Bombardier-Challenger_01-Aircraft_General庞巴迪挑战者飞机概述

航空发表于 2010-5-9 08:46:45

Bombardier-Challenger_01-Aircraft_General
 
**** Hidden Message *****

航空发表于 2010-5-9 08:47:11

OPERATING MANUAL PSP 601A-6 SECTION 1 AIRCRAFT - GENERAL TABLE OF CONTENTS MODEL DESIGNATION AND TYPE OPERATING ROLE AND DESIGN CONCEPT AIRCRAFT DIMENSIONS AIRCRAFT TURNING RADII DANGER AREAS AIRCRAFT PARKING AND MOORING SERVICING POINTS AIRCRAFT ANTENNAS DOORS A. Passenger/Crew Door B. Emergency Exit Door C. Baggage Compartment Door D. Rear Equipment Bay Door E. Service Doors F. Door Indication Lights FLIGHT COMPARTMENT A. Crew Seats B. Instrument and Control Panels C. Cabin Sign Switches Page 1 1 1 1 1 2 2 2 2 2 3 3 4 4 4 4 4 4 4 1 - CONTENTS Page 1 Mar 10/95 OPERATING MANUAL PSP 601A-6 LIST OF ILLUSTRATIONS Figure Title Page Number 1 Aircraft Basic Dimensions and Ground Clearances 5 2 Aircraft Turning Radii 6 3 Engine Intake and Exhaust Danger Areas, and APU Exhaust 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 Danger Area Aircraft Servicing Points (2 Sheets) Aircraft Antenna Locations Passenger/Crew Door Baggage Compartment Door Service Doors and Panels Door Indication Lights and Cabin Signs Switches (2 Sheets) Crew Seats (2 Sheets) Flight Compartment Instrument and Control Panel Arrangement Pilot's Instrument Panel Copilot's Instrument Panel Centre Instrument Panel (3 Sheets) Overhead Panel and Glareshield (2 Sheets) Centre Pedestal (2 Sheets) Pilot's Console, Side and Facia Panels Copilot's Console, Side and Facia Panels 7/8 9 11 12 13 14 15 16B 18 19 20 20A 22 24 26 27 1 - CONTENTS Page 2 May 01/96 OPERATING MANUAL PSP 601A-6 SECTION 1 AIRCRAFT - GENERAL 1. MODEL DESIGNATION AND TYPE The aircraft, named Challenger, is manufactured by Canadair Limited. The Challenger model covered by this manual is the CL-601, Model 2B16, Variant 601-3A, {Variant 601-3R for airplanes 5135 and subsequent), powered by two General Electric CF34 turbofan engines. 2. OPERATING ROLE AND DESIGN CONCEPT Primarily, the Challenger is a long-range (transcontinental) business aircraft operated by a crew of two. The aircraft is designed to carry up to 19 passengers in spacious comfort over long distances. The combination of a technologically advanced supercritical wing, quiet and efficient engines, and a wide body enables the Challenger to achieve a high standard of performance, economy and passenger comfort. 3. AIRCRAFT DIMENSIONS (Figure 1) All basic dimensions, including ground clearances, are given in Figure 1. 4. AIRCRAFT TURNING RADII (Figure 2) Using the nose gear steering control wheel, the pilot can turn the aircraft, during taxiing, without differential braking. Figure 2 shows the turning radii applicable to the maximum nose wheel steering angle of 55 degrees, the minimum taxi strip width required for a 180-degree turn at the maximum steering angle, and the turning radii for the maximum towing angle of 90 degrees. 