CRJ700/900 Technical Familiarization Manual - ANTN … · INDEX Chapter AG - Aircraft General Chapter 21 - Air Conditioning Chapter 22 - Autoflight Chapter 23 - Communication Chapter

FOR 1 June 2005

CSP B-026

AL

TRAINING PURPOSES ONLY

TECHNICAL FAMILIARIZATION MANU

FOR 1 June 2005

erved.

rjet Inc., prietary n of the . Public orporate thereof, ervices,

d other r in part ential to patent, therein ntation,

reverse olely for

TRAINING PURPOSES ONLY

Copyright © 1999 - 2005 Bombardier Inc. or its subsidiaries. All rights res

Bombardier Inc., by its groups, divisions or its corporate subsidiary Leaprovides this information to the government in confidence. This is proconfidential information, which we consider excluded from the applicatioAccess to information Act and may also be a trade secret of our companyrelease of this information would be harmful to Bombardier Inc. or its csubsidiary Learjet Inc. Any intention to disclose such information, or partmust be indicated in advance and in writing to the Vice-President Legal SCorporate Office.

It is understood that this documentation, comprising technical data aninformation in any media shall not be reproduced or disclosed in whole owithout Bombardier's written authorization, and is proprietary and confidBombardier or its corporate subsidiary Learjet Inc. and that all rights andcopyright, trademark, trade secret and other intellectual property rightsbelong to Bombardier or its corporate subsidiary Learjet Inc. Such documetechnical data and other information shall not be modified, translated,assembled, reverse engineered or decompiled and shall be used straining purposes only.

INDEX

Chapter AG - Aircraft GeneralChapter 21 - Air ConditioningChapter 22 - AutoflightChapter 23 - CommunicationChapter 24 - Electrical PowerChapter 26 - Fire ProtectionChapter 27 - Flight ControlsChapter 28 - FuelChapter 29 - Hydraulic Power Chapter 30 - Ice & Rain ProtectionChapter 31 - Indicating & RecordingChapter 32 - Landing GearChapter 33 - LightsChapter 34 - NavigationChapter 35 - OxygenChapter 36 - PneumaticsChapter 38 - Water & Waste Chapter 45 - Maintenance DiagnosticsChapter 49 - Auxiliary Power UnitChapter 52 - Doors Chapter 56 - WindowsChapter 70 - Powerplant

TECHNICAL TRAINING MANUAL

01 - AIRCRAFT GENERALCopyrigh 1 June 2005

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DESIGNINTR

AIRFRASERVICBAGGA

AFT

FOR

AVIO

FLIGHTPASSE

PASS

FLIG

GALL

CLOS

LAVA

EME

t © Bombardier Inc. For Training Purposes Only

TABLE OF CONTENTS

FEATURES..........................................................2ODUCTION ............................................................................2

ME STRUCTURE ..................................................8ING/TOWING/TAXIING.......................................10GE/CARGO & EQUIPMENT COMPARTMENTS 18

CARGO/BAGGAGE COMPARTMENT ................................18

WARD BAGGAGE COMPARTMENT ..................................19

NICS EQUIPMENT COMPARTMENTS ..............................21

COMPARTMENT................................................24NGER COMPARTMENT ......................................34ENGER SEATS ..................................................................34

HT ATTENDANT SEATS .....................................................36

EY COMPARTMENTS ........................................................37

ETS AND PARTITIONS .....................................................39

TORY ..................................................................................41

RGENCY EQUIPMENT ........................................................42


01 - AIRCRAFT GENERAL1 June 2005

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Copyright © Bombardier Inc. For Training Purposes Only
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01 - AIRCRAFT GENERALCo 1 June 2005

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pyright © Bombardier Inc. For Training Purposes Only
AIRCRAFT GENERAL



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RJ900 AND CRJ705is the first variant of the CRJ200.ude but are not limited to a longer engines, a new wing with leadingargo compartment, and upgradeds. This aircraft is marketed as theJ701 (70 seats) and the CRJ702 (77ndard or extended range version.

s the second variant of the CRJ200.pared to the CRJ200 series aircraft) a longer fuselage, FADEC-controlledleading edge slats, a forward cargod automated aircraft systems. ThisCRJ900 (up to 90 seats). It, too, isnded range versions. landing performance improvementsnce improvements consisted of a

ger winglets, software changes, new added selection of Flap 20, and an

the third CRJ200 variant. This variantd CL-600-2D24 series 900 aircraftd for a maximum of 75 passengers

705 (75 seats).


DESIGN FEATURES

INTRODUCTIONThe CRJ700 series and CRJ900 series regional jet aircraft aredesigned for the short- to medium-range airline markets. Themodel designator for these aircraft are as follows:• CRJ700: CL-600-2C10

• CRJ900: CL-600-2D24

• CRJ705: CL-600-2D15

General features of the CRJ700, CRJ900 and CRJ705 aircraftinclude:• Quiet, fuel efficient, high bypass turbofan engines.

• State-of-the-art avionics system featuring six ‘glass’ displays,digital data communications and an advanced maintenancediagnostic system.

