flight attendants not assigned to an exit is to assess conditions and then assist in evacuating the passengers. • in mixed class configurations, the forward exits could be under-utilized due to a lower passenger density in the forward zones • assist in minimizing evacuation time by ensuring there is a continuous passenger flow through all exits • continue to evaluate the situation, redirecting passengers to under-utilized exits which may change as the evacuation progresses January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines Chapter 9 Ditching Section 30 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 9.30.1 9.30 Non-Normal Situation Guidelines-Ditching [Options shown - ARM/DISARM, Option: AUTOMATIC/MANUAL, FLIGHT/PARK; Option shown: Life raft not installed] Ditching Overview This section provides some guidelines for the safe evacuation of passengers and crew in the event of a water landing. It also contains procedures for slide interchangeability. Ditching is an emergency landing on water. Complete knowledge of procedures and equipment is necessary. All loose objects must be secured. The passengers and crew must be safely belted into seats prior to impact. With few exceptions, ditching procedures are similar to those used in land evacuation. Communication with the flight deck is required to ensure that the cabin is prepared in a timely manner. The passenger briefing should be amended to suit the situation. Passengers are instructed to put on life vests and follow inflation instructions. Life vests are stored under each passenger seat and spare vests are located throughout the cabin. Ditching studies for the 747-400 series airplanes indicate that, with an optimum center of gravity and normal gross weight, the airplane should come to rest slightly nose high in the water. The forward doors should be approximately 5 feet (1.5 meters) above the water and the aft doors should be over two feet and one half above the water. Additional studies involving high gross weight ditching situations, such as those encountered during or soon after takeoff, indicate that the aft doors may be very near or below the water level. This condition could cause malfunction or damage to the slide/rafts and allow water to enter the airplane. WARNING: Before opening the door, verify that the actual water level is below the door sill. If the door is unusable, the slide/raft may be re-positioned at another door and manually deployed. WARNING: Door 3 is not to be used as a primary exit during ditching operations. Deployment of both the door 3 ramp/slide and the door 4 slide/raft on the same side of the aircraft will cause interference with the normal operation of the door 4 slide/raft and the door 4 slide/raft may then be unusable. January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Ditching Copyright © The Boeing Company. See title page for details. 9.30.2 D6-30151-TBC (pax) Ditching Guidelines Communicate with the flight deck. Brief the passengers on the evacuation/ditching. If time permits, use the PA to: • brief the passengers (exits, protective positions, and other information, as required) • direct passengers to put on life vests • assign helpers • establish evacuation zones • order the removal of high heels and other restrictive articles. Maintain brace position until airplane comes to a complete stop.
作者:
帅哥
时间:
2008-12-28 03:17:22
Initiate Ditching Evacuation Passenger Entry Door • move to assigned stations • assess safety of inside and outside conditions • slide/raft automatically deploys and inflates • verify slide/raft is safe for use • shout evacuation and loading commands • direct passengers away from unusable exits. January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Ditching Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 9.30.3 Overwing Exit WARNING: Door 3 ramp/slides are not usable as life rafts and should not be deployed during a ditching situation. Deployment of both the door 3 ramp/slide and the door 4 slide/raft on the same side of the airplane will cause interference with normal operation of the door 4 slide/raft. The door 4 slide/raft may then be unusable. If door 3 is used during ditching, the door mode selector lever must be in MANUAL to allow the door to be opened without deploying the ramp/slide. • move to assigned stations • assess safety of inside and outside conditions • move the mode select lever to MANUAL WARNING: The Mode Select Lever must be placed in the MANUAL position to prevent the deployment of the overwing slide. • open the door January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Ditching Copyright © The Boeing Company. See title page for details. 