5. DANGER AREAS (Figure 3) I t is essential that persons involved with engine or APU running are aware of the danger areas in front of and to the rear of the engine(s). Before running an engine or the APU, the information illustrated in figure 3 must be used to consider the safety of persons, equipment and buildings in the vicinity of the aircraft. SECTION 1 Page 1 Apr 10/95 OPERATING MANUAL PS? 601A-6 AIRCRAFT PARKING AND MOORING When the aircraft is stationary on the ground, precautions must be taken to ensure safety of personnel and equipment. The extent of safety measures to be observed depends upon the prevailing or expected weather conditions and the expected length of time the aircraft will be stationary. For complete instructions on parking and mooring the aircraft, refer to Ground Handling and Servicing Information, PSP 601-13. SERVICING POINTS (Figure 4) Location and details for all aircraft servicing points are shown in Figure 4. AIRCRAFT ANTENNAS (Figure 5) Location and nomenclature of the aircraft antennas are given in Figure 5. DOORS The aircraft is provided with a passenger/crew door, a baggage compartment door, a rear equipment bay door, landing gear doors and various small doors which provide access to servicing points. An overwing emergency exit door is provided on the right side of the passenger compartment. The baggage compartment and emergency exit doors are of the plug type which open inward; all other doors open outward. All doors are flush with the aircraft outer skin when closed* A. Passenger/Crew Door (Figure 6) The entrance door is electrically or manually operated and downward opening, with the stairs forming an integral part of the door structure. I t s movement i s controlled .by a counterbalance system of gas springs. An electrical power assist system provides an optional means of closing the door from inside the aircraft. A control switch, labelled CABIN DOOR, is located just forward of the entrance door. Holding the switch to the RAISE position activates the system which raises the door from any open position up to the closed position. Once the switch is released, the door can s t i ll be operated manually. A pull-in handle on the rear handrail can be used to reduce the force required to close the door manually from the inside of the aircraft. The latching mechanism is operated by an internal single-lever handle, located on the forward side of the steps, a T-handle which is recessed in a riser of a step and an external handle with a keylock. SECTION 1 Page 2 Apr 02/87 cacnhaadliaBirn qer OPERATING MANUAL PSP 601A-6 On aircraft 5041 and 5146, a vent flap linked with the external handle locking mechanism is located just above the external handle recess, to ensure that the cabin cannot be fully pressurized unless the door is correctly locked. The vent opens whenever the external handle is moved from the stowed position. A viewing window adjacent to the T-handle displays the legends LOCKED and UNLOCKED to indicate the position of the external handle. Once closed, the door is latched from the inside by pushing the internal handle downward. The T-handle is then pulled out of its recess to stow the external handle, which clicks audibly when stowed. Verification that the external handle is stowed can be made by ensuring that the internal handle cannot be pulled up. After this check, the T-handle must be stowed in the riser of the step. From outside the airplane, the door is latched by rotating the external handle fully clockwise to engage the door latches and stow the pull-out handle. Pushing the external handle then places it in the stowed position. The door is unlocked from the inside when the internal handle is pulled upward, ejecting the external handle from its pocket. The door is then unlatched by continuing to pull the internal handle upward. As the door opens, the handrails unfold upward. The door unlocks from the outside by the operation of