• Advanced technology wings with polished leading edge slats.

• Modern airframe structure with composite material used innon-structural areas.

• Class C forward and aft cargo compartments with convenientexternal access.

• Wide fuselage with 4 abreast seating.

• Several configuration options for location of lavatories andgalley.

• Flexible cabin layout options including mixed seat-pitch andtwo class interiors.

HISTORY OF CRJ700, CThe CL-600-2C10 aircraft Product improvements inclfuselage, FADEC-controllededge slats, a forward cautomated aircraft systemCRJ700 (68 seats), the CRseats). It is available in a staThe CL-600-2D24 aircraft iProduct improvements (cominclude but are not limited toengines, a new wing with compartment, and upgradeaircraft is marketed as the available in standard or exteLater, short field takeoff andwere introduced. Performalarger wingspan due to bigslat/flap relationship with anoptional long range version.The CL-600-2D15 aircraft isis identical to the improveexcept that it is only certifieand is marketed as the CRJ



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GThsera

/900ER CRJ705/900 LR

M(

500 lb 421 kg)

84,500 lb(38,329 kg)

M g) 75,100 lb(34,065 kg)

M(

R 06 nm 60 km)

1940 nm (3593 km)

M

S 5, up to 90 - CRJ900


ENERAL AIRCRAFT DATAe following table provides a general comparison of the CRJ700ries and CRJ705/900 series aircraft, as well as the extendednge (ER) and long range (LR) model configurations.

CRJ700 CRJ700ER CRJ705/900 CRJ705

aximum Take-off Weight MTOW)

72,750 lb (33,000 kg)

75,000 lb (34,019 kg)

80,500 lb (36,514 kg)

82,(37,

aximum Landing Weight (MLW) 67,000 lb (30,391 kg) 73,500 lb (33,340 k

aximum Usable Fuel@ 6.75 lbs/US gallon) 19,595 lb (8,888 kg)

ange (@ Mach 0.74) 1685 nm (3121 km)

1985 nm (3767 km)

1479 nm (2739 km)

17(31

aximum Operating Altitude 41,000 ft (12,500 m)

tandard Seating Capacity 68 to 78 74 or 75 - CRJ70



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ain Wheel Track Nose to Main

ft, 6 in11 m

37 ft, 5 in11.43 m

ft, 6 in11 m

48 ft, 4 in14.73 m

ft, 6 in11 m

48 ft, 4 in14.73 m


AIRCRAFT DIMENSIONSThe following table offers quick reference to dimensionaldifferences between the aircraft series.

FIGURE 1 - CABIN CROSS SECTION

Length Wingspan Tailspan Height M

CRJ700 106 ft, 8 in32.51 m

76 ft, 3 in23.25 m

28 ft8.53 m

24 ft, 10 in7.57 m

134.

CRJ705 119 ft, 4 in36.4 m

81 ft, 7 in24.9 m

28 ft8.53 m

24 ft, 7 in7.5 m

134.

CRJ900 119 ft, 4 in36.4 m

76 ft, 3 in23.25 m

28 ft8.53 m

24 ft, 7 in7.5 m

134.



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28 ft(8.54 m)


FIGURE 2 - AIRCRAFT DIMENSIONS - CRJ700

76 ft, 3 in. (23.25 m)

13 ft, 6 in.(4.11 m)

43 ft, 8 in(13.31 m)

.

24 ft, 10 in.(7.57 m)

49 ft, 3 in. (15.01 m)

106 ft, 8 in. (32.51 m)

CR7/AG-09-00-0003/CGM



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28 ft.(8.54 m)


FIGURE 3 - AIRCRAFT DIMENSIONS - CRJ705/900

56 ft, 9 in. (17.29 m)

118 ft, 11 in. (36.4 m)

13 ft, 6 in.(4.11 m)

81 ft, 7 in. (24.87 m)

51 ft, 2 in.(15.60 m)

7 ft, 6 in.(2.29 m)

5 ft.(1.58 m)

24 ft.(7.31 m)

CR9/AG-09-00-0002/CGM



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rake is not installed on the aircraft,alled on the base of the fuselage. Thestiffness of the aircraft. Relative to theset the effects of the fuselage stretchthe fuselage upper strake.

an all-metal structure consisting of aluminum alloy planks with integralribs and a central box structure.

let is installed which increases the

vides structural support for the mainain landing gear retracts into the aft

tructure. The wing has provisions forlats, two-section slotted flaps, groundspoilers and space for fuel storage.fully-cantilevered, swept-back designl stabilizer mounted on the top edge. wing, slats, vertical and horizontaling aluminum alloy.ed in the aircraft secondary structurests, belly fairings, landing gear doors.


AIRFRAME STRUCTURE

The fuselage is a semi-monocoque, all-metal, damage-tolerantstructure, using an aluminum alloy, chemically milled skin withriveted stringers and frames.The forward fuselage contains the radome, flight compartment,forward pressure bulkhead, forward avionics bay, main passengerentrance and support mountings for the nose landing gear.The center fuselage contains the passenger compartment, mainavionics bay, forward cargo compartment, and the structural wingattachment.