9.30.4 D6-30151-TBC (pax) • remove escape strap from stowage bin end cap access in forward part of door Escape strap Overwing Exit Door 3L (typical) January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Ditching Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 9.30.5 • attach escape strap to hook on leading edge of wing between engines • direct passengers on to wing using escape strap as necessary • shout evacuation and loading commands to direct passengers to closest slide/raft where space is available. Upper Deck Doors WARNING: Do not open the upper deck doors; the upper deck slides cannot be used as rafts. The upper deck exit doors should not be used during ditching operations. Redirect the passengers down the stairs to the main deck exits. Escape strap attachment point January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Ditching Copyright © The Boeing Company. See title page for details. 9.30.6 D6-30151-TBC (pax) Board Passengers Into The Passenger Entry Door Slide/Raft • direct balanced loading of available rafts • keep weight distribution even; direct passengers to the less used slide/raft side or to alternate sides • instruct the passengers to stay low and sit back against inflated tubes Once all passengers have boarded • check the airplane for additional passengers • evacuate into the slide/raft. Note: If the slide/raft is under inflated or has small leaks, additional inflation or repair should not be attempted until the slide/raft is detached from the airplane. January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Ditching Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 9.30.7 Detach The Slide/Raft From The Door Sill Note: Do not detach the slide/raft from the airplane until all the passengers have been boarded • pull the door strap release handle • releases pack board from slide/raft • pull up the fabric flap over the slide/raft detachment handle • pull the slide/raft detachment handle • causes the top of the slide/raft to fall free of airplane • cut the mooring line. Note: The slide/raft remains attached to the airplane by a mooring line (approximately 12 feet (3.7 meters) long). The mooring line can be detached by pulling the mooring line handle or cutting with a knife. The mooring line will break if the airplane sinks. Note: Typical passenger entry door interior, looking out TO RELEASE SLIDE/RAFT RAISE FLAP & PULL HANDLE STEP 2 PULL DOOR STRAP HANDLE STEP 1 January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Ditching Copyright © The Boeing Company. See title page for details. 9.30.8 D6-30151-TBC (pax)
作者:
帅哥
时间:
2008-12-28 03:17:32
Slide/Raft Portability Under ditching conditions, flight attendants must assess outside conditions prior to opening a door. Sea state conditions may preclude deploying a slide/raft at the door on which it is installed. A slide/raft may be moved from its door position to another passenger entry door for deployment. Note: The slide/raft assembly may not be deployed at door 3L or 3R. Slide/Raft Portability Procedures The following provides instructions for portability of the slide/raft during ditching operations when the slide/raft is removed from an unusable door for use at another exit. Remove slide/raft bustle • Lift and pull the slide/raft cover at top and bottom. • Remove survival kit. 1 January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Ditching Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 9.30.9 Mode Select Lever • Place the lever in the AUTOMATIC position. Partially open the door • Rotate door operating handle 45 degrees. 2 3 January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Ditching Copyright © The Boeing Company. See title page for details. 9.30.10 D6-30151-TBC (pax) Remove Slide/Raft from Door • Press retainer springs on girt bar ends, move the slider blocks toward center, and lift girt bar free. • Locate L-bar loop on top of slide/raft package. • While supporting slide/raft against door, pull L-bar loop to reveal L-bar lever. • Rotate lever inward horizontally until slide/raft disengages from door. • Support slide/raft at both ends and allow it to pivot away from door as it disconnects. 4 5 January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Ditching Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 9.30.11 Prepare the usable door • Ensure the usable door is latched open. • Press retainer springs on girt bar ends, move the slider blocks toward center, and lift girt bar free. Note: Check mooring line secured to girt bar before the girt bar is engaged in the floor fitting, • Align the girt bar with the floor fittings and engage the slider blocks. Carry the slide/raft pack and sliders to the alternative door • With the slide/raft lying soft side down, place the girt bar, sliders and survival kit on top of the pack. CAUTION: Do not pull red inflation loop. Do not drop girt bar or snag it on seat during transfer. Slide may deploy and inflate. • Position 1 person on each side of the pack. • Carefully transfer the slide/raft, girt bar, sliders and survival kit to the door and position it soft side down on the floor beside the door. 6 7 January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Ditching Copyright © The Boeing Company. See title page for details. 