a PUSH trigger in the external handle, which is ejected from its pocket. To unlatch the door, the external handle is then turned 45 degrees counterclockwise. Pull-out and pull-in handles are also provided to assist the operator in opening or closing the door from the outside or inside, respectively. When the door is fully open, a door support leg extends to the ground. B. Emergency Exit Door For details of the emergency exit door, refer to Section 8. C. Baggage Compartment Door (Figure 7) The baggage compartment door is located on the left side of the aircraft immediately aft of the passenger compartment. The door opens inwards and upwards, and is assisted during opening by balance springs. The door is held closed by two plungers which are operated by an external and an internal handle. Two proximity switches are installed to provide an indication in the flight compartment when the door is not safely closed. The external handle stows flush into a pocket in the door outer skin and, in this position, acts as a lock for the latching mechanism. The handle has a keylock which unlocks or locks a PUSH trigger. The PUSH trigger, when pressed, ejects the handle which can then be turned to release the locking plungers and to open the door. SECTION 1 Page 3 Aug 14/02 cacnhaadJaieirn per OPERATING MANUAL PSP 601A-6 D. Rear Equipment Bay Door (Figure 8) The rear equipment bay door, located at the bottom of the rear fuselage, provides access to the APU, engine oil replenishment system, air conditioning units, replenishment points for No. 1 and No. 2 hydraulic systems, and the aircraft battery. The door opens downward, has two integral steps, and is secured at the forward edge by two hinges which are equipped with quick-release pins to facilitate easy door removal. The rear equipment bay door is held closed by two plungers at the rear edge, and is opened and closed by a handle. Handle operation is the same as for the baggage compartment door, with the exception that the rear equipment bay door must be supported during opening because of opening direction. E. Service Doors (Figure 8) Quick-release service door sand panels are provided for easy access to the servicing points throughout the aircraft. Location and nomenclature of these doors and panels are given in Figure 8. F. Door Indication Lights (Figure 9) For operation of the DOOR INDICATION lights, refer to Figure 9. FLIGHT COMPARTMENT Miscellaneous items in the flight compartment include a portable fire extinguisher, located behind the copilot's seat on the bulkhead that separates the flight and passenger compartments, two oxygen masks, two cup holders, and storage boxes and pouches for checklists, etc. The windshield centre post incorporates a pilot's eye locator to enable seat adjustments for optimum field of vision. A. Crew Seats (Figure 10) The pilot's and copilot's seats are identical except that certain controls are installed on opposite sides. On both seats, inertia reel and forward/rearward controls are located inboard, and lumbar support, height and reclining controls are located outboard. B. Instrument and Controls panels (Figure 11) The instrument and control panels are arranged as shown in Figure 11, and are presented in Figures 12 to 18. Circled numbers on the instrument and control panels refer to sections of this manual where information on the item can be found. c. Cabin 5ign Switches (Figure 9) For operation of the NO