CRJ-00 and 00-Airplane General

01--20--1Vol. 1AIRPLANE GENERAL

Exterior REV 3, May 03/05

Flight Crew Operating ManualCSP C--013--067

External Aircraft Dimensions <2224>Figure 01---20---1

24 ft 1 in(7.34 m)

109 ft 10.8 in (33.50 m)

118 ft 10.7 in (36.24 m)

8 ft 10 in(2.69 m)

28 ft 4 in(8.63 m)

36 ft 4 in(11.07 m)

15 ft 11 in(4.85 m)

6 ft 3 in (1.90 m)

3 ft (0.91 m)

24 ft 1 in(7.34 m)

81 ft 6 in (24.85 m)

10 ft 7 in(3.23 m)

5 ft 1 in (1.55 m)

9 ft 6 in (2.89 m)6 ft 4 in(1.93 m)

7 ft 1 in(2.16 m)


Exterior REV 1, Jan 13/03


Engine Hazard Areas <2224>Figure 01---20---2

100 mph(161 km/h)

60 mph(97 km/h)

7.7 ft(4 m)

140 mph(225 km/h)

140 mph(225 km/h)100 mph

(161 km/h)60 mph

(97 km/h)

12 ft(8 m)

LEGEND

Maximum thrust

Idle thrust

ENGINE EXHAUSTDANGER AREA WIDTH

TEMP. VELOCITY

IDLE 25 ft (8 m) 21 ft (6 m)

TAKE--OFF 37 ft (11 m) 36 ft (11 m)

(3)(6)(9.1)(12.2)(15.2 m)(18.3)(21.3)(24.4)(27.4)(30.5 m)

(0 m)10203040

50 ft60708090

100 ft

0 ft(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)

(0 m)10203040

50 ft60708090

100 ft110120130140

150 ft160170180190

200 ft210220230240

250 ft260270280290

0 ft




Taxiing and Turning RadiiFigure 01---20---3

NOTE

Maximum steeringSymmetrical and idle thrustNo differential braking80 degree steering angleSlip of 3 degreesDry runwaySlow continuous turnMaximum airplane weightAft center of gravity

R6R4

R5

R3

R2NOSE WHEELANGLE

R1

147.1389.7059.1139.1524.3212.244.69

44.8527.3418.0211.937.413.731.43

163.55106.1075.5355.5740.7428.6521.10

166.24114.0188.9174.7766.2761.1759.05

167.93116.8592.7579.4571.6166.9965.08

177.70124.4197.9882.2972.0264.9661.35

49.8532.3423.0216.9412.428.736.43

50.6734.7527.1022.7920.2018.6418.00

51.1935.6228.2724.2221.8320.4219.84

54.1637.9229.8625.0821.9519.8018.70

197.18139.76109.3089.4974.8563.0054.84

60.1042.5933.3127.2722.8119.2016.71

ft m ft ft ft ftm m m mft mR1 R2 R3 R5 R6R4ANGLE

TURNING RADII FOR VARIOUS NOSE WHEELANGLES


Exterior Sep 09/02


Airplane Service Points <2224>Figure 01---20---4

GROUNDPOWER

EXTERNALSERVICES

ADG

ADGPUMP

OXYGENREFILL

FORWARDLAVATORYWASTE DRAIN

FORWARDPOTABLEWATER

AFT LAVATORYWASTE DRAIN

HYDRAULICSYSTEM 3

SINGLE POINTREFUEL/DEFUEL

REFUELDEFUELCONTROLPANEL

APU

HYDRAULICSYSTEMS 1 & 2

GROUND AIRCONDITIONING AIR

BRAKEACCUMULATORS

LAVATORYPOTABLE WATER

OVERWING GRAVITYFUEL FILLER

OVERWING GRAVITYFUEL FILLER

ENGINE STARTHIGH PRESSURE AIR


Exterior REV 1, Jan 13/03


Airplane Mooring PointsFigure 01---20---5

WS111.23

FS278.00 FS819.25 FS1163.11

JACKINGPOINT

MOORINGADAPTERPLATE

JACKINGPAD

NYLONPLUG

NYLONPLUG

MOORINGPOINT

MOORINGTIE--DOWNRING

WL29.31




Airplane Antenna Locations <1045, 1027,1212>Figure 01---20---6

WEATHERRADAR

GLIDESLOPE

VOR ANDLOCALIZER(BOTH SIDES)

EMERGENCYLOCATORTRANSMITTER(OTHER SIDE)

MARKERBEACON

RADIOALTIMETER

Radar hazard areais 2 ft (0.6 m)from antenna withradome closed.