CRJ705/900: a 90 in (229 cm) structural plug is installed forwardof the wing box on the center fuselage section.

The rear fuselage contains the pylon structure, rear pressurebulkhead, cargo compartment, support structure for the verticalstabilizer, the aft equipment bay and tail cone.

CRJ705/900: a 62 in (157.5 cm) structural plug is installed aft ofthe wing box on the center fuselage section.

Two pressure bulkheads and a pressure floor make the mid-center fuselage ‘D’ shaped. This provides an area external to thepressure zone where the wing attaches to the fuselage.

CRJ705/900: has a reinforced wing.

CRJ700: a dorsal strake is installed on top of the fuselage of theCRJ700 to make an aerodynamic transition between the top ofthe fuselage and the leading edge of the vertical stabilizer.

CRJ705/900: the dorsal sthowever ventral fins are instfins increase the directional CRJ700, the ventral fins offand eliminates the need for

The single piece wing is machined upper and lowerstringers covering the spar,

CRJ705/900: a new wingwingspan by 5 ft, 4 in.

The auxiliary rear spar prolanding gear trunnion. The msection of the center box sthe installation of ailerons, sspoilers, multifunction flight The vertical stabilizer is a with a swept-back horizontaThe leading edges of thestabilizers are fabricated usComposite materials are ussuch as the radome, wingleand empennage top fairings



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VERTICAL STABILIZERTIP FAIRING

ER

INGTURE

TAIL CONE

PYLONTRAILING EDGESTRUCTURE

CORE COWL

FAN COWLDOORS

LIPSKIN

PRIMARY STRUCTURE

SECONDARY STRUCTURE

ING TRAILINGGE STRUCTURE


FIGURE 4 - GENERAL CONSTRUCTION

MAINLANDINGGEAR

WING TOFUSELAGEFAIRINGS

NOSE LANDINGGEAR DOORS

RADOME

WING LEADINGEDGE SLATS

FLAP FAIRINGS

HORIZONTAL STABILIZTIP STRUCTURE

DORSALFAIRING

RAM AIRINLET DUCT

DORSAL STRAKE(CRJ700 ONLY)

PYLON LEADEDGE STRUC

WING TOFUSELAGEFAIRINGS

VERTICAL STABILIZERLEADING EDGESTRUCTURE

CR7/AG-51-00-0001/CGM

WINGLET

The wing trailing edge primary structureincludes the support structure for theflaps, ailerons and spoilers.

1

VENTRAL FINS(CRJ705/900)

WED

1

PLUGS(CRJ705/900)



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SERVICING / TOWING / TAXIING

Typical aircraft servicing includes general replenishing ofconsumables as well as scheduled and unscheduled servicing.The aircraft is normally controlled by using a nosewheel steeringsystem. The aircraft can also be controlled without the steeringsystem by the use of differential thrust and braking. Themaximum steering limit when taxiing is 80° either left or right sideof center.The aircraft can be pushed or towed with the tow bar connectedto the axle of the nose landing gear (NLG). The steering torquearms may be connected or disconnected depending on towingequipment used. The nosewheel steering system switch must beselected OFF before towing. An approved tow-barless towingvehicle may also be used.A dual pin quick disconnect mechanism, integral to the uppertorque arm, connects the upper and lower torque arms.The recommended steering angle limit when towing is 70° eitherside of center with torque arm connected or disconnected.Disconnection isolates the steering collar and the steeringactuators, preventing damage to the steering actuator system.When disconnected, the spring-loaded torque arms separate androtate into a safe fixed position to maintain its position clear of thenose wheels and the aft door during towing.Landing gear lock pins must be installed when the aircraft is onground. Grounding lugs or receptacles are installed at landinggear, wing and refueling panel locations.



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ATORYABLE WATER

ENGINE STARTHIGH-PRESSURE AIR

ENGINE OILSERVICING


FIGURE 5 - AIRCRAFT SERVICING LOCATIONS

BRAKEACCUMULATORS

LAVPOT

APU

#1 & #2HYDRAULICSYSTEMS

GROUND AIR CONDITIONING AIR

AFT LAVATORYWASTE DRAIN

#3 HYDRAULICSYSTEM

SINGLE-POINTREFUEL/DEFUEL

REFUEL / DEFUELCONTROL PANEL

FORWARDLAVATORYWASTE DRAIN

FORWARDPOTABLEWATER

GROUNDPOWER

EXTERNALSERVICES

ADG

ADG PUMP

OXYGENREFILL

OVERWING GRAVITYFUEL FILLER

OVERWING GRAVITYFUEL FILLER

CR7/52-45-00-0001/CGM



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QUICK-DISCONNECTMECHANISM

AXLEENGAGEMENTPIN

UPPER TORQUE LINK (ARM)

LOWER TORQUE LINK (ARM)


FIGURE 6 - TOW BAR / TOW-BARLESS TOWING

METAL EYE

TOW BARLESS TOWING

TOW BARTOW BAR

CR7/AG-09-00-0001/CGM



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118 ft.(35.9 m)


