Flight Attendant Manual 777/200
Copyright © 2000The Boeing Company
All Rights Reserved
Document Number D611W302-TBC (200 GenFam)
January 1, 2000
Revision Number: 03
Revision Date: February 14, 2003
777-200
Flight Attendant Manual
The Boeing Company
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.
Flight Attendant Manual
Preface Chapter 0
Table of Contents Section 0
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 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
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Table of Contents
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0.0.2 D611W302-TBC (200 GenFam)
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Preface Chapter 0
Model Identification Section 1
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 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.
The table permits flight crew correlation of configuration differences by Registry
Number in alpha/numeric order within an operator’s fleet for airplanes covered in
this manual. Configuration data reflects the airplane as delivered configuration.
Airplane number is supplied by the operator. Registry number is supplied by the
national regulatory agency. Serial and tabulation numbers are supplied by Boeing.
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.
Airplane Number Registry Number Serial Number Tabulation
Number
200 77-200 7201 WY201
February 14, 2003
Flight Attendant Manual
Preface -
Model Identification
Copyright © The Boeing Company. See title page for details.
0.1.2 D611W302-TBC (200 GenFam)
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Preface Chapter 0
Introduction Section 3
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 0.3.1
0.3 Preface-Introduction
Foreword
The material in this publication provides introductory information about the
Boeing 777-200 airplane. The information is operationally oriented and is
intended to be used as a reference by a trained flight attendant.
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 777-200 airplane. It is suggested that appropriate sections of the Operations
Manual and Airplane Flight Manual be consulted to supplement the material
contained in this publication.
Note: This manual shall be revised and re-published as necessary.
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.
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Introduction
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0.3.2 D611W302-TBC (200 GenFam)
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Chapter 0
Section 2
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Airplane Description (tab)
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Control Panels (tab)
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Cabin Management System (tab)
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Cabin Management System (cont)
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Lighting (tab)
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Communications (tab)
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Lavatories (tab)
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Galleys (tab)
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Doors, Slides and Emergency Exits (tab)
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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.
D611W302-TBC (200 GenFam) 1.TOC.0.1
1.0 Airplane Description-Table of Contents
Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.1
Overview. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.1
Airplane Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.1
Principal Dimensions - 777-200/777-200ER. . . . . . . . . . . . . . 1.10.2
Airplane Systems General. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.3
Auxiliary Power Unit (APU) . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.3
Airplane Electrical Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.3
Air Conditioning and Pressurization . . . . . . . . . . . . . . . . . . . . 1.10.3
Passenger Cabin . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.3
Cabin Systems Electrical Power . . . . . . . . . . . . . . . . . . . . . . . 1.10.3
Cabin Management System . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.4
Cabin Doors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.4
Galleys . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.4
Lavatories . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.5
Closets and Partitions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.5
Overhead Stowage Bins . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.5
Passenger and Attendant Seating. . . . . . . . . . . . . . . . . . . . . . . 1.10.6
Passenger and Attendant Seating Layout. . . . . . . . . . . . . . . . . 1.10.7
Passenger Service Units . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.8
Emergency Oxygen . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.8
Medical Power Outlets . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.9
Flight Deck Security Door . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.10
Normal Flight Deck Access . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.10.11
Flight Deck Emergency Access Panel . . . . . . . . . . . . . . . . . . 1.10.12
Non-Normal Operations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.20.1
Passenger Cabin Non-Normals . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.20.1
Overhead Stowage Bin Will Not Open . . . . . . . . . . . . . . . . . . 1.20.1
Passenger Overhead Stowage Bin Will Not Open. . . . . . . . . . 1.20.2
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1.TOC.0.2 D611W302-TBC (200 GenFam)
Airplane Description -
Table of Contents
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Flight Attendant Manual
Airplane Description Chapter 1
Introduction Section 10
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 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
Airplane model: 777-200
Engines: General Electric GE90–76B, rated at
76,400 pounds of thrust each.
Pratt & Whitney PW4077, rated at 77,200
pounds of thrust each.
Rolls Royce Trent 875, rated at 73,400
pounds of thrust each.
Maximum takeoff weight: 445,000 pounds
Maximum takeoff weight: 201,848 kilograms
Maximum takeoff weight: 545,000 pounds (247,207 kilograms)
Crew: Captain
First Officer
Passenger seating capacity (typical): 281 total:
18 first class
70 business class
193 economy class
Fuel capacity: 31,000 gallons (117,300 liters)
Maximum operating altitude: 43,100 feet
Maximum operating speed: 330 knots (0.87 Mach)
Range: 4,000 to 5,000 nautical miles
4,600 to 5,800 statute miles (7,400 to 9,300
kilometers)
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Flight Attendant Manual
Airplane Description -
Introduction
Copyright © The Boeing Company. See title page for details.