9.30.12 D6-30151-TBC (pax) • Pull the packboard slide/raft release handle • Pull the ditching release handle • Pull the mooring line release handle. Deploy the slide • Rotate/push the slide/raft pack squarely out through the door. 8 9 January 15, 2004 747-400 Flight Attendant Manual Miscellaneous Chapter 10 Table of Contents Section 0 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 10.TOC.0.1 10.0 Miscellaneous-Table of Contents Portable Electronic Devices . . . . . . . . . . . . . . . . . . . . . . . . . 10.10.1 Approved Electronic Devices . . . . . . . . . . . . . . . . . . . . . 10.10.1 Non-Approved Electronic Devices . . . . . . . . . . . . . . . . . 10.10.2
作者:
帅哥
时间:
2008-12-28 03:17:43
0.0 Preface -Title Page Initiate Evacuation • ensure the airplane has stopped and the engines are shutdown • activate the emergency evacuation signal (if required) • move to assigned stations • assess safety of inside and outside conditions January 15, 2004 747-400 Flight Attendant Manual Non-Normal Situation Guidelines - Land Evacuation Copyright © The Boeing Company. See title page for details. 9.20.4 D6-30151-TBC (pax) Escape Slide Usability All Landing Gear Down Point Description Escape Slide Condition 1 Door 1L & 1R Usable 2 Upper Deck Door L & R Usable 3 Door 2L & 2R Usable 4 Door 3L & 3R Usable 5 Door 4L & 4R Usable 6 Door 5L & 5 R Usable January 15, 2004 747-400 Flight Attendant Manual Copyright © The Boeing Company. See title page for details. 10.TOC.0.2 D6-30151-TBC (pax) Miscellaneous - Table of Contents Intentionally Blank January 15, 2004 747-400 Flight Attendant Manual Miscellaneous Chapter 10 Portable Electronic Devices Section 10 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 10.10.1 10.10 Miscellaneous-Portable Electronic Devices Portable Electronic Devices Portable electronic devices can cause interference with airplane flight control, navigation and communication systems. Because of this interference, local regulatory agencies may prohibit or limit the use of these devices on airplanes. If the airline allows use of portable electronic devices, procedures must be established to control their use. As a minimum, the airline should provide the following: • Methods to inform passengers of when portable electronic devices may be used. This may be accomplished through the departure briefing, passenger information cards, captain’s announcement, or any other method deemed appropriate by the airline. • Procedures to stop the operation of the portable electronic devices suspected of causing interference with the airplane systems. • Cabin to flight deck coordination and pilot monitoring procedures. • Procedures for determining acceptability of devices that are allowed to be operated. • Procedures for reporting instances of suspected and confirmed interference by portable electronic devices to the local aviation regulatory agency. • Prohibit the operation of portable electronic devices during takeoff and landing phases of flight. • Prohibit the operation of portable electronic devices classified as intentional radiators or transmitters, such as citizens’ band and amateur radios, cellular telephones, and remote control devices. The following is a partial list of approved and non approved electronic devices: Approved Electronic Devices • heart pacemakers • hearing aids • compact disk (CD) players • portable voice recorders • tape cassette players (self-contained) • electric shavers • calculators • portable computers or typewriters (electronic or mechanical) that are briefcase size and able to fit under the passenger seat or in the overhead bins; a mouse cord may be attached to the computer. June 1, 2001 747-400 Flight Attendant Manual Miscellaneous - Portable Electronic Devices Copyright © The Boeing Company. See title page for details. 10.10.2 D6-30151-TBC (pax) Non-Approved Electronic Devices • portable telephones, such as cellular, etc., except those installed by the airline • radios: AM, FM, VHF (battery or cord operated) • TV sets, video players, TV cameras, TV camcorders (battery or cord operated) • electronic games, except those installed by the airline • toys with remote controls • computers or typewriters larger than a briefcase that cannot be stored under the seat or in an overhead bin • data entry pad (a device with a numeric keyboard, hand-held with umbilical cord attachment; a mouse attached to a computer is not a data entry pad). June 1, 2001 747-400 Flight Attendant Manual Crew Rest Chapter 11 Table of Contents Section 0 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 11.TOC.0.1 11.0 Crew Rest-Table of Contents Overview . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11.10.1 Door 5 Overhead Crew Rest Layout . . . . . . . . . . . . . . . . . . 11.10.2 Entrance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11.10.2 Bunks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11.10.3 Passenger Service Unit (PSU) . . . . . . . . . . . . . . . . . . . . . 11.10.5 Temperature Control Panel . . . . . . . . . . . . . . . . . . . . . . . 11.10.7 Oxygen System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11.10.8 Emergency Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . 11.10.8 Door 5 Overhead Crew Rest Fire Protection . . . . . . . . . . . . 11.10.9 Smoke Detection System . . . . . . . . . . . . . . . . . . . . . . . . . 11.10.9 Smoke Detection Panel . . . . . . . . . . . . . . . . . . . . . . . . . 11.10.10 Decompression . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11.20.1 Cruising Altitude . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11.20.1 Airplane Level Off . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11.20.1 Firefighting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11.20.2 If smoke is detected in the Door 5 Overhead Crew Rest, and it is occupied . . . . . . . . . . . . . . . . . . . . . 11.20.2 If the fire can be immediately extinguished . . . . . . . . . . 11.20.2 After smoke has cleared . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11.20.2 Evacuation Using Emergency Hatch . . . . . . . . . . . . . . . . . . 11.20.3 Evacuating an Incapacitated Person . . . . . . . . . . . . . . . . . . . 11.20.8 Main Stairway Evacuation . . . . . . . . . . . . . . . . . . . . . . . . 11.20.8 Emergency Hatch Evacuation . . . . . . . . . . . . . . . . . . . . 11.20.10 Decompression . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11.30.1 Cruising Altitude . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11.30.1 Airplane Level Off . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11.30.1 Firefighting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11.30.2 If smoke is detected in the Door 5 Overhead Crew Rest, and it is occupied . . . . . . . . . . . . . . . . . . . . . 11.30.2 If the fire can be immediately extinguished . . . . . . . . . . 11.30.2 After smoke has cleared . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11.30.2 Evacuation Using Emergency Hatch . . . . . . . . . . . . . . . . . . 11.30.3 January 15, 2004 747-400 Flight Attendant Manual Copyright © The Boeing Company. See title page for details. 11.TOC.0.2 D6-30151-TBC (pax) Crew Rest - Table of Contents Evacuating an Incapacitated Person . . . . . . . . . . . . . . . . . . . 11.30.8 Main Stairway Evacuation . . . . . . . . . . . . . . . . . . . . . . . . 11.30.8 Emergency Hatch Evacuation . . . . . . . . . . . . . . . . . . . . 11.30.10 January 15, 2004 747-400 Flight Attendant Manual Crew Rest Chapter 11 Introduction Section 10 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 11.10.1 11.10 Crew Rest-Introduction [Options shown - Passenger only: Door 5 overhead crew rest installed, 8 bunks, 2 seats; Option: 6 bunks, 10 bunks] Overview This chapter provides information on the Door 5R Overhead Crew Rest compartment installed in the cabin overhead above door 5. Crew members occupying the crew rest compartment must be trained in the use of evacuation routes in accordance with FAA approved evacuation procedures contained in Boeing document D926U303, Appendix D. January 15, 2004 747-400 Flight Attendant Manual Crew Rest - Introduction Copyright © The Boeing Company. See title page for details. 11.10.2 D6-30151-TBC (pax) Door 5 Overhead Crew Rest Layout Entrance Entry into the overhead crew rest is through an entrance enclosure located in the passenger cabin, aft of door 5R. The entrance to the overhead crew rest compartment has the same external appearance as a lavatory, but is placarded “CREW ONLY”. The door should remain closed at all times. CREW ONLY June 1, 2001 747-400 Flight Attendant Manual Crew Rest - Introduction Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 11.10.3 Bunks The door 5 overhead crew rest area contains the following: • bunks (circled numbers 1 through 8) 1 2 3 4 5 6 8 7 January 15, 2004 747-400 Flight Attendant Manual Crew Rest - Introduction Copyright © The Boeing Company. See title page for details. 