FIGURE 7 - TURNING RADIUS - CRJ700

MAXIMUM TAXIINGANGLE 80°

MAXIMUM TOWINGANGLE 70°

48 ft, 5 in.(14.75 m)

55 ft, 3 in.(16.84 m)

57 ft.(17.61m)

49 ft, 7 in.(15.11 m)

CR7/AG-09-00-0002/CGM

TURNINGCENTERS

• MAXIMUM TOWING / TURNING RADIUS WITH TORQUE ARMS CONNECTED OR DISCONNECTED• TURNING RADII SHOWN REPRESENTS THE THEORETICAL GEOMETRIC TURNING CENTERS• TOWING BASED ON MAXIMUM AIRCRAFT WEIGHT



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126 ft, 5 in.(38.2 m)


FIGURE 8 - TURNING RADIUS - CRJ705/900CR9/AG-09-00-0001/CGM

TURNINGCENTERS

61 ft, 4 in.(18.7 m)

65 ft.(19.8 m)

59 ft. (18 m)

55 ft, 3 in.(16.84 m)

21 ft.(6.4 m)

• MAXIMUM TOWING / TURNING RADIUS WITH TORQUE ARMS CONNECTED OR DISCONNECTED• TURNING RADII SHOWN REPRESENTS THE THEORETICAL GEOMETRIC TURNING CENTERS• TOWING BASED ON MAXIMUM AIRCRAFT WEIGHT

MAXIMUM TAXIINGANGLE 80°

MAXIMUM TOWINGANGLE 70°



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FIGURE 9 - MAIN AND NOSE GEAR LOCKPIN LOCATIONSCR7/AG-10-20-0008/CGM



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UND LUGERE)


FIGURE 10 - AIRCRAFT GROUNDING

GRO(H

CR7/AG-10-20-0002/CGM

ALLIGATORCLAMP

GROUNDINGLUG

GROUND STUDRECEPTACLE

GROUNDSTUD

GROUNDINGLUG



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CARGO COMPARTMENT

S992.00

FS959.50 CARGOLINERS

BULKHEAD

CARGOLINERS

OUTERSKIN


BAGGAGE / CARGO AND EQUIPMENT COMPARTMENTS

The aircraft is provided with a forward and aft class C cargo orbaggage compartment with access by manually operated doorson the left side of the fuselage. An underfloor compartment holdsventilated equipment racks on the left and right sides with a lowerfuselage access door along the fuselage centerline.

AFT CARGO / BAGGAGE COMPARTMENTThe aft cargo compartment provides sufficient space for thestorage of cargo and passenger baggage.A restraint net is installed across the cargo door entrance toprevent baggage from blocking the door if shifting occurs duringflight.The cargo compartment has two smoke detectors and a fireextinguishing system installed on the cargo compartment liners.

FIGURE 11 - AFT

FS1096.08

FOUTERSKIN

CARGO DOORRESTRAINT NETTING

BULKHEADLINERS

CR7/25-50-00-0005/CGM


21 - Air ConditioningCopyrigh 1 June 2005

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INTRODCONTR

AIR CCON

AIR C

CABI

AVIO

GALL

EICA

DISTRIFLIG

PASS

VENT

GALL

AVIO

AFT

COOLINFLOW

RAM

AIR C

TEMPE PRESS


TABLE OF CONTENTS

UCTION ................................................................2OLLERS / PANELS / DISPLAYS ...........................3ONDITIONING SYSTEM/CABIN PRESSURE

TROLLERS ............................................................................3

ONDITIONING CONTROL PANEL ...................................... 4

N PRESSURE CONTROL PANEL........................................ 5

NICS COOLING PANEL........................................................ 6

EY PANEL ............................................................................6

S ECS INDICATIONS............................................................ 7

BUTION...................................................................8HT COMPARTMENT DISTRIBUTION .................................10

ENGER COMPARTMENT DISTRIBUTION ....................... 11

ILATION.............................................................................. 12

EY HEATING ......................................................................12

NICS EQUIPMENT/DISPLAY COOLING ............................14

CARGO COMPARTMENT CONDITIONED AIR ..................16

G .........................................................................18 CONTROL AND PRE-COOLER .......................................20

AIR SYSTEM ......................................................................20

ONDITIONING UNITS (PACKS) ........................................22

RATURE CONTROL ............................................24URIZATION CONTROL.......................................26


21 - Air Conditioning1 June 2005

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22 - AutoflightCopyrigh 1 June 2005

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INTRODCOM

INTEGRFLIGHT

FLIG

AUTOPYAW DFCC DI

REPO

INPU

OUT


TABLE OF CONTENTS

UCTION ................................................................2PONENTS ............................................................................. 3

ATED AVIONICS PROCESSOR...........................7 DIRECTOR ...........................................................8HT DIRECTOR MODES ...................................................... 10

ILOT......................................................................12AMPER SYSTEM..................................................14AGNOSTICS.........................................................16