1.10.2 D611W302-TBC (200 GenFam)
Principal Dimensions - 777-200/777-200ER
199 feet 11 inches
70 feet
36 feet
205 feet 10 inches
60 feet 6 inches
84 feet 11 inches
(60.9 meters)
(21.3 meters)
(11 meters)
(62.7 meters)
(18.4 meters)
(25.9 meters)
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Flight Attendant Manual
Airplane Description -
Introduction
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 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 bleed 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 bleed air system at or below 22,000 feet.
Airplane Electrical Power
The electrical power system supplies 115 volt 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, bleed 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. Flight attendants control
cabin temperature through the cabin management system (CMS). The cabin
management system is also used to adjust the selected temperatures for each
passenger zone.
The cabin pressure is controlled automatically to provide a programmed cabin
altitude.
Passenger Cabin
Cabin Systems Electrical Power
Electrical power to the cabin Inflight Entertainment Equipment (IFE) and galley
power systems is primarily controlled from the flight deck. Additional control of
the IFE system is available to the cabin crew through the IFE Master Power switch
located in the Video Control Center (VCC). Galley power may be turned off by
moving the appropriate galley Emergency Power switch to the OFF position.
IFE and Passenger Seats Power Control
Electrical power to the IFE and passenger seats may be controlled by the
IFE/passenger seats power switch on the flight deck electrical panel or the IFE
power switch in the VCC. With the switch ON, the IFE and all passenger seat and
related systems are powered normally.
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Airplane Description -
Introduction
Copyright © The Boeing Company. See title page for details.
1.10.4 D611W302-TBC (200 GenFam)
Placing the IFE/passenger seats power switch OFF removes power from the
following:
• IFE (all components)
• passenger seats (including seat motor power, personal computer power
outlets, and telephones)
Cabin and Utility Systems Power Control
Electrical power to various cabin and utility systems may be controlled by the
cabin/utility power switch on the flight deck electrical panel. With the switch ON,
the ground service system and galleys are powered normally.
Moving the flight deck cabin/utility power switch OFF removes power from items
such as:
• ground service system
• galleys
• fluorescent cabin lighting
Additionally, when the flight deck cabin/utility power switch is selected OFF, the
following cabin lights are turned on:
• night lights, supplemental night lights, and reading lights
• attendant work lights and some galley/crew rest lights
Each galley has a galley emergency power off switch to control the power for that
galley. See Chapter 6, Section 20, Galleys - Non-Normal Operations.
Cabin Management System
The cabin management system is designed to control and monitor many cabin and
passenger functions. Control panels for the cabin management system are located
at designated attendant stations.
See Chapter 2A, Cabin Management System, for detailed information.
Cabin Doors
The passenger cabin is served by four entry doors, numbered 1L, 2l, 3l, and 4L,
located on the left side of the airplane. Service doors, numbered 1R, 2R, 3R, and
4R, are located on the right side of the airplane.
See Chapter 7, Doors, Slides and Emergency Exits, for detailed information.
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.
February 14, 2003
Flight Attendant Manual
Airplane Description -
Introduction
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 1.10.5
Lavatories
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
Closets are installed in the forward half of the airplane. Partitions, lavatories, and
galleys are used to separate class seating. Some partitions have literature pockets.
Overhead Stowage Bins
Door 1 and Door 4 Stowage Bin
There are overhead stowage bins located in the ceiling over doors 1L, 1R, 4L, and
4R.
Passenger Overhead Stowage Bins
Overhead stowage bins over both the outboard and center seats accommodate
blankets, pillows, and carry-on items. Emergency equipment may also be stored
in the bins. Each bin has a placard stating its maximum weight capacity.
February 14, 2003
Flight Attendant Manual
Airplane Description -
Introduction
Copyright © The Boeing Company. See title page for details.
1.10.6 D611W302-TBC (200 GenFam)
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 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. Designated flight attendant direct view seats must be occupied by flight attendants during taxi, takeoff and landing. See the Passenger and Attendant Layout for direct view seat locations.
Flight Attendant Stations
Flight attendant stations are located at each door and include an attendant switch
panel, service unit, attendant work lights, handset, seats, and cabin area control
panels.
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.
February 14, 2003
Flight Attendant Manual
Airplane Description -
Introduction
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 1.10.7
Passenger and Attendant Seating Layout
A•*
A A
A•
A• A•
A•* A•
A•*
A
A•
A
AAA
A = Attendant Seats (15)
• = Handsets (8)
Purser Work Station
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Flight Attendant Manual
Airplane Description -
Introduction
Copyright © The Boeing Company. See title page for details.
