AIRPLANE GENERAL Exterior REV 3, May 03/05

Transcription

1 Vol AIRPLANE GENERAL Exterior REV 3, May 03/05 24 ft 1 in (7.34 m) 5ft1in(1.55m) 10 ft 7 in (3.23 m) 6ft4in (1.93 m) 81 ft 6 in (24.85 m) 9ft6in(2.89m) 8ft10in (2.69 m) 36 ft 4 in (11.07 m) 28 ft 4 in (8.63 m) 15 ft 11 in (4.85 m) 3 ft (0.91 m) 7ft1in (2.16 m) 24 ft 1 in (7.34 m) 6ft3in(1.90m) 109 ft 10.8 in (33.50 m) 118 ft 10.7 in (36.24 m) External Aircraft Dimensions <2224> Figure

2 Exterior Vol REV 1, Jan 13/03 LEGEND Maximum thrust Idle thrust 0ft ft ft (0 m) (3) (6) (9.1) (12.2) (15.2 m) (18.3) (21.3) (24.4) (27.4) (30.5 m) 140 mph (225 km/h) 100 mph (161 km/h) 60 mph (97 km/h) ENGINE EXHAUST DANGER AREA WIDTH 7.7 ft (4 m) TEMP. VELOCITY IDLE 25 ft (8 m) 21 ft (6 m) TAKE--OFF 37 ft (11 m) 36 ft (11 m) Engine Hazard Areas <2224> Figure ft (8 m) 140 mph (225 km/h) 100 mph (161 km/h) 60 mph (97 km/h) 0ft ft ft ft ft ft (0 m) (3) (6) (9.1) (12.2) (15.2 m) (18.3) (21.3) (24.4) (27.4) (30.5 m) (33.5) (36.6) (39.6) (42.7) (45.7 m) (48.8) (51.8) (54.8) (57.9) (61 m) (64) (67.1) (70.1) (73.1) (76.2 m) (79.2) (82.2) (85.3) (88.4)

3 Vol AIRPLANE GENERAL Exterior REV 3, May 03/05 R4 R6 R5 NOSE WHEEL ANGLE R2 R3 R1 NOTE Maximum steering Symmetrical and idle thrust No differential braking 80 degree steering angle Slip of 3 degrees Dry runway Slow continuous turn Maximum airplane weight Aft center of gravity TURNING RADII FOR VARIOUS NOSE WHEEL ANGLES ANGLE R1 R2 R3 R4 R5 R6 ft m ft m ft m ft m ft m ft m Taxiing and Turning Radii Figure

4 Exterior Vol Sep 09/02 GROUND AIR CONDITIONING AIR SINGLE POINT REFUEL/DEFUEL REFUEL DEFUEL CONTROL PANEL FORWARD POTABLE WATER OXYGEN REFILL FORWARD LAVATORY WASTE DRAIN ADG PUMP ADG GROUND POWER EXTERNAL SERVICES APU HYDRAULIC SYSTEMS 1 & 2 AFT LAVATORY WASTE DRAIN HYDRAULIC SYSTEM 3 OVERWING GRAVITY FUEL FILLER LAVATORY POTABLE WATER ENGINE START HIGH PRESSURE AIR OVERWING GRAVITY FUEL FILLER BRAKE ACCUMULATORS Airplane Service Points <2224> Figure

5 Vol AIRPLANE GENERAL Exterior REV 1, Jan 13/03 FS FS FS WS WL29.31 JACKING POINT NYLON PLUG NYLON PLUG MOORING ADAPTER PLATE JACKING PAD MOORING POINT MOORING TIE--DOWN RING Airplane Mooring Points Figure

6 Exterior Vol REV 3, May 03/05 TCAS DIRECTIONAL ATC 1 (ATC 2 OTHER SIDE) GPS 1 VHF 1 GPS 2 UNDERWATER LOCATOR BEACONS (CVR AND FDR) VOR AND LOCALIZER (BOTH SIDES) TCAS OMNI DIRECTIONAL VHF 2 ATC 2 (ATC 1 OTHER SIDE) ADF DME 1 (DME 2 OTHER SIDE) 2ND RADIO ALTIMETER MARKER BEACON EMERGENCY LOCATOR TRANSMITTER (OTHER SIDE) RADIO ALTIMETER WEATHER RADAR GLIDESLOPE NOTE Radar hazard area is2ft(0.6m) from antenna with radome closed. Airplane Antenna Locations <1045, 1027,1212> Figure

7 Vol AIRPLANE GENERAL Flight Compartment REV 1, Jan 13/03 GLARESHIELD OVERHEAD PANEL CENTER INSTRUMENT PANEL PILOT S INSTRUMENT PANEL PILOT S SIDE PANEL COPILOT S INSTRUMENT PANEL COPILOT S SIDE PANEL PILOT S SIDE CONSOLE COPILOT S SIDE CONSOLE CENTER PEDESTAL Flight Compartment Panel Layout Figure