RT MODE ..........................................................................16

T MODE ...............................................................................16

PUT MODE ...........................................................................16


22 - Autoflight1 June 2005

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23 - CommunicationCopyrigh 1 June 2005

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INTRODAUDIO

AUD

AUD

MAIN

MEC

RAD

MICR

SPEA

PASSEPASSEINTEGR

RAD

STAN

RTU

FMS

VHF COSELECHF COMCOCKPARINC REPOR


TABLE OF CONTENTS

UCTION ................................................................2INTEGRATING SYSTEM .......................................3IO ELECTRONICS CONTROL UNIT .....................................3

IO CONTROL PANEL ............................................................ 4

TENANCE INTERPHONE UNITS......................................... 5

HANIC CALL SWITCH/LIGHTS .............................................5

IO TRANSMIT / INTERCOM SWITCH ...................................5

OPHONES ............................................................................5

KERS ....................................................................................5

NGER ADDRESS AND CABIN INTERPHONE .....7NGER BRIEFING SYSTEM....................................9ATED AUTOMATIC TUNING..............................10

IO TUNING UNITS ...............................................................10

DBY TUNING UNIT ............................................................12

INHIBIT PUSH SWITCHES .................................................12

TUNE INHIBIT SWITCH ......................................................12

MMUNICATION SYSTEM...................................13TIVE CALL SYSTEM ............................................15

MUNICATIONS SYSTEM...................................16IT VOICE RECORDER SYSTEM ........................18COMMUNICATIONS ADDRESSING AND TING SYSTEM.....................................................20


23 - Communication1 June 2005

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4 - Electrical Power SystemCopyrigh 1 June 2005

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INTRODCONTRAC POW

INTE

AUXI

AC POWGEN

AC P

AIR D

AC P

AC P

AUTO

AC E

AC S

EXTEREMERG

AIR D

GEN

AUTO

STOW

MAN

UPLO

EJEC

ADG

DC POW

NITS ..........................................26

................................................... 27

DISTRIBUTION ................28................................................... 29

2t © Bombardier Inc. For Training Purposes Only

TABLE OF CONTENTS

UCTION ................................................................2OLS AND INDICATIONS .......................................4ER GENERATION................................................8

GRATED DRIVE GENERATOR ............................................8

LIARY (APU) GENERATOR ................................................10

ER CONTROL AND DISTRIBUTION.................12ERATOR CONTROL UNITS ................................................12

OWER CENTER ..................................................................12

RIVEN GENERATOR POWER CENTER ..........................12

OWER DISTRIBUTION ....................................................... 14

OWER SOURCE SELECTION............................................ 15

TRANSFER INHIBIT .......................................................... 17

SSENTIAL BUS CONTROL ................................................ 18

ERVICE BUS .......................................................................18

NAL AC POWER ..................................................20ENCY AC POWER GENERATION .....................22RIVEN GENERATOR .........................................................22

ERATOR CONTROL UNIT ..................................................22

MATIC DEPLOY CONTROL UNIT ....................................22

PUMP ...............................................................................22

UAL DEPLOYMENT HANDLE .............................................24

CK ASSEMBLY ..................................................................24

TION ACTUATOR ...............................................................24

CONTROL PANEL.............................................................. 25

ER GENERATION .............................................26

TRANSFORMER RECTIFIER U

BATTERIES ..............................

DC POWER CONTROL AND DC BUSES................................


24 - Electrical Power System1 June 2005

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26 - Fire ProtectionCopyrigh 1 June 2005

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INTRODCONTRENGINE

ENG

ENG

ENG

APU FIRAPU

APU

APU

MAIN LCARGO

CAR

CAR

CAR

LAVATOLAVA

LAVA

PORTA


TABLE OF CONTENTS

UCTION ................................................................2OLLERS AND PANELS .........................................4 FIRE PROTECTION ............................................6

INE FIRE DETECTION ..........................................................6

INE FIRE EXTINGUISHING ...................................................7

INE FIRE EXTINGUISHING OPERATION............................. 8

E PROTECTION.................................................10FIRE DETECTION ...............................................................10

FIRE EXTINGUISHING ....................................................... 11

FIRE EXTINGUISHING OPERATION................................. 12

ANDING GEAR OVERHEAT DETECTION ..........14 COMPARTMENT FIRE PROTECTION..............16

GO COMPARTMENT SMOKE DETECTION .......................16

GO COMPARTMENT FIRE EXTINGUISHING ....................17

GO COMPARTMENT FIRE EXTINGUISHING OPERATION18

RY FIRE PROTECTION.....................................20TORY SMOKE DETECTION ..............................................20

TORY WASTE BIN FIRE EXTINGUISHING .......................20

BLE FIRE EXTINGUISHERS ...............................21


26 - Fire Protection1 June 2005

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27 - Flight ControlsCopyrigh 1 June 2005

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INTRODCONTR

SPO

SLAT

STAL

CON

PITC

SPO

SPO

SLAT

STAB

AILE

YAW

EME

STAL

STAL

ROLL

FLIG

AILEROROLL

AILE

RUDDERUD

YAW

RUD

..........................................26ION ...........................................28

....................................................30

RIM CONTROL.................32M ......................................34..........................................36..........................................40