1.10.8 D611W302-TBC (200 GenFam)
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. 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. Oxygen is available
for approximately 12 minutes.
Passenger oxygen masks are located in overhead modular compartments. 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.
See Chapter 8, Emergency Equipment System Description, for detailed
information.
February 14, 2003
Flight Attendant Manual
Airplane Description -
Introduction
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 1.10.9 Medical Power Outlets
Six medical power outlets are located in the passenger cabin:
• after the second row of first class seats on the right side of the airplane in
the lower sidewall.
• after the forth row of first class seats on the left side of the airplane in the
lower sidewall.
• in front of the first row of business class seats on the left and right side of
the airplane in the lower sidewall.
• in front of the first row of economy class seats on the left side of the
airplane in the lower sidewall.
• aft of the last row of economy class seats on the right side of the airplane
in the lower sidewall.
The outlets are covered with a plug similar to the plugs in the existing cabin
service outlets. Power to the outlets is controlled by switches on the flight deck.
February 14, 2003
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Airplane Description -
Introduction
Copyright © The Boeing Company. See title page for details.
1.10.10 D611W302-TBC (200 GenFam)
Flight Deck Security Door
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.
February 14, 2003
Flight Attendant Manual
Airplane Description -
Introduction
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 1.10.11
1 Decompression Blow Out Panel
2 Flight Deck Emergency Access Panel
3 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.
4 Door Handle
Normal Flight Deck Access
Access to the flight deck is by permission of the flight crew.
FWD
1 2
5
3 4
ENT
1
2
3
4
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Introduction
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1.10.12 D611W302-TBC (200 GenFam)
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.
February 14, 2003
Flight Attendant Manual
Airplane Description -
Introduction
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 1.10.13
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
February 14, 2003
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Airplane Description -
Introduction
Copyright © The Boeing Company. See title page for details.
1.10.14 D611W302-TBC (200 GenFam)
Normal Operation
If emergency access to the flight deck is required, entry of the correct emergency
access 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.
February 14, 2003
Flight Attendant Manual
Airplane Description Chapter 1
Non-Normal Operations Section 20
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 1.20.1
1.20 Airplane Description-Non-Normal Operations
Passenger Cabin Non-Normals
Overhead Stowage Bin Will Not Open
If the handle jams and the stowbox cannot be opened:
• remove the plugs located in the lower left and lower right corners of the
stowbox (removing the plugs gains access to the emergency release
levers)
• apply pressure to hold the stowbox in position so that it doesn’t drop open
quickly possibly causing injury
• using a finger or a pencil, push up on both of the emergency release levers
at the same time
• carefully lower the stowage bin.
Emergency
Release
Lever
Plugs
View looking up at stowbox
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Airplane Description -
Non-Normal Operations
Copyright © The Boeing Company. See title page for details.
1.20.2 D611W302-TBC (200 GenFam)
Passenger Overhead Stowage Bin Will Not Open
If a stowage bin cannot be opened using the stowage bin handle:
Note: Usually the stowage bin handle releases one of the two latches. Use the
emergency release lever to release the other latch.
• while pulling on the handle, gently pull down each end of the bin to
determine which end is not releasing
• open the stowage bin adjacent to the end of the stowage bin that is not
being released
• locate the emergency release lever on the end of the stowage bin that will
not release.
February 14, 2003
Flight Attendant Manual
Airplane Description -
Non-Normal Operations
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 1.20.3
• center aisle bin - using your index finger, pull the emergency release lever
up, towards you, while pulling on the bin handle.
• outboard stowage bins - using a name badge, comb, etc., slide it down the
outer edge of the stowbin toward the emergency release lever while
pulling on the bin handle
Center Aisle Bin
Emergency Release Lever
• Pull to open.
Emergency Release Lever
• Pull down to open.
Outboard Bin
February 14, 2003
Flight Attendant Manual
Airplane Description -
Non-Normal Operations
Copyright © The Boeing Company. See title page for details.
1.20.4 D611W302-TBC (200 GenFam)
Intentionally
Blank
February 14, 2003
Flight Attendant Manual
Control Panels Chapter 2
Table of Contents Section 0
FCOM Template 12/12/98
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2.TOC.0.1
2.0 Control Panels-Table of Contents
Attendant Switch Panels . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.10.1
General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.10.1
Attendant Switch Panels (ASP) . . . . . . . . . . . . . . . . . . . . . . . . . . 2.10.1
Door 1 Left . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.10.2
Door 4 Right . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.10.3
Door 2 Left/Right, Door 3 Left/Right, Door 4 Left. . . . . . . . . 2.10.4
Door 1 Center, Door 4 Center . . . . . . . . . . . . . . . . . . . . . . . . . 2.10.5
Passenger Control Unit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.20.1
Passenger Control Unit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.20.1
PCU - All Classes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.20.2
PCU - Crew Rest . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.20.3 February 14, 2003
Flight Attendant Manual
Copyright © The Boeing Company. See title page for details.