SMOKING and FASTEN SEAT BELT signs in the passenger cabin, refer to Figure 9. SECTION 1 Page 4 Mar 10/95 OPERATING MANUAL PSP 601A-6 t i 8 ft 10 in ] _ Cabin interior dimensions | [ Length Width {max dia) 28ft 3in I 8ft 2in Headroom (floor to max height) 6ft 1 in | Volume Floor area Floor width 1150 cu. ft 202.5 sq. ft 7ft 2in / \ Measurement at manufacturers empty weight y 21 feet elevator up / s \ Open passenger door ground clearance 4 inches EFFECTIYITY J Ji] A/C5001TO5134 r^ A/C 5135 & SUBS AND ^ POSTSB601-O262 20 ft 8 i r j ^ ^ Aircraft Basic Dimensions and Ground Clearances SECTION 1 Figure 1 pa g e 5 May 01/96 canactatr ctiauencjer OPERATING MANUAL PSP 601A-6 , MAXIMUM TURNING RADII USING NOSE WHEEL STEERING {MAXIMUM STEERING ANGLES I 61 FT MINIMUM TAXI STRIP WIDTH FOR 180 DEGREE TURN MINIMUM TURNING RADII WITH NOSE WHEEL AT 90?(AIRCRAFT MAXIMUM TOWING ANGLE) Aircraft Turning Radii SECTION 1 Figure 2 page 6 Apr 02/87 ctiauenQer OPERATING MANUAL PSP 601A-6 IDLE THRUST MAXIMUM THRUST 50FT + 100FT + 110 + 120 + 1301 4 SOFT APU EXHAUST DANGER AREA +100 FT + 150 FT 4-160 J-170 Engine Intake and Exhaust Danger Areas, and APU Exhaust Danger Area Figure 3 SECTION 1 Page 7/8 Apr 02/87
OPERATING MANUAL PSP 601A-6 N0.3HYDRAUUC SYSTEM DC EXTERNAL POWER AC EXTERNAL POWER PRESSURE REFUEUDEFUEL PANEL AND ADAPTER Aircraft Servicing Points Figure 4 {Sheet 1) SECTION 1 Page 9 Apr 10/95 OPERATING MANUAL PSP 601A-6 ?BRAKE ACCUMULATOR CHARGING POINTS AND INTERPHONE ?OXYGEN SYSTEM CHARGING VALVE AND GAUGE ACCUMULATOR PRESSURE GAUGE ^ ^ k * RESERVOIR FILL N0.1 HYDRAULIC SYSTEM AND REAR INTERPHONE OIL LEVEL CONTROL PANEL NO.3 HYDRAULIC SYSTBt RESBWOff) FILLS CONNECTION - ? Aircraft Servicing Points Figure 4 (Sheet 2) MO J HYDRAULIC SYSTEM ACCUMULATOR CHARGING POtflTAND PRESSURE GAUGE SECTION 1 Page 10 Apr 10/95 chauenper OPERATING MANUAL PSP 601A-6 Aircraft Antenna Locations Figure 5 SECTION 1 Page 11 Mar 10/95 canadair challenQsr OPERATING MANUAL PSP 601A-6 EFFECTIVITY Q] A/C 5041 and 5146 CABIN DOOR SWITCH o C3 3 O D EXTERNAL HANDLE Passenger/Crew Door SECTION 1 Figure 6 Page 12 Aug 14/02 OPERATING MANUAL PSP 601A-6 BALANCE SPRING BOXES PLUNGER GUIDE TRACKS HANDLE HANDLE KEY LOCK HANDLE HANDLE UNSTOW BUTTON Baggage Compartment Door Figure 7 SECTION 1 Page 13 Apr 02/87 OXYGEN REFILL OPERATING MANUAL PSP 601A-6 UPPER ELECTRONICS EQUIPMENT BAY DC GROUND POWER FLIGHT CONTROL ACCESS REFUELING CONTROL 7 UPPER ELECTRONICS EQUIPMENT BAY K HYORAUUC SYSTEM* SERVICE NO. 3 FLIGHT COMPARTMENT UNDERFLOOR ANO AVIONICS BAY ACCESS BRAKE AND STEERING HYDRAULIC BAY \r<8F FUGHT CONTROLS ACCESS APU CONTROL AND GROUND AIR START EQUIPMENT BAY DOOR Service Doors and Panels SECTION 1 Figure 8 Page 14 Apr 02/87 chaJlenQer OPERATING MANUAL PSP 601A-6 PASSENGER/CREW DOOR UNLOCKED LIGHT Amber light comes on when the door is unlatched, or when the external handle is not stowed. PASSENGER/CREW DOOR NOT READY LIGHT Amber light comes on when the T-handle is not correctly stowed. SEAT BELT SIGN SWITCH When set to ON, the cabin FASTEN SEAT BELT sign comes on and remains on until set to OFF or AUTO. When set to AUTO, the sign comes on if cabin air pressure is low, or the landing gear is down, or if the flaps are at any angle other than 0 degrees. CABIN SIGNS ^ \ 0N ff*<=^\ 0 FF AUTO NO/SMKG SEAT BLTS PASSENGER/CREW DOOR READY LIGHT Green light comes on when the external and internal handles are stowed. NO SMOKING SIGN SWITCH When