TABLE OF CONTENTS

UCTION ................................................................2OLLERS/PANELS/DISPLAYS ...............................4

ILER/STABILIZER CONTROL UNIT ......................................4

/FLAP ELECTRONIC CONTROL UNIT ................................ 5

L PROTECTION COMPUTER ............................................. 6

TROL WHEEL SWITCHES ....................................................7

H AND ROLL DISCONNECT HANDLES ...............................7

ILER CONTROL PANEL ........................................................7

ILER CONTROL LEVER ........................................................7

/FLAP CONTROL LEVER .....................................................7

ILIZER/MACH TRIM CONTROL PANEL.............................. 8

RON/RUDDER CONTROL PANEL ........................................8

DAMPER CONTROL PANEL ...............................................8

RGENCY FLAP SWITCH .......................................................8

L PROTECTION CONTROL SWITCH.................................. 9

L PROTECTION SWITCH/LIGHT .........................................9

PRIORITY SWITCH/LIGHTS ...............................................9

HT CONTROL INDICATIONS.............................................. 10

N CONTROL........................................................12 DISCONNECT OPERATION .............................................14

RON TRIM OPERATION .....................................................16

R CONTROL........................................................18DER ANTI-JAM OPERATION ..............................................20

DAMPER/RUDDER TRIM OPERATION ............................22

DER TRAVEL LIMITER ........................................................24

ELEVATOR CONTROL ..........PITCH DISCONNECT OPERAT

PITCH FEEL OPERATION ......

HORIZONTAL STABILIZER TSTALL PROTECTION SYSTESPOILER SYSTEM ................SLAT / FLAP SYSTEM...........


27 - Flight Controls1 June 2005

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28 - Fuel SystemCopyrigh 1 June 2005

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INTRODCONTR

FUEL

FUEL

REFU

EICA

FUEL SFUEL

TANK

FUEL LFUEL

FUEL

POW

GRA

FUEL DMOT

ENG

STAN

APU

REFU

FUEL INFUEL

FUEL

FUEL


TABLE OF CONTENTS

UCTION ................................................................2OLLERS / PANELS / DISPLAYS ...........................4 QUANTITY GAUGING COMPUTER ...................................4

CONTROL PANEL............................................................... 5

EL/DEFUEL CONTROL PANEL .......................................... 6

S FUEL INDICATIONS.......................................................... 7

TORAGE ................................................................8 TANKS .................................................................................8

VENTING ...........................................................................10

OAD MANAGEMENT ...........................................12 SCAVENGE .......................................................................12

TRANSFER ........................................................................12

ER CROSS-FLOW ..............................................................14

VITY CROSS-FLOW ............................................................14

ISTRIBUTION ......................................................17IVE FLOW SYSTEM ............................................................17

INE FUEL FEED SYSTEM................................................... 18

DBY FUEL FEED SYSTEM ................................................20

FUEL FEED SYSTEM .........................................................22

EL / DEFUEL SYSTEM ......................................................24

DICATING...........................................................28 QUANTITY GAUGING SYSTEM .......................................28

MAGNETIC LEVEL INDICATORS .....................................30

TEMPERATURE INDICATING ..........................................32


28 - Fuel System1 June 2005

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29 - Hydraulic PowerCopyrigh 1 June 2005

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INTRODCONTR

HYD

HYD

EICA

HYDRAHYD

HYDRAHYD

ACMP CHYDRA


TABLE OF CONTENTS

UCTION ................................................................2OLS AND INDICATIONS .......................................4

RAULIC SHUTOFF VALVE PANEL .......................................4

RAULIC PUMP CONTROL PANEL ........................................4

S INDICATIONS .................................................................... 5

ULIC SYSTEMS NO. 1 AND 2...............................6RAULIC SYSTEMS 1 AND 2 OPERATION ...........................8

ULIC SYSTEM NO. 3 ...........................................10RAULIC SYSTEM NO. 3 OPERATION................................ 12

ONTROL.............................................................14ULIC SYSTEMS GROUND SERVICING .............15


29 - Hydraulic Power1 June 2005

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30 - Ice and Rain ProtectionCopyrigh 1 June 2005

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INTRODCONTR

ANTI

AIR D

WIND

BLEE

ANTI

WIPE

EICA

WING AWING

INLET CICE DEAIR DAANTI-ICWINDSWINDS


TABLE OF CONTENTS

UCTION ................................................................2OLLERS / PANELS / DISPLAYS ...........................4-ICE AND LEAK DETECTION CONTROLLER ......................4

ATA SENSOR HEAT CONTROLLERS................................ 5

SHIELD HEAT CONTROLLERS.......................................... 6

D AIR CONTROL PANEL..................................................... 7

-ICE CONTROL PANEL ........................................................7

R CONTROL PANEL ............................................................7

S ANTI-ICE INDICATIONS.................................................... 8

NTI-ICING SYSTEM............................................10 ANTI-ICE OPERATION .....................................................12