11.10.4 D6-30151-TBC (pax) • handset • light switches • emergency hatch • bunk service unit at each bunk • temperature control panel • smoke detection panel • emergency equipment. Note: An emergency escape hatch is located on the floor on the left side of the compartment, under bunk number 4. See Chapter 11, Crew Rest, Section 11.20, Non-Normal Situation Guidelines for detailed information. Handset/Light Switches Temperature Control Panel Smoke Detection Panel Emergency Equipment January 15, 2004 747-400 Flight Attendant Manual Crew Rest - Introduction Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 11.10.5 Passenger Service Unit (PSU) Door 5 Crew Rest Seat Passenger Service Unit (PSU) Light Smoke Seat Belt / No Gasper Oxygen Mask Air Vent Sniffer Smoking Sign Reading Bunk (typical) January 15, 2004 747-400 Flight Attendant Manual Crew Rest - Introduction Copyright © The Boeing Company. See title page for details. 11.10.6 D6-30151-TBC (pax) The typical bunk in the crew rest area contains the following: • seat belt / no smoking sign • smoke sniffer port • reading light • oxygen mask • gasper air vent. January 15, 2004 747-400 Flight Attendant Manual Crew Rest - Introduction Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 11.10.7 Temperature Control Panel 1 Temperature Selector Rotate - selects temperature for overhead crew rest. Temperature range is 65 degrees F to 85 degrees F (18 degrees C to 29 degrees C). 2 Temperature Indicator Indicates temperature in degrees F (C). 3 FAN RESET Switch Push - restarts overhead crew rest fans after smoke has been cleared. COOLER WARMER NORMAL TEMPERATURE CONTROL 1 2 3 January 15, 2004 747-400 Flight Attendant Manual Crew Rest - Introduction Copyright © The Boeing Company. See title page for details. 11.10.8 D6-30151-TBC (pax) Oxygen System The oxygen masks in the PSU will drop automatically in the event of a decompression. They can also be manually opened by inserting a hair pin or thin rod into the hole of the compartment cover. There are 8 Portable Oxygen Bottles (POB) with masks installed in the crew rest area and are located at the foot of each bunk. The 4.25 cubic foot POBs will provide approximately 30 minutes of oxygen. There are 2 oxygen masks located in the PSU above the seats. Note: Use the low flow setting on the portable oxygen bottles. Emergency Equipment Emergency equipment is installed inside the door 5 crew rest compartment at the top of the stairs. It includes: • halon fire extinguisher • water fire extinguisher • portable breathing equipment (PBE) • flashlight. Additionally, each bunk has a portable oxygen bottle (POB). January 15, 2004 747-400 Flight Attendant Manual Crew Rest - Introduction Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 11.10.9 Door 5 Overhead Crew Rest Fire Protection Smoke Detection System Two smoke detectors are installed in the overhead crew rest area with 14 smoke sniffer ports in the door 5 crew rest area, including 4 in the common area. Additionally, there are two smoke detectors in the ceiling. If smoke is detected in the crew rest area, the smoke detection warning panel inside the compartment will illuminate red and an intermittent horn will sound. The FIRE and EVAC lights illuminate on the smoke detection panel and a horn sounds in the entrance enclosure. On the flight deck, an aural caution alarm sounds and a SMOKE DR5 REST message is displayed. January 15, 2004 747-400 Flight Attendant Manual Crew Rest - Introduction Copyright © The Boeing Company. See title page for details. 11.10.10 D6-30151-TBC (pax) Smoke Detection Panel 1 Door 5 Zone Smoke Detector (DETR A/B) Indicator Light Illuminated (white) - smoke detected by zone smoke detector. Note: Smoke detected in the overhead crew rest area causes an EICAS message to be displayed on the flight deck. Push - • tests individual smoke detector zone • illuminates respective zone smoke detector indicator light. 2 HORN Cancel (CNCL) Push - silences alarm horn. 3 Smoke Detection Alarm Horn 4 Light (LT) TEST Switch Push - illuminates smoke detector lights. ZONE 2 ZONE 1 (PUSH TO TEST) SMOKE DETECTION LT TEST HORN CNCL DETR B DETR A DETR B DETR A (PUSH TO TEST) SMOKE DOOR 5 SMOKE DOOR 5 SMOKE DOOR 5 DOOR 5 SMOKE 2 4 1 3 January 15, 2004 747-400 Flight Attendant Manual Crew Rest Chapter 11 Non-Normal Situation Guidelines Section 20 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 11.20.1 11.20 Crew Rest-Non-Normal Situation Guidelines [Options shown - Passenger only: Door 5 overhead crew rest installed, 8 bunks, 2 seats; Option: 10 bunks] Decompression Cruising Altitude If a cabin decompression occurs during cruise, the oxygen masks located in the bunk service units will automatically deploy when the cabin altitude is above 13,500 feet. Oxygen flow is available when the mask