set to ON, the cabin NO SMOKING sign comes on and remains on until set to OFF or AUTO. When set to AUTO, the sign comes on if cabin air pressure is low or the landing gear is down. BAGGAGE COMPARTMENT DOOR UNSAFE LIGHT Amber light comes on when door locking plungers are not safely engaged. CENTRE PEDESTAL EFFECTIVITY A/C 5001 - 5040, 5042-5145, 5147 and subsequent Door Indication Lights and Cabin Signs Switches SECTION 1 Figure 9 (Sheet 1) page 15 Aug 14/02 dhsjJenqer OPERATING MANUAL PSP 601A-6 CABIN PASSENGER/CREW DOOR INDICATOR PANEL Pressing DOOR FAULT switch/light causes either green PASS DOOR LKD or red PASS DOOR UNLOCKED light to come on for the same conditions activating flight compartment indications. Red DOOR FAULT light comes on if microswitch contacts are stuck in lock position when door is unlocked. PASS DOOR LKD PASS DOOR UNLKD DOOR FAULT ADJACENT TO PASSENGER/CREW DOOR PASS DR LKD LIGHT NO SMOKING SIGN SWITCH When set to ON, the cabin NO SMOKING sign comes on and remains on until set to OFF or AUTO. When set to AUTO, the sign comes on if cabin air pressure is low or the landing gear is down. Green light comes on to indicate that all door latches and both handles are safely locked. SEAT BELT SIGN SWITCH When set to ON, the cabin FASTEN SEAT BELT sign comes on and remains on until set to OFF or AUTO. When set to AUTO, the sign comes on if cabin air pressure is low, or the landing gear is down, or if the flaps are at any angle other than 0 degrees. CABIN SIGNS ON OFF AUTO NO SMKG SEAT BLTS PASS DR UNLKD LIGHT Red light comes on whenever door latches are not in fully latched position or both handles are not safely locked. BAG DR UNSAFE LIGHT Amber light comes on if either of the door's two locking plungers are not fully engaged. CENTRE PEDESTAL EFFECTIVITY A/C5041 and 5146 Door Indication Lights and Cabin Signs Switches SECTION 1 Figure 9 (Sheet 2) page 16 Aug 14/02 OPERATING MANUAL PSP 601A-6 THIS PAGE INTENTIONALLY LEFT BLANK SECTION 1 Page 16A Mar 10/95 canactatr ctiauencjer OPERATING MANUAL PSP 601A-6 QUICK-RELEASE BUCKLE Front of buckle can be turned to simultaneously release shoulder straps, crotch strap and one pan of lap belt; buckle remains attached to other pari of lap belt. Snap-in attachments are incorporated at strap ends so that safety harness can be easily connected. SHOULDER STRAPS LAP BELT, LUMBAR SUPPORT ARMREST CONTROL BUTTON Releases armrest lock to allow angular adjustment of armrests. RECUNE CONTROL LEVER Releases seatback lock to allow adjustment from upright to recline. Seatback locks m position when lever is released. LUMBAR SUPPORT CONTROL VALVE Releases air from lumbar support to suit contour of pilot's back. With pilot's back pressed against support, opening valve allows support to match contour of pilot's back. and dosing valve allows support to maintain selected shape. With no pressure on support, opening varve allows support to return to original shape. HEIGHT CONTROL LEVER Releases height lock to allow vertical adjustment of seat. Seat locks in selected position when lever is released. NOTE Pilot's seat shown, copilot's seat identical but opposite. Crew Seats Figure 10 (Sheet 1) SECTION 1 Page 16B Mar 10/95 chaueneter OPERATING MANUAL PSP 601A-6 INERTIA REEL INERTIA REEL CONTROL LEVER When the lever is fully forward The inertia reel allows shoulder strap reei-ou: until strap acceleration exceeds Ig. then the reel locking device