2.TOC.0.2 D611W302-TBC (200 GenFam)
Control Panels -
Table of Contents
Intentionally
Blank
February 14, 2003
Flight Attendant Manual
Control Panels Chapter 2
Attendant Switch Panels Section 10
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2.10.1
2.10 Control Panels-Attendant Switch Panels
General
This chapter provides a general description of the various control panels located
throughout the passenger cabin.
The circled numbers adjacent to the panels refer to the chapter where a description
and specific information may be found.
Attendant Switch Panels (ASP)
An attendant switch panel is installed at each attendant station. The attendant
switch panel (ASP) may be used to:
• initiate passenger evacuation
• silence the evacuation horn
• turn on emergency lights
• test emergency lights
• turn work lights on or off
• select the alternate mode for Passenger Address announcements if the
normal mode fails
• select the alternate mode for Cabin Interphone operations if the normal
mode fails.
February 14, 2003
Flight Attendant Manual
Control Panels -
Attendant Switch Panels
Copyright © The Boeing Company. See title page for details.
2.10.2 D611W302-TBC (200 GenFam)
Door 1 Left
4 3 3 8
ACC JACK SERVICE LIGHTS/TST LIGHTS
GROUND EMER EMER
NORM/ALT NORM/ALT LIGHT 2 LIGHT 1
CI PA WORK WORK
SHUT OFF COMMAND
HORN EVAC
Maintenance
use only.
Maintenance
use only.
EVAC
INOP
February 14, 2003
Flight Attendant Manual
Control Panels -
Attendant Switch Panels
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2.10.3
Door 4 Right
3 8 3
LIGHTS/TST
EMER
LIGHT 2 LIGHT 1
WORK WORK
EVAC
SHUT OFF COMMAND
HORN EVAC
Maintenance
use only.
ACC JACK
INOP
February 14, 2003
Flight Attendant Manual
Control Panels -
Attendant Switch Panels
Copyright © The Boeing Company. See title page for details.
2.10.4 D611W302-TBC (200 GenFam)
Door 2 Left/Right, Door 3 Left/Right, Door 4 Left
LIGHT 2 LIGHT 1
WORK WORK
EVAC
SHUT OFF COMMAND
HORN EVAC
Maintenance
use only.
8 3
ACC JACK
INOP
February 14, 2003
Flight Attendant Manual
Control Panels -
Attendant Switch Panels
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2.10.5
Door 1 Center, Door 4 Center
LIGHT 2 LIGHT 1
WORK WORK
3
February 14, 2003
Flight Attendant Manual
Control Panels -
Attendant Switch Panels
Copyright © The Boeing Company. See title page for details.
2.10.6 D611W302-TBC (200 GenFam)
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February 14, 2003
Flight Attendant Manual
Control Panels Chapter 2
Passenger Control Unit Section 20
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2.20.1
2.20 Control Panels-Passenger Control Unit
Passenger Control Unit
There is a passenger control unit (PCU) located in the arm rest of each passenger
seat.
Also, there are passenger control units (PCUs) located in the crew rest area(s).
The PCU is used to make entertainment selections, turn the reading light 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 vendor’s manuals for specific details and operation.
Note: PCU’ s, where applicable, must be stowed during ground taxi operations,
takeoff, and landing.
February 14, 2003
Flight Attendant Manual
Control Panels -
Passenger Control Unit
Copyright © The Boeing Company. See title page for details.
2.20.2 D611W302-TBC (200 GenFam)
PCU - All Classes
4
February 14, 2003
Flight Attendant Manual
Control Panels -
Passenger Control Unit
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2.20.3
PCU - Crew Rest
Each crew rest bunk contains a PCU which is used to the select various in-flight
entertainment system functions, turn the reading lights on or off, or call for
service/assistance.
C
V
O
L
L
H
A
N
E
N
4
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Control Panels -
Passenger Control Unit
Copyright © The Boeing Company. See title page for details.