is pulled. Crew rest occupants should immediately don the bunk service unit oxygen mask. Airplane Level Off When notified that the airplane has leveled off: • detach the portable oxygen bottle (POB) located at the foot of the bunk • verify oxygen quantity sufficient • remove the mask from the plastic bag • open the dust cover and attach the mask to the outflow valve • rotate the ON/OFF valve fully counter-clockwise After ensuring that oxygen is flowing from the POB, the flight attendant should remove the bunk service unit oxygen mask and don the POB. Note: The POB will provide oxygen for approximately 30 minutes. Evacuate the door 5 crew rest area when directed. CAUTION: When exiting the crew rest compartment, use the safety strap when transporting the POB to prevent damage to the POB. January 15, 2004 747-400 Flight Attendant Manual Crew Rest - Non-Normal Situation Guidelines Copyright © The Boeing Company. See title page for details. 11.20.2 D6-30151-TBC (pax) Firefighting If smoke is detected in the Door 5 Overhead Crew Rest, and it is occupied • find the source of the smoke/fire • establish communications with the flight deck • request help from crew members If the fire can be immediately extinguished • one attendant puts on the smoke hood and fights the fire • crew members not fighting the fire are to evacuate the crew rest compartment • an attendant not involved in fighting the fire, silences the smoke alarm horn by pushing the HORN CNCL switch on the smoke detection panel at the top of the stair • continue to monitor the overhead crew rest compartment After smoke has cleared • at flight crew direction, push fan reset switch on bottom of temperature control panel CAUTION: If the fire is extinguished and smoke has cleared, reset the temperature control panel when directed by the flight crew. January 15, 2004 747-400 Flight Attendant Manual Crew Rest - Non-Normal Situation Guidelines Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 11.20.3 Evacuation Using Emergency Hatch An emergency escape hatch is located on the floor on the left side of the crew rest area, under bunk number 4. Emergency Escape Hatch (under bunk 4) 4 June 1, 2001 747-400 Flight Attendant Manual Crew Rest - Non-Normal Situation Guidelines Copyright © The Boeing Company. See title page for details. 11.20.4 D6-30151-TBC (pax) If the main stair is unusable, evacuation through the emergency hatch is possible. Bunk Cushion Bunk Panel Escape Hatch Placard ESCAPE HATCH Remove Upper and Lower Mattresses Unlatch and Remove Upper Bunk Panel Open and Latch Escape Hatch Kick Down on Ceiling Panel Sit Facing Outboard Grab Handholds Swing Down to Main Deck June 1, 2001 747-400 Flight Attendant Manual Crew Rest - Non-Normal Situation Guidelines Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 11.20.5 To use the escape hatch: • remove the upper and lower bunk mattresses • remove upper bunk panel • open escape hatch and latch open Bunk Panel Release Latch Escape Hatch Latch June 1, 2001 747-400 Flight Attendant Manual Crew Rest - Non-Normal Situation Guidelines Copyright © The Boeing Company. See title page for details. 11.20.6 D6-30151-TBC (pax) • sit on floor with both legs in hatch • kick down on ceiling panel • sit on floor facing outboard • lower legs into hatch opening • reach out and grab the outboard handholds • keep elbows close to sides • swing down to main deck FWD June 1, 2001 747-400 Flight Attendant Manual Crew Rest - Non-Normal Situation Guidelines Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 11.20.7 Intentionally Blank June 1, 2001 747-400 Flight Attendant Manual Crew Rest - Non-Normal Situation Guidelines Copyright © The Boeing Company. See title page for details. 11.20.8 D6-30151-TBC (pax) Evacuating an Incapacitated Person Main Stairway Evacuation Place the incapacitated person on the floor, face up, with feet near the top of the stairs. With one assistant located on the top landing to handle the incapacitated person's feet, and the other in the crew rest placing hands under the incapacitated person's shoulders, move the incapacitated person so most of his legs are down the stairs. With the incapacitated person sitting on the edge at the top of stairs, • the upper assistant should: • The lower assistant shall work the feet around into the lower stairway and then take as much weight as possible. The upper assistant, without supporting much of the incapacitated person's weight, should lean outboard until the head contacts the outboard ceiling/wall. June 1, 2001 747-400 Flight Attendant Manual Crew Rest - Non-Normal Situation Guidelines Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 11.20.9 • the lower assistant should: • work the feet around into the lower stairway and then take as much weight as possible • the upper assistant should: • lean outboard until the head contacts the outboard ceiling/wall Note: Do not support much of the incapacitated person's weight • transfer grip to the back of the jacket or shirt (or under the shoulders) of the incapacitated person (without moving the incapacitated person) and proceed down the stairs to the top of the landing. With the upper assistant grasping the back of the jacket or shirt (or under the shoulders) with both hands and the lower assistant grasping about the knees, carry the incapacitated person down and out of the stairway. June 1, 2001 747-400 Flight Attendant Manual Crew Rest - Non-Normal Situation Guidelines Copyright © The Boeing Company. See title page for details. 11.20.10 D6-30151-TBC (pax) Emergency Hatch Evacuation Place the incapacitated person on the floor face up with feet adjacent to the hatch. One assistant should open the hatch and evacuate to the main deck using the previously described procedure. The assistant remaining in the crew rest should: • place the incapacitated person's feet over the hatch • then move to a position behind the incapacitated person and raise the incapacitated person to a sitting position • place hands under the incapacitated person's shoulders • slide the incapacitated person until the majority of the legs are through the hatch. • transfer hold of the incapacitated person from under the shoulders to the wrists • lower the incapacitated person down through the hatch June 1, 2001 747-400 Flight Attendant Manual Crew Rest - Non-Normal Situation Guidelines Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 11.20.11 The assistant on the main deck shall: • receive the incapacitated person • lower him/her to the floor while protecting the head and neck June 1, 2001 747-400 Flight Attendant Manual Crew Rest - Non-Normal Situation Guidelines Copyright © The Boeing Company. See title page for details. 11.20.12 D6-30151-TBC (pax) Intentionally Blank June 1, 2001 747-400 Flight Attendant Manual Crew Rest Chapter 11 Non-Normal Situation Guidelines Section 30 Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 11.30.1 11.30 Crew Rest-Non-Normal Situation Guidelines [Options shown - Passenger only: Door 5 overhead crew rest installed, 8 bunks, 2 seats; Option: 10 bunks] Decompression Cruising Altitude If a cabin decompression occurs during cruise, the oxygen masks located in the bunk service units will automatically deploy when the cabin altitude is above 13,500 feet. Oxygen flow is available when the mask is pulled. Crew rest occupants should immediately don the bunk service unit oxygen mask. Airplane Level Off When notified that the airplane has leveled off: • detach the portable oxygen bottle (POB) located at the foot of the bunk • verify oxygen quantity sufficient • remove the mask from the plastic bag • open the dust cover and attach the mask to the outflow valve • rotate the ON/OFF valve fully counter-clockwise After ensuring that oxygen is flowing from the POB, the flight attendant should remove the bunk service unit oxygen mask and don the POB. Note: The POB will provide oxygen for approximately 30 minutes. Evacuate the door 5 crew rest area when directed. CAUTION: When exiting the crew rest compartment, use the safety strap when transporting the POB to prevent damage to the POB. January 15, 2004 747-400 Flight Attendant Manual Crew Rest - Non-Normal Situation Guidelines Copyright © The Boeing Company. See title page for details. 11.30.2 D6-30151-TBC (pax) Firefighting If smoke is detected in the Door 5 Overhead Crew Rest, and it is occupied • find the source of the smoke/fire • establish communications with the flight deck • request help from crew members If the fire can be immediately extinguished • one attendant puts on the smoke hood and fights the fire • crew members not fighting the fire are to evacuate the crew rest compartment • an attendant not involved in fighting the fire, silences the smoke alarm horn by pushing the HORN CNCL switch on the smoke detection panel at the top of the stair • continue to monitor the overhead crew rest compartment After smoke has cleared • at flight crew direction, push fan reset switch on bottom of temperature control panel CAUTION: If the fire is extinguished and smoke has cleared, reset the temperature control panel when directed by the flight crew. January 15, 2004 747-400 Flight Attendant Manual Crew Rest - Non-Normal Situation Guidelines Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 11.30.3 Evacuation Using Emergency Hatch An emergency escape hatch is located on the floor on the left side of the crew rest area, under bunk number 4. 