operates to prevent reel-out. When the lever is fully rearward, the inertia reel is locked, thus allowing no reel-out of shoulder straps. and the harness is effectivery fixed. FORWARD/REARWARD MOVEMENT CONTROL LEVER Releases seat/ track lock to allow sea: forward/ rearward movement. Releasing control lever allows locking pins to engage when aligned with holes in track. Track lock positions are approximately one inch apart. Crew Seats Figure 10 (Sheet 2) SECTION 1 Page 17 Apr 02/87 OPERATING MANUAL PSP 601A-6 AURAL WARNING/JNTERCOM SPEAKBiS Flight Compartment Instrument and Control Panel Arrangement Figure 11 SECTION 1 Page 18 Apr 02/87 OPERATING MANUAL PSP 601A-6 Pilot's Instrument Panel Figure 12 SECTION 1 Page 19 Apr 02/87 OPERATING MANUAL PSP601A-6 Copilot's Instrument Panel Figure 13 SECTION 1 Page 20 Apr 02/87 OPERATING MANUAL PSP 601A-6 EFFECTMTY: A/C 5136 AM) SUBS Centre Instrument Panel Figure 14 {Sheet 1) SECTION 1 Page 20A Apr 10/95 OPERATING MANUAL PSP 6C1A-6 ? E*GJNE JET WE/FYIOK urt BFFECTMTY: JVC 8001 TO 6134 Centre Instrument Panel Figure 14 (Sheet 2) SECTION 1 Page 206 Apr 10/95 OPERATING MANUAL PSP 601A-6 EFFECTIVITY: A/C POST SB 601-0262 EFFECT1VITY: A/C 5001,5027 AND SUBS AND A/C POST SB 601-0225 ?? EFFECTIVITY: A/C POST SB 601-0262 e Centre Instrument Panel SECTION 1 Figure 14 (Sheet 3) Page 21 Apr 10/95 OPERATING MANUAL PSP 601A-6 j Overhead Panel and Glareshield SECTION 1 Figure 15 (Sheet 1) Page 22 May 01/96 chaflsriqer OPERATING MANUAL PSP 601A-6 HI TEMP HI TEMP HI TEMP & A ?MISC LTS ? I ROARDING DOMI COMR SERVICE ON V S ^ O N W ON V ^ / OW I W / ON PLS OFF STOV r?LANDING LTS - i IIT NOtE RIGHT I RE COG/ TAXI LT OFF/ ON* PLS OFF STDY OFF ?r EXTERNAL LTS -JOVMDFNL I1HKAAVV WtIMNGO AANNTT1I CCOOLUL ' x ^ CX \OFF / f i \ O F F / f i \ O FF OM 'ON ON OFF 昍T EFFECTIVITY : A/C POST SB 601-0363 EFFECTIVITY : A/C 5041 AND 5146 o ?? L-MTH STAGE'R WJBH ON/ OFF 昄EED OLOSID DUCT I MIL | OUCT MOM LOOP A /?N BOTH K=?J LOOPB > - ^ | M.CEO I CLOUD \m\\ OPEN I I BLEEQ I CLOUD OUCT 11 PAH. I 桺USH ON/ OFF OFF FAIL I ? I1 1 '*IL 1 z @ CABIN PRESSURIZATION EFFECTIVITY : A/C 5135 AND SUBS e EFFECTIVITY : A/C 5135 AND SUBS G Overhead Panel and Glareshield SECTION 1 Figure 15 (Sheet 2) page 23 Aug 14/02 canadair chanenqer OPERATING MANUAL PSP 601A-6 r ? Centre Pedestal SECTION 1 Figure 16 (Sheet 1) Page 24 Mar 10/95 cacnhaadnaeinr cjer OPERATING MANUAL PSP 601A-6 I EFFECTIVITY: A/C 5067, 5087 AND SUBS e f LASEREF / I AUON/ ^ > t ^ ATT | ALIGN | | NAVRDY | | ON BAH | FAULT "| NO AIR | BATTFAIL J . 1 1 mm /TEST J EFFECTIVITY : 5041 and 5146 EFFECTIVITY: A/C POST SB 601-0231 ? Centre Pedestal SECTION 1 Figure 16 (Sheet 2) Page 25 Aug 14/02 cacnhaacUlaeinr qer OPERATING MANUAL PSP 601A-6 Pilot's Console, Side and Facia Panels Figure 17 SECTION 1 Page 26 Apr 10/95 OPERATING MANUAL PSP 601A-6 Copilot's Console, Side and Facia Panels SECTION 1 Figure 18 Page 27 Apr 10/95

f214216709 发表于 2010-5-18 10:37:41

庞巴迪挑战者飞机概述

guomai127 发表于 2010-9-11 09:21:07

:lol :lol :lol

march20042004 发表于 2010-10-7 14:06:27

好东西，顶顶顶顶

super_xxx 发表于 2010-10-29 15:55:39

飞行标准类监察员（飞行运行）专业知识培训教材

:victory: 

dul 发表于 2011-2-11 13:15:57

找手册

zhege市概述不啊？

bocome 发表于 2011-7-31 11:22:13

庞巴迪挑战者防火

domoto0516 发表于 2011-10-22 18:51:16

很有趣的title 載來瞧瞧

xinlunll 发表于 2011-10-25 15:49:46

非常需要，谢谢楼主！

页: [1] 2

航空论坛_航空翻译_民航英语翻译_飞行翻译's Archiver

Bombardier-Challenger_01-Aircraft_General庞巴迪挑战者飞机概述

飞行标准类监察员（飞行运行）专业知识培训教材

找手册