2.20.4 D611W302-TBC (200 GenFam)
Intentionally
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February 14, 2003
Flight Attendant Manual
Cabin Management System Chapter 2A
Table of Contents Section 0
FCOM Template 12/12/98
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.TOC.0.1
2A.0 Cabin Management System-Table of Contents
Overview. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.10.1
Cabin Management System Overview . . . . . . . . . . . . . . . . . . . 2A.10.1
Control Panels . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.10.1
Cabin System Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.10.3
Cabin System Control Panel Menu. . . . . . . . . . . . . . . . . . . . . . 2A.10.3
Cabin System Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.10.5
Cabin Controls Main Menu . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.10.5
Cabin Controls Main Menu Screen . . . . . . . . . . . . . . . . . . . 2A.10.6
Lighting. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.15.1
Lighting Menu. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.15.1
Cabin Lighting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.15.3
Cabin Lighting System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.15.3
Cabin Lighting Display . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.15.3
Cabin Lighting Operation . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.15.5
Entry Way Lights. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.15.7
Entry Way Lights System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.15.7
Entry Way Lights Display . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.15.7
Entry Way Lights Operation . . . . . . . . . . . . . . . . . . . . . . . . 2A.15.9
Reading Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.15.11
Reading Lights System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.15.11
Reading Lights Display . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.15.11
Reading Lights Operation . . . . . . . . . . . . . . . . . . . . . . . . . 2A.15.13
February 14, 2003
Flight Attendant Manual
Copyright © The Boeing Company. See title page for details.
2A.TOC.0.2 D611W302-TBC (200 GenFam)
Cabin Management System -
Table of Contents
Service Calls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.20.1
Service Call/Chime Control Menu . . . . . . . . . . . . . . . . . . . . . . 2A.20.1
Service Call . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.20.3
Service Call Display . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.20.3
Service Call Operation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.20.5
Area Chimes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.20.7
Area Chime Control Display. . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.20.7
Area Chime Control Operation . . . . . . . . . . . . . . . . . . . . . . 2A.20.9
Seat Chimes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.20.11
Seat Chime Control Display . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.20.11
Seat Chime Control Operation . . . . . . . . . . . . . . . . . . . . . . 2A.20.13
Cabin Temperature . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.25.1
Cabin Temperature Display. . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.25.1
Cabin Temperature Control System . . . . . . . . . . . . . . . . . . . . . 2A.25.3
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Table of Contents
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.TOC.0.3
System operation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.25.3
Water/Waste Tank . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.30.1
Water/Waste Tank Status Menu . . . . . . . . . . . . . . . . . . . . . . . . 2A.30.1
Lavatories. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.30.3
Lavatory/Waste Tank Status Display . . . . . . . . . . . . . . . . . . . . 2A.30.3
Lavatory/Waste Tank Status Overview . . . . . . . . . . . . . . . . 2A.30.4
Lavatory Inoperable . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.30.5
Lavatory Inoperable Control Display . . . . . . . . . . . . . . . . . . . . 2A.30.5
Lavatory Inoperable Control . . . . . . . . . . . . . . . . . . . . . . . . 2A.30.7
Potable Water. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.30.9
Potable Water Status Display . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.30.9
Potable Water System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.30.11
Potable Water Status . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.30.11
Passenger Address . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.35.1
Passenger Address Display. . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.35.1
Passenger Address Operations. . . . . . . . . . . . . . . . . . . . . . . 2A.35.3
Cabin Door Status . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.40.1
Cabin Door Status Display . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.40.1
Cabin Door Status Display . . . . . . . . . . . . . . . . . . . . . . . . . 2A.40.1
Display Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.45.1
Display Controls Menu . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.45.1
Smoking Assignments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.50.1
Smoking Assignments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.50.1
Smoking Assigments Display . . . . . . . . . . . . . . . . . . . . . . . 2A.50.1
Smoking Assignments Operations. . . . . . . . . . . . . . . . . . . . 2A.50.3
February 14, 2003
Flight Attendant Manual
Copyright © The Boeing Company. See title page for details.
2A.TOC.0.4 D611W302-TBC (200 GenFam)
Cabin Management System -
Table of Contents
Boarding Music . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.51.1
Boarding Music Display . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.51.1
Boarding Music Operation. . . . . . . . . . . . . . . . . . . . . . . . . . 2A.51.2
Non-Normal Operations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.60.1
Alert Messages . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.60.1
Smoke Detection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.60.2
Cabin Temperature . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.60.4
Water/Waste Tank. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.60.5
Communications . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.60.7
FUNCTION LOCK-OUT Messages. . . . . . . . . . . . . . . . . . . . . 2A.60.9
Decompression. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.60.9
Invalid Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.60.10
Reduced Power. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.60.11
Error Messages . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.60.12
NOT A VALID ENTRY Messages . . . . . . . . . . . . . . . . . . 2A.60.12
Miscellaneous Messages . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2A.60.14
ENTRY OUT OF SEQUENCE . . . . . . . . . . . . . . . . . . . . . 2A.60.14 February 14, 2003
Flight Attendant Manual
Cabin Management System Chapter 2A
Overview Section 10
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.10.1
[Options shown: CSCP: Door 1L, Option: Door 2L;
CACP: Door 2L/4R (777-200/777-200ER), 2L/5R (777-300/777-300ER);
Option: CACP Door 1L/4R (777-200/777-200ER), 1L/5R (777-300/777-300ER)]
2A.10 Cabin Management System-Overview
Cabin Management System Overview
The Cabin Management System (CMS) is a computerized system designed to
control cabin services. Flight attendants use the Cabin System Control Panel
(CSCP) or a Cabin Area Control Panel (CACP) to operate the CMS.
Each airplane has one CSCP and two CACPs. Both the CSCP and CACPs have
touch sensitive displays that enable the user to select all functions. The display is
approximately 12 inches wide.
Control Panels
Cabin System Control Panel (CSCP)
The CSCP is located at the attendant station at door 1L.
The CSCP has two main functions:
• Cabin Control
• Cabin Maintenance.
Touch Sensitive Display
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Overview
Copyright © The Boeing Company. See title page for details.
2A.10.2 D611W302-TBC (200 GenFam)
Cabin Area Control Panel (CACP)
The CACPs are near the following locations:
• the door 2L attendant station
• the door 4R attendant station
The CACP is primarily used to monitor and control cabin functions.
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Cabin System Control
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.10.3
2A.10 Cabin Management System-Cabin System Control
Cabin System Control Panel Menu
Note: When power is first supplied to the cabin management system, the Cabin
System Control Panel menu appears on the CSCP.
1 Cabin Controls
Push - accesses the CABIN CONTROLS MAIN MENU display.
2 Cabin Maintenance
Used by maintenance personnel to test the cabin management system and to install
software.
CABIN CONTROLS
CABIN MAINTENANCE
CABIN SYSTEM CONTROL PANEL
2
1
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Cabin System Control
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2A.10.4 D611W302-TBC (200 GenFam)
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February 14, 2003
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Cabin System Control
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.10.5
[Options shown: Boarding Music control, Smoking Assignemnts, CSCP and
CACP Panel Override;
Option: Lavatory Inoperative Control]
2A.10 Cabin Management System-Cabin System Control
Cabin Controls Main Menu
When power is first supplied to the cabin management system (CMS), the Cabin
Controls Main Menu automatically appears on the CACPs. The flight attendant is
able to monitor and control passenger cabin functions using this menu. The CSCP
and all of the CACP’s are configured to control all of the areas throughout the
passenger cabin.
Pushing the PANEL OVERRIDE switch, located in the upper right hand corner of
the Cabin Controls Main Menu display, lets the CACPs control any area in the
passenger cabin.
The Cabin Controls Main Menu automatically appears on the CACPs. It also
appears on the CSCP when Cabin Controls is selected from the display. Access to
the selections is by pushing the desired display switch .
Note: Pushing the Cabin Controls selection on the CSCP displays the Cabin
Controls Main Menu. February 14, 2003
Flight Attendant Manual
Cabin Management System -
Cabin System Control
Copyright © The Boeing Company. See title page for details.
2A.10.6 D611W302-TBC (200 GenFam)
Cabin Controls Main Menu Screen
1 EXIT
Displays the Cabin System Control Panel menu.
2 LIGHTING
Controls the cabin, entry way and reading lights.
3 SERVICE CALL/CHIME CONTROL
Provides information on passenger-to-attendant calls and allows the cabin crew to
disable passenger to attendant chimes.
4 CABIN TEMPERATURE
Allows the cabin crew to control the temperature in the passenger cabin.
5 WATER/WASTE TANK STATUS
Provides information on potable water and waste tank level status. It also provides
selection for lavatory inoperable controls.
6 BOARDING MUSIC
Turns boarding music on/off.
PANEL
OVERRIDE CABIN CONTROLS MAIN MENU
LIGHTING
SERVICE CALL/CHIME CONTROL
CABIN TEMPERATURE
WATER/WASTE TANK STATUS
PASSENGER ADDRESS
CABIN DOOR STATUS
DISPLAY CONTROLS
EXIT
SMOKING ASSIGNMENTS
BOARDING MUSIC
4
5
3
2
6
1
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Cabin System Control
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.10.7
1 PANEL OVERRIDE
Allows the CSCP and the CACPs to control functions for all areas.
The PANEL OVERRIDE switch is located in the top right corner of the CSCP and
the CACPs. It is available from the CABIN CONTROLS MAIN MENU only.
Pushing the PANEL OVERRIDE switch causes the switch to illuminate green and
gives the CSCP and CACPs control of all areas in the passenger cabin.
The area description in the area select indicator is updated to include the additional
areas. Displays that have an All Areas Controlled By Panel selection will now
have an All Areas Controlled By Airplane selection. The PANEL OVERRIDE
switch illuminating green indicates the override condition is activated and remains
active until the override condition is reset.