NOTE

GPS 2

DME 1(DME 2OTHER SIDE)

GPS 1

VHF 2

ATC 2(ATC 1OTHER SIDE)

TCAS OMNIDIRECTIONAL

TCASDIRECTIONAL

ATC 1(ATC 2OTHER SIDE)

VHF 1

UNDERWATERLOCATORBEACONS(CVR AND FDR)

2ND RADIOALTIMETER

ADF

01--30--1Vol. 1AIRPLANE GENERALFlight Compartment REV 1, Jan 13/03


Flight Compartment Panel LayoutFigure 01---30---1

OVERHEAD PANEL CENTERINSTRUMENTPANEL

COPILOT’SINSTRUMENTPANEL

COPILOT’SSIDE CONSOLE

PILOT’SINSTRUMENTPANEL

PILOT’SSIDE CONSOLE

CENTER PEDESTAL

GLARESHIELD

PILOT’SSIDE PANEL

COPILOT’SSIDE PANEL

01--30--2Vol. 1AIRPLANE GENERALFlight Compartment Sep 09/02


Pilot’s Side Console <1205>Figure 01---30---2

N100%PUSH

PRESSTOTESTAND

RESET

OXYGENMASK

Indicates Chapter in which information on item may be found.

AIR--CONDITIONINGSYSTEM INTAKE

FLIGHT BAGCOMPARTMENT

HDPH/ MIC

16NOSE WHEELSTEERING TILLER

OXYGEN MASKREGULATOR STORAGECOMPARTMENT

9

AIR--CONDITIONINGSYSTEM OUTLET

HEADPHONE (HDPH)MICROPHONE (MIC)JACKS 5

01--30--3Vol. 1AIRPLANE GENERALFlight Compartment REV 3, May 03/05


Pilot’s Side Panel <2040>Figure 01---30---3


1

2

3

4

7

6

98

5

1. Clock.2. Display control panel.3. Air data reference panel.4. Display reversionary panel.5. Stall protection panel.

LEGEND6. Windshield wiper control panel.7. Lighting panel.8. Nose wheel steering subpanel.9. Air conditioning system gasper.

12 18

12 182

11

15

1716

8

12



Pilot’s Instrument Panel <1015, 2217>Figure 01---30---4

Indicates chapter in which information on item may be found.

MULTIFUNCTIONDISPLAY

COCKPIT VOICERECORDER

ERASEHEADSET

HOLD5 SEC

TEST

COCKPIT VOICERECORDER (CVR)CONTROL UNIT

5

PRIMARY FLIGHTDISPLAY

AIRSPEED LIMITSPLACARD (TYP)

18

18



Centre Instrument Panel <1001>Figure 01---30---5

STANDBYINSTRUMENT


EICAS SECONDARYDISPLAY

ENGINE INDICATION AND CREW ALERTINGSYSTEM (EICAS) PRIMARY DISPLAY

2

12

RAM AIR OPEN

2



Overhead Panel <1020><1201>Figure 01---30---6


19

8

10

11

12

13

1 2

3

4

5

6

714

15

17

16

18

20 21

9

LEGEND1. Cabin pressurization panel.2. Copilot’s dome light control.3. Air--conditioning panel.4. Anti--ice panel.5. Engine / ignition panel.6. Miscellaneous lights panel.7. Hydraulic pump panel.8. Emergency lights panel.9. Passenger signs panel.10. Passenger oxygen control. 9

117

1417

2015

817

11. Standby compass.12. Emergency locator transmitter control.13. Landing lights panel.14. External lights panel.15. Hydraulic shutoff panel.16. APU panel.17. Fire detection / FIREX monitor panel.18. Pilot’s dome light control.19. Electrical panel.20. Bleed air panel.21. Fuel panel.

12

1717

144

177

1913

9

10

8



Glareshield <2040>Figure 01---30---7

Right Glareshield

Indicates chapter in which information on item may be found.

Left Glareshield

Center Glareshield

12 3 4 5 6

7

9 6

5

12

34

8

7 7

LEGEND1. Roll select.2. Master warning.3. Master caution.4. Stall warning.5. GPWS and glideslope warning.

11

112

2

18

6. Engine fire warning.7. Firex bottle discharge.8. Flight control panel.9. APU fire warning. 10

310

10



Centre Pedestal (Upper) <2040, 1214>Figure 01---30---8


1

34

1. Landing gear control panel.2. Flight management system control display unit.3. Interphone panel.4. Engine / miscellaneous test panel.5. Ground proximity warning panel.

16

5

1820 2 17

18

LEGEND

5 22



Center Pedestal --- Thrust Lever and Flight Controls <1029, 2040>Figure 01---30---9


41 3

8

2

57 6

LEGEND1. Spoilers system control subpanel.2. Pitch disconnect control.3. Flight spoiler lever.4. Roll disconnect control.5. Slat/ flap lever6. Metric altimeter subpanel.7. Thrust lever quadrant.8. Thrust reverser subpanel.