OWL ANTI-ICING SYSTEM................................14TECTION SYSTEM ..............................................16TA PROBES AND SENSORSING SYSTEM.......................................................17

HIELD/WINDOW HEATING SYSTEM..................18HIELD WIPER SYSTEM.......................................20


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INTRODENGINE(EICAS

EICA

CON

EICA

CLOCKFLIGHTQUICK

31 - Indicatit © Bombardier Inc. For Training Purposes Only

TABLE OF CONTENTS

UCTION ................................................................2 INDICATING AND CREW ALERTING SYSTEM

)...............................................................................4S CONTROLLERS ................................................................4

TROL PANELS ......................................................................6

S DISPLAYS.......................................................................... 9

S ...........................................................................16 DATA RECORDING............................................18ACCESS RECORDER .........................................20


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31 - InCopyright © Bombardier Inc. For Training Purposes Only



32 - Landing GearCopyrigh 1 June 2005

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INTRODCONTR

PRO

ANTI

NOS

LAND

ALTE

PARK

EICA

MAIN LNOSE LLANDINSYSTE

LAND

NLG

NLG

MLG

MLG

MLG

LANDINWHEEL

MAIN

NOS

MAIN

PARK

TORING SYSTEM .....................24

ING SYSTEM ............................24

.................................................26

STEM................................28M .....................................30

ONICS UNIT .............................30

ITCHES ..................................32

..........................................34


TABLE OF CONTENTS

UCTION ................................................................2OLLERS / PANELS / DISPLAYS ...........................4

XIMITY SENSOR ELECTRONICS UNIT ...............................4

-SKID CONTROL UNIT .........................................................5

EWHEEL STEERING ELECTRONIC CONTROL UNIT .........5

ING GEAR CONTROL PANEL .............................................6

RNATE EXTENSION HANDLE .............................................6

ING BRAKE HANDLE ..........................................................6

S INDICATIONS ....................................................................7

ANDING GEAR AND DOORS................................8ANDING GEAR AND DOORS.............................10G GEAR EXTENSION AND RETRACTION

M ...........................................................................12ING GEAR SELECTOR VALVE .........................................14

LOCK ACTUATOR ..............................................................14

RETRACT ACTUATOR AND TRANSFER CYLINDER .......14

LOCK ACTUATOR ..............................................................14

RETRACT ACTUATOR .......................................................14

UPLOCK ASSEMBLY .........................................................14

G GEAR ALTERNATE EXTENSION SYSTEM...16S AND BRAKES...................................................18 GEAR WHEEL / TIRE ASSEMBLIES ................................18

E GEAR WHEEL / TIRE ASSEMBLIES ...............................18

GEAR BRAKES .................................................................20

ING BRAKE SYSTEM ........................................................23

BRAKE TEMPERATURE MONI

BRAKE PRESSURE MONITOR

ANTI-SKID CONTROL SYSTEM

NOSEWHEEL STEERING SYPROXIMITY SENSING SYSTE

PROXIMITY SENSOR ELECTR

PROXIMITY SENSORS AND SW

SUPPLEMENTARY GEAR.....


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33 - Lighting SystemsCopyrigh 1 June 2005

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INTRODFLIGHT

PPFM

PASSECBGRLO

SERVICFANAA

EXTERTWNSBL

EMERG


TABLE OF CONTENTS

UCTION ................................................................2 COMPARTMENT LIGHTING................................3ANEL FLOODLIGHTS ..........................................................4ANEL INTEGRAL LIGHTING ................................................5LIGHT DISPLAY LIGHTING ..................................................6ISCELLANEOUS LIGHTING ................................................7

NGER COMPARTMENT LIGHTING .....................8EILING AND SIDEWALL LIGHTS ........................................8OARDING LIGHTS ................................................................9ALLEY LIGHTS ...................................................................10EADING LIGHTS ................................................................10AVATORY LIGHTS .............................................................10RDINANCE LIGHTS ...........................................................10

E AND MAINTENANCE LIGHTING ....................12ORWARD AND AFT BAGGAGE BAYS ..............................12VIONICS EQUIPMENT COMPARTMENT ..........................12OSE AND MAIN LANDING GEAR BAYS ...........................12FT EQUIPMENT BAY .........................................................12UXILIARY POWER UNIT BAY ............................................12

IOR LIGHTING......................................................14AXI / RECOGNITION AND LANDING LIGHTS ...................14ING INSPECTION LIGHTS ................................................14AVIGATION LIGHTS ..........................................................14TROBE (ANTICOLLISION) LIGHTS ...................................14EACON (ANTICOLLISION) LIGHTS ...................................14OGO LIGHTS ......................................................................14

ENCY LIGHTING.................................................16


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34 - NavigationCopyrigh 1 June 2005

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INTRODELECTR

PRIM

MUL

DISP

DISP

SOU

PITOT SINTEGRAIR DA

AIR D

AIR D

AIR D

AUTOMVHF NADISTANWEATH

WEA

DISP

WEA

RADIO ENHAN(EGPW

EGP

ROLS ........................................32

R SYSTEM .......................34SION AVOIDANCE SYSTEM ..........................................36....................................................38