To reset the override condition, push the PANEL OVERRIDE switch. It
extinguishes, and the CSCP and each CACP revert to their original configurations.
2 PASSENGER ADDRESS
Provides volume control for the PA system.
3 CABIN DOOR STATUS
Provides data for door position (locked or not locked).
PANEL
OVERRIDE CABIN CONTROLS MAIN MENU
LIGHTING
SERVICE CALL/CHIME CONTROL
CABIN TEMPERATURE
WATER/WASTE TANK STATUS
PASSENGER ADDRESS
CABIN DOOR STATUS
DISPLAY CONTROLS
EXIT
BOARDING MUSIC
SMOKING ASSIGNMENTS
1
2
3
4
5
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Cabin Management System -
Cabin System Control
Copyright © The Boeing Company. See title page for details.
2A.10.8 D611W302-TBC (200 GenFam)
4 DISPLAY CONTROLS
Provides panel brightness controls and panel lockout controls.
5 SMOKING ASSIGNMENTS
Provides selection to revise smoking areas.
February 14, 2003
Flight Attendant Manual
Cabin Management System Chapter 2A
Lighting Section 15
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.15.1
2A.15 Cabin Management System-Lighting
Lighting Menu
The Lighting Menu displays three lighting selections:
• CABIN LIGHTING – allows the cabin crew to review and control the
cabin lighting settings by area/zone.
• ENTRY WAY LIGHTS – allows the cabin crew to control the entry way
lights settings by door.
• READING LIGHTS – allows the cabin crew to either give control of the
reading lights to the passengers through their PCU, or turn the lights on or
off.
LIGHTING MENU
MAIN
MENU
CABIN LIGHTING
ENTRY WAY LIGHTS
READING LIGHTS
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Copyright © The Boeing Company. See title page for details.
2A.15.2 D611W302-TBC (200 GenFam)
Intentionally
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Cabin Lighting
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.15.3
2A.15 Cabin Management System-Cabin Lighting
Cabin Lighting System
Cabin Lighting Display
1 MAIN MENU
Push - returns to the MAIN MENU.
2 PREVIOUS MENU
Push - returns to the Lighting Menu.
3 Segmented Bar
Segment illuminated (green) - corresponds to the selected area description.
The number of segments in the bar correspond to the number of areas controlled
by the CSCP/CACP.
When ALL AREAS is selected, all segments of the segmented bar illuminate.
4 Left/Right Arrow Switches
Push - displays the desired area/zone.
MENU
PREVIOUS
NIGHT LOW MEDIUM HIGH
MENU
MAIN
CABIN LIGHTING
ALL AREAS 4
6
5
3 2 1
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Cabin Lighting
Copyright © The Boeing Company. See title page for details.
2A.15.4 D611W302-TBC (200 GenFam)
5 Area Description
Displays the selected area:
• FIRST CLASS, BUSINESS CLASS
• ECONOMY CLASS FWD
• ECONOMY CLASS AFT
• ALL AREAS.
6 Lighting Level Switches
Push the appropriate switch for the level of lighting desired.
The selected switch illuminates green when the cabin achieves the desired lighting
level.
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Cabin Lighting
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.15.5 Cabin Lighting Operation
The Cabin Lighting display shows:
• the default area in the area description
• the appropriate lighting level switch for that area is illuminated.
To change/reset the lighting for an area/zone:
• push the left/right arrow switches to select the desired area/zone
• select the desired lighting level by pushing the NIGHT, LOW, MEDIUM,
or HIGH switch
Note: The selected switch remains gray until the cabin lighting achieves the
selected lighting level, then illuminates green.
• verify lighting changes to the selected level
• verify the selected switch illuminates.
Panel Selections
CSCP 1L -
• FIRST CLASS, BUSINESS CLASS, ECONOMY CLASS FWD,
ECONOMY CLASS AFT, and ALL AREAS.
CACP 2L, CACP 4R -
• ECONOMY CLASS FWD, ECONOMY CLASS AFT, and ALL
AREAS.
Things to Remember
A power failure or failure of a cabin management system control panel will not
change the light settings.
A power failure or failure of a CACP will not change the light settings.
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Cabin Lighting
Copyright © The Boeing Company. See title page for details.
2A.15.6 D611W302-TBC (200 GenFam)
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February 14, 2003
Flight Attendant Manual
Cabin Management System -
Entry Way Lights
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.15.7
2A.15 Cabin Management System-Entry Way Lights
Entry Way Lights System
Entry Way Lights Display
1 MAIN MENU
Push - returns to the Main Menu.
2 PREVIOUS MENU
Push - returns to the Lighting Menu.
3 Segmented Bar
Segment illuminated (green) - corresponds to the selected area description.
The number of segments in the bar correspond to the number of areas controlled
by the CSCP/CACP.
When ALL AREAS is selected, all segments of the segmented bar illuminate.
4 Left/Right Arrow Switches
Push - displays the desired area/zone.
ON OFF
MENU
PREVIOUS
DOOR 1 LEFT
ENTRY WAY LIGHTS
MAIN
MENU
3
4
5
6 7
2 1
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Entry Way Lights
Copyright © The Boeing Company. See title page for details.
2A.15.8 D611W302-TBC (200 GenFam)
5 Area Description
Displays the selected area:
• DOOR 1 LEFT
• DOOR 2 LEFT
• CABIN ENTRY WAY LIGHTS CONTROL
6 ON
Push - turns entry way lights on.
Verify switch illuminates green.
7 OFF
Push - turns Entry Way Lights off.
Verify switch illuminates green.
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Entry Way Lights
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.15.9
Entry Way Lights Operation
The Entry Way Lights display shows:
• the default area in the area description display
• the active entry way light switch for that area.
To change/reset the level for an area/zone:
• push the left/right arrow switches to select the desired area/zone
• select the desired state of the entry way lights (push the ON or OFF
switch)
• verify lighting changes to the selected level
• verify the selected switch illuminates green.
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Entry Way Lights
Copyright © The Boeing Company. See title page for details.
2A.15.10 D611W302-TBC (200 GenFam)
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February 14, 2003
Flight Attendant Manual
Cabin Management System -
Reading Lights
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.15.11
2A.15 Cabin Management System-Reading Lights
Reading Lights System
Reading Lights Display
1 MAIN MENU
Push - returns to the Main Menu.
2 PREVIOUS MENU
Push - returns to the Lighting Menu.
3 Segmented Bar
Segment illuminated (green) - corresponds to the selected area description.
The number of segments in the bar correspond to the number of areas controlled
by the CSCP/CACP.
When ALL AREAS is selected, all segments of the segment bar illuminate.
4 Left/Right Arrow Switches
Push - displays the desired area/zone.
PREVIOUS
MENU
NORMAL OFF ON
READING LIGHTS
MAIN
MENU
FIRST CLASS 4
5
8
6 7
3 2 1
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Reading Lights
Copyright © The Boeing Company. See title page for details. 2A.15.12 D611W302-TBC (200 GenFam)
5 Area Description
Displays the selected area:
• FIRST CLASS
• BUSINESS CLASS
• ECONOMY CLASS FWD
• ECONOMY CLASS AFT
• ALL AREAS
• CABIN READING LIGHTS CONTROL.
6 ON
Push (illuminated green) - turns the reading lights on.
7 OFF
Push (illuminated green) - turns the reading lights off.
8 NORMAL
Push (illuminated green) - gives the passenger control of the reading lights
through the PCU.
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Reading Lights
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.15.13
Reading Lights Operation
There are three Reading Lights states:
• NORMAL - allows the passenger to control the reading light from the
PCU
• ON - turns all reading lights on, regardless of the PCU selection
• OFF - turns all reading lights off, regardless of the PCU selection.
The Reading Lights display shows:
• the default area in the area description display
• the active reading light switch for that area.
To change/reset the lights for an area/zone:
• verify the NORMAL switch is illuminated
• push the left/right arrow switches to select the desired area/zone
• select the desired state of the reading lights by pushing the ON or OFF
switch
• verify lighting changes to the selected level
• verify the selected switch illuminates green momentarily, then
extinguishes
• verify the NORMAL switch illuminates, giving the passengers control of
their reading lights.
Panel Selections
CSCP 1L -
• FIRST CLASS, BUSINESS CLASS, ECONOMY CLASS FWD,
ECONOMY CLASS AFT, ALL AREAS, and
CABIN READING LIGHTS CONTROL
CACP 2L -
• BUSINESS CLASS, ECONOMY CLASS FWD,
ECONOMY CLASS AFT, ALL AREAS, and
CABIN READING LIGHTS CONTROL
CACP 4R -
• ECONOMY CLASS FWD, ECONOMY CLASS AFT, ALL AREAS,
and CABIN READING LIGHTS CONTROL
Note: CABIN READING LIGHTS CONTROL available only when PANEL
OVERRIDE has been selected at CACP 2R or CACP 4L.
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Reading Lights
Copyright © The Boeing Company. See title page for details.
2A.15.14 D611W302-TBC (200 GenFam)
Intentionally
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February 14, 2003
Flight Attendant Manual
Cabin Management System Chapter 2A
Service Calls Section 20
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.20.1