8 Flight Compartment Vol Sep 09/02 NOSE WHEEL STEERING TILLER 16 OXYGEN MASK REGULATOR STORAGE COMPARTMENT 9 HEADPHONE (HDPH) MICROPHONE (MIC) JACKS 5 N 100 % PUSH OXYGEN MASK PRESS TO TEST AND RESET AIR--CONDITIONING SYSTEM OUTLET HDPH /MIC FLIGHT BAG COMPARTMENT AIR -CONDITIONING SYSTEM INTAKE Indicates Chapter in which information on item may be found. Pilot s Side Console <1205> Figure

9 Vol AIRPLANE GENERAL Flight Compartment REV 3, May 03/ LEGEND 1. Clock Display control panel. 3. Air data reference panel. 4. Display reversionary panel. 5. Stall protection panel Windshield wiper control panel. 7. Lighting panel Nose wheel steering subpanel. 9. Air conditioning system gasper Indicates Chapter in which information on item may be found. Pilot s Side Panel <2040> Figure

10 Flight Compartment Vol Sep 09/02 PRIMARY FLIGHT DISPLAY 18 AIRSPEED LIMITS PLACARD (TYP) COCKPIT VOICE RECORDER 5 SEC HOLD TEST HEADSET ERASE COCKPIT VOICE RECORDER (CVR) CONTROL UNIT 5 MULTIFUNCTION DISPLAY 18 Indicates chapter in which information on item may be found. Pilot s Instrument Panel <1015, 2217> Figure

11 Vol Flight Compartment Sep 09/02 12 STANDBY INSTRUMENT RAM AIR OPEN ENGINE INDICATION AND CREW ALERTING SYSTEM (EICAS) PRIMARY DISPLAY 2 EICAS SECONDARY DISPLAY 2 Indicates Chapter in which information on item may be found. Centre Instrument Panel <1001> Figure

12 Flight Compartment Vol Sep 09/ LEGEND 1. Cabin pressurization panel Copilot s dome light control Air--conditioning panel. 4. Anti--ice panel Engine / ignition panel Miscellaneous lights panel Hydraulic pump panel Emergency lights panel Passenger signs panel Passenger oxygen control. 9 Indicates Chapter in which information on item may be found. Overhead Panel <1020><1201> Figure Standby compass Emergency locator transmitter control Landing lights panel External lights panel Hydraulic shutoff panel APU panel Fire detection / FIREX monitor panel Pilot s dome light control Electrical panel Bleed air panel Fuel panel. 13

13 Vol AIRPLANE GENERAL Flight Compartment REV 1, Jan 13/ Left Glareshield Center Glareshield Right Glareshield LEGEND 1. Roll select Master warning Master caution Stall warning GPWS and glideslope warning Engine fire warning Firex bottle discharge Flight control panel APU fire warning. 10 Indicates chapter in which information on item may be found. Glareshield <2040> Figure

14 Flight Compartment Vol REV 3, May 03/ LEGEND 1. Landing gear control panel Flight management system control display unit Interphone panel Engine / miscellaneous test panel Ground proximity warning panel. 18 Indicates Chapter in which information on item may be found. Centre Pedestal (Upper) <2040, 1214> Figure

15 Vol AIRPLANE GENERAL Flight Compartment REV 3, May 03/ LEGEND 1. Spoilers system control subpanel Pitch disconnect control Flight spoiler lever Roll disconnect control Slat/ flap lever Metric altimeter subpanel Thrust lever quadrant Thrust reverser subpanel. 20 Indicates Chapter in which information on item may be found. Center Pedestal --- Thrust Lever and Flight Controls <1029, 2040> Figure

16 Flight Compartment Vol Sep 09/ A LEGEND 1. Radio tuning unit EICAS control panel Audio control panel Aileron/rudder trim panel Lighting panel Weather radar control panel Yaw damper panel Interphone control panel Source selector panel. 10. Cargo firex panel Emergency flap deploy control Air driven generator -- auto--deploy panel Air driven generator -- manual deploy handle. 14. Landing gear -- manual release handle Parking brake handle Compass control panel (on both sides) A. <1025> IRS mode select unit Avionics cooling control panel Stabilizer/Mach trim panel Backup tuning unit. 5 7 Indicates Chapter in which information on item may be found. Centre Pedestal (Lower) <1012, 1025,> Figure

17 Vol AIRPLANE GENERAL Flight Compartment REV 1, Jan 13/03 AIRSPEED LIMITS PLACARD (TYPICAL) 18 MULTIFUNCTION DISPLAY 18 PRIMARY FLIGHT DISPLAY 18 Indicates Chapter in which information on item may be found. Copilot s Instrument Panel <1015, 2217> Figure

18 Flight Compartment Vol REV 3, May 03/ LEGEND 1. Air conditioning system gasper Lighting panel Stall protection panel Windshield wiper control panel Display reversionary panel Air data reference panel Display control panel Clock. 12 Indicates Chapter in which information on item may be found. Copilot s Side Panel <2040> Figure

19 Vol Flight Compartment Sep 09/02 AUDIO WARNING DISABLE 2 HEADPHONE (HDPH) MICROPHONE (MIC) JACKS 5 OXYGEN MASK REGULATOR STORAGE COMPARTMENT 9 AIR--CONDITIONING SYSTEM OUTLET AIR--CONDITIONING SYSTEM INTAKE FLIGHT BAG COMPARTMENT Indicates Chapter in which information on item may be found. Copilot s Side Console <1205> Figure

20 Flight Compartment Vol Sep 09/02 STABILIZER TRIM LEVER SWITCHES (BLACK) 11 A B AUTOPILOT/STICK PUSHER DISCONNECT SWITCH (RED) 3 11 INTERCOM/ RADIO TRANSMIT SWITCH (BLACK) 5 Pilot s Control Wheel (Copilot s Opposite) FLIGHT DIRECTOR SYNC CONTROL SWITCH (BLACK) 3 STABILIZER TRIM DISCONNECT SWITCH (RED) 11 A TOP VIEW B REAR VIEW Indicates Chapter in which information on item may be found. Control Wheels Figure

21 Vol AIRPLANE GENERAL Flight Compartment REV 3, May 03/05 1. REINFORCED FLIGHT COMPARTMENT DOOR <1226> A. General The reinforced flight compartment door is installed to enhance aircraft security. The door is used to protect the flight crew from ballistic threat and to prevent unauthorized access to the flight compartment. The door is made from Nomex core panels sandwiched in the middle with a bullet proof insert. The door consists of: (1) Slide latch (2) Deadbolt assembly with key lock (3) Two quick--release hinge pins (4) Two decompression panels release latches (5) Cabin viewer (6) Strap handles B. Operation The slide latch is used to latch and unlatch the door The deadbolt assembly is used securely lock the door. To lock or unlock the door from inside the flight compartment, the deadbolt knob is manually rotated to engage the deadbolt pin into the flight compartment bulkhead. A key is required to lock or unlock the door from the passenger compartment. The door is hinged to the galley bulkhead. The door opens towards the passenger compartment and can be held open with a door retainer on the galley wall. The two quick--release pins are used to remove the door from inside the flight compartment and the strap handles are used to lift the door out of the way. The bullet proof viewer has two lenses to increase the magnification for field of view. The decompression panels are hinged on the door and held closed by the pressure release latches. When the pressure differential between the passenger compartment and the flight compartment exceeds a preset limit, the latches release to allow both panels to open. This is done to equalize the pressure between the two compartment. At any time during the flight, if one of the required flight crew leaves the flight compartment, another crew member must replace him/her in the flight compartment to ensure that the required crew member is not locked out of the flight compartment.

22 Flight Compartment Vol REV 3, May 03/05 B A HINGE ASSEMBLY UPPER DECOMPRESSION PANEL VIEWER (PEEPHOLE ASSEMBLY) COCKPIT DOOR MAIN DEADBOLT LATCH DEADBOLT ASSEMBLY POCKET ENCLOSURE LOWER DECOMPRESSION PANEL HINGE ASSEMBLY Reinforced Flight Compartment Door Figure A

23 Vol AIRPLANE GENERAL Flight Compartment REV 3, May 03/05 C. Evacuation If the latch has failed or if the door has jammed, the following steps are used to remove the door in an emergency WARNING The lower door hinge pin must be released before the upper hinge pin. Failure to do so could result in the door suddenly coming disengaged from the hinges causing injury to persons. From inside the flight compartment: (1) Unlock and lift lower hinge pin. (2) Unlock and pull down upper hinge pin. (3) Remove the door by forcibly pushing it out at the hinge side. (4) Rotate door clockwise and stow against the galley. From the passenger compartment: In the event that the flight crew becomes trapped in the flight compartment or becomes incapacitated, it has been demonstrated that rescue personnel can remove the door using normally available, non-powered, hand carried, rescue tools (e. g., crowbar, axe, etc.).

24 Flight Compartment Vol REV 3, May 03/05 UPPER HINGE HANDLE PRESSURE RELEASE LATCH RETRACTABLE BOLTS STRAP HANDLE NAMEPLATE LATCH STRAP HANDLE DEADBOLT LOWER HINGE HANDLE PRESSURE RELEASE LATCH Reinforced Flight Compartment Door --- Placards Figure B