2020

1211

11

11

1111



Centre Pedestal (Lower) <1012, 1025,>Figure 01---30---10


LEGEND11. Emergency flap deploy control.12. Air driven generator -- auto--deploy panel.13. Air driven generator -- manual deploy handle.14. Landing gear -- manual release handle.15. Parking brake handle.16. Compass control panel (on both sides).16A. <1025> IRS mode select unit.17. Avionics cooling control panel.18. Stabilizer/Mach trim panel.19. Backup tuning unit.

117

716

128

511

16

1. Radio tuning unit.2. EICAS control panel.3. Audio control panel.4. Aileron/rudder trim panel.5. Lighting panel.6. Weather radar control panel.7. Yaw damper panel.8. Interphone control panel.9. Source selector panel.10. Cargo firex panel.

5

10

1118

18

52

5 18

17

11

2 12

12

2

1

3

45

6

7

8

9

10

11

121314

15

16

17

18

19

6

3

1

3

16A



Copilot’s Instrument Panel <1015, 2217>Figure 01---30---11


MULTIFUNCTIONDISPLAY

PRIMARY FLIGHTDISPLAY

AIRSPEED LIMITSPLACARD (TYPICAL)

1818

18



Copilot’s Side Panel <2040>Figure 01---30---12


8

7

6

5

2

3

1

4

1. Air conditioning system gasper.2. Lighting panel.3. Stall protection panel.4. Windshield wiper control panel.5. Display reversionary panel.6. Air data reference panel.7. Display control panel.8. Clock. 12

2

181212 18

8

1115

17

LEGEND



Copilot’s Side Console <1205>Figure 01---30---13


OXYGEN MASKREGULATOR STORAGECOMPARTMENT

FLIGHT BAGCOMPARTMENT

9

AUDIO WARNINGDISABLE 2

AIR--CONDITIONINGSYSTEM INTAKE

HEADPHONE (HDPH)MICROPHONE (MIC)JACKS 5

AIR--CONDITIONINGSYSTEM OUTLET



Control WheelsFigure 01---30---14

STABILIZER TRIMDISCONNECTSWITCH (RED)

INTERCOM/RADIO TRANSMITSWITCH (BLACK)

STABILIZER TRIMLEVER SWITCHES(BLACK)

AUTOPILOT/STICKPUSHER DISCONNECTSWITCH (RED)

FLIGHT DIRECTORSYNC CONTROLSWITCH (BLACK)

Pilot’s Control Wheel(Copilot’s Opposite)

REAR VIEW

TOP VIEW


113

11

3

5

11

B

A

B

A



1. REINFORCED FLIGHT COMPARTMENT DOOR <1226>

A. General

The reinforced flight compartment door is installed to enhance aircraft security. Thedoor is used to protect the flight crew from ballistic threat and to prevent unauthorizedaccess to the flight compartment. The door is made from Nomex core panelssandwiched 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 frominside the flight compartment, the deadbolt knob is manually rotated to engage thedeadbolt pin into the flight compartment bulkhead. A key is required to lock or unlockthe door from the passenger compartment.

The door is hinged to the galley bulkhead. The door opens towards the passengercompartment and can be held open with a door retainer on the galley wall. The twoquick--release pins are used to remove the door from inside the flight compartment andthe 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 pressurerelease latches. When the pressure differential between the passenger compartmentand the flight compartment exceeds a preset limit, the latches release to allow bothpanels 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 flightcompartment, another crew member must replace him/her in the flight compartment toensure that the required crew member is not locked out of the flight compartment.



Reinforced Flight Compartment DoorFigure 01---30---15

HINGE ASSEMBLY

COCKPIT DOOR

HINGE ASSEMBLY

UPPERDECOMPRESSIONPANEL

LOWERDECOMPRESSIONPANEL

MAINDEADBOLTLATCH

DEADBOLTASSEMBLY

VIEWER(PEEPHOLEASSEMBLY)

POCKETENCLOSURE

A

AB



C. Evacuation

If the latch has failed or if the door has jammed, the following steps are used to removethe door in an emergency

WARNING

The lower door hinge pin must be released before theupper hinge pin. Failure to do so could result in thedoor suddenly coming disengaged from the hingescausing 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 becomesincapacitated, it has been demonstrated that rescue personnel can remove the doorusing normally available, non-powered, hand carried, rescue tools (e. g. , crowbar, axe,etc.).



Reinforced Flight Compartment Door --- PlacardsFigure 01---30---16

B

PRESSURERELEASELATCH

UPPER HINGEHANDLE

RETRACTABLEBOLTS

LATCH

DEADBOLT

NAMEPLATE

STRAPHANDLE

STRAPHANDLE

LOWER HINGEHANDLE PRESSURE

RELEASELATCH

Documents

CRJ-00 and 00-Airplane General