4 Emergency Escape Hatch (under bunk 4) January 15, 2004 747-400 Flight Attendant Manual Crew Rest - Non-Normal Situation Guidelines Copyright © The Boeing Company. See title page for details. 11.30.4 D6-30151-TBC (pax) If the main stair is unusable, evacuation through the emergency hatch is possible. Escape Hatch Placard Bunk Panel Bunk Cusion ESCAPE HATCH Remove Upper and Lower Mattresses Unlatch and Remove Upper Bunk Panel Open and Latch Escape Hatch Kick Down on Ceiling Panel Sit Facing Outboard Grab Handholds Swing Down to Main Deck January 15, 2004 747-400 Flight Attendant Manual Crew Rest - Non-Normal Situation Guidelines Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 11.30.5 To use the escape hatch: • remove the upper and lower bunk mattresses • remove upper bunk panel • open escape hatch and latch open Bunk Panel Release Latch Escape Hatch Latch January 15, 2004 747-400 Flight Attendant Manual Crew Rest - Non-Normal Situation Guidelines Copyright © The Boeing Company. See title page for details. 11.30.6 D6-30151-TBC (pax) • sit on floor with both legs in hatch • kick down on ceiling panel • sit on floor facing outboard • lower legs into hatch opening • reach out and grab the outboard handholds • keep elbows close to sides • swing down to main deck FWD January 15, 2004 747-400 Flight Attendant Manual Crew Rest - Non-Normal Situation Guidelines Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 11.30.7 Intentionally Blank January 15, 2004 747-400 Flight Attendant Manual Crew Rest - Non-Normal Situation Guidelines Copyright © The Boeing Company. See title page for details. 11.30.8 D6-30151-TBC (pax) Evacuating an Incapacitated Person Main Stairway Evacuation Place the incapacitated person on the floor, face up, with feet near the top of the stairs. With one assistant located on the top landing to handle the incapacitated person's feet, and the other in the crew rest placing hands under the incapacitated person's shoulders, move the incapacitated person so most of his legs are down the stairs. With the incapacitated person sitting on the edge at the top of stairs, • the upper assistant should: • The lower assistant shall work the feet around into the lower stairway and then take as much weight as possible. The upper assistant, without supporting much of the incapacitated person's weight, should lean outboard until the head contacts the outboard ceiling/wall. January 15, 2004 747-400 Flight Attendant Manual Crew Rest - Non-Normal Situation Guidelines Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 11.30.9 • the lower assistant should: • work the feet around into the lower stairway and then take as much weight as possible • the upper assistant should: • lean outboard until the head contacts the outboard ceiling/wall Note: Do not support much of the incapacitated person's weight • transfer grip to the back of the jacket or shirt (or under the shoulders) of the incapacitated person (without moving the incapacitated person) and proceed down the stairs to the top of the landing. With the upper assistant grasping the back of the jacket or shirt (or under the shoulders) with both hands and the lower assistant grasping about the knees, carry the incapacitated person down and out of the stairway. January 15, 2004 747-400 Flight Attendant Manual Crew Rest - Non-Normal Situation Guidelines Copyright © The Boeing Company. See title page for details. 11.30.10 D6-30151-TBC (pax) Emergency Hatch Evacuation Place the incapacitated person on the floor face up with feet adjacent to the hatch. One assistant should open the hatch and evacuate to the main deck using the previously described procedure. The assistant remaining in the crew rest should: • place the incapacitated person's feet over the hatch • then move to a position behind the incapacitated person and raise the incapacitated person to a sitting position • place hands under the incapacitated person's shoulders • slide the incapacitated person until the majority of the legs are through the hatch. • transfer hold of the incapacitated person from under the shoulders to the wrists • lower the incapacitated person down through the hatch January 15, 2004 747-400 Flight Attendant Manual Crew Rest - Non-Normal Situation Guidelines Copyright © The Boeing Company. See title page for details. D6-30151-TBC (pax) 11.30.11 The assistant on the main deck shall: • receive the incapacitated person • lower him/her to the floor while protecting the head and neck January 15, 2004 747-400 Flight Attendant Manual Crew Rest - Non-Normal Situation Guidelines Copyright © The Boeing Company. See title page for details. 11.30.12 D6-30151-TBC (pax) Intentionally Blank January 15, 2004
作者:
joseph
时间:
2010-11-10 20:15:54
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