....................................................39

ENCE SYSTEM................40TEM...................................42TEM ..................................46M OPERATION ........................48

EM ...................................50M ......................................52


TABLE OF CONTENTS

UCTION ................................................................2ONIC FLIGHT INSTRUMENT SYSTEM...............4

ARY FLIGHT DISPLAY .........................................................5

TIFUNCTION FLIGHT DISPLAY ............................................6

LAY CONTROL PANEL .........................................................8

LAY REVERSION SWITCH PANEL ......................................8

RCE SELECTOR PANEL .......................................................8

TATIC / TEMPERATURE SENSING .................10ATED STANDBY INSTRUMENT ........................12

TA SYSTEM..........................................................14ATA COMPUTER ...............................................................14

ATA REFERENCE PANEL .................................................14

ATA INDICATIONS ............................................................16

ATIC DIRECTION FINDER..................................18VIGATION SYSTEM............................................20CE MEASURING EQUIPMENT...........................22ER RADAR SYSTEM...........................................24THER RADAR PANEL .........................................................25

LAY CONTROL PANEL .......................................................25

THER RADAR DISPLAY .....................................................26

ALTIMETER SYSTEM..........................................28CED GROUND PROXIMITY WARNING SYSTEM S) ..........................................................................30WS COMPUTER ..................................................................30

EGPWS SWITCH/LIGHT CONT

ATC MODE S TRANSPONDETRAFFIC ALERT AND COLLI(TCAS)....................................

TCAS INDICATIONS ...............

TCAS CONTROLS ...................

ATTITUDE/HEADING REFERINERTIAL REFERENCE SYSFLIGHT MANAGEMENT SYS

FLIGHT MANAGEMENT SYSTE

GLOBAL POSITIONING SYSTSTANDBY COMPASS SYSTE


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35 - Oxygen SystemCopyrigh 1 June 2005

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INTRODPANEL

GRO

PASS

HIGH

EICA

CREW OXY

PRES

PRES

MAS

PASSEOXY

MAS

GEN

DEPL

PORTAPRO

POR


TABLE OF CONTENTS

UCTION ................................................................2S / SWITCHES / INDICATORS...............................4UND SERVICE OXYGEN PANEL .........................................4

ENGER OXYGEN SWITCH .................................................4

PRESSURE DISCHARGE INDICATOR ..............................4

S INDICATIONS ....................................................................4

OXYGEN SYSTEM.................................................6GEN CYLINDER .....................................................................6

SURE TRANSDUCER .........................................................6

SURE SWITCH ....................................................................6

K STOWAGE BOX AND CREW MASKS ...............................8

NGER OXYGEN SYSTEM ...................................10GEN MASK CONTAINERS ..................................................10

KS .........................................................................................10

ERATORS ............................................................................10

OYMENT ............................................................................10

BLE OXYGEN SYSTEM.......................................12TECTIVE BREATHING EQUIPMENT ..................................12

TABLE OXYGEN CYLINDERS AND MASKS ......................12


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36 - PneumaticsCopyrigh 1 June 2005

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INTRODCONTR

AIR C

ANTI

BLEE

EICA

ENGINEBLEEDBLEED

AUTO

MAN

CLSD

BLEED


TABLE OF CONTENTS

UCTION ................................................................2OLLERS / PANELS / DISPLAYS ...........................4ONDITIONING SYSTEM CONTROLLERS ..........................4

-ICE AND LEAK DETECTION CONTROLLER ......................4

D AIR CONTROL PANEL .....................................................5

S INDICATIONS ....................................................................6

BLEED AIR PORT SWITCHING..........................7 AIR DUCTING........................................................8 AIR MANAGEMENT ............................................10

MODE ...............................................................................10

UAL MODE ..........................................................................10

MODE ................................................................................10

AIR LEAK DETECTION .......................................12


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38 - Water and WasteCopyrigh 1 June 2005

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INTRODPOTAB

CONWATWAT

WAT

DRA

PRES

WASTE


TABLE OF CONTENTS

UCTION ................................................................2LE/WASH WATER SYSTEM..................................4TROLLER / CONTROL PANEL .............................................6ER SERVICE PANELS ...........................................................7ER STORAGE.........................................................................8

ER HEATER ...........................................................................8

IN MASTS ...............................................................................8

SURIZATION SYSTEM ......................................................10

DISPOSAL SYSTEM ..........................................11


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tenance Diagnostic SystemCopyrigh 1 June 2005

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INTRODMDS COMDS M

CUR

CUR

AIRC

LRU

LRU

SYST

ATA

LRU

MDC

CON

FCC

REPO

PILO

45 - Maint © Bombardier Inc. For Training Purposes Only

TABLE OF CONTENTS

UCTION ................................................................2MPONENTS .........................................................4

ENU NAVIGATION .................................................6RENT FAULTS ......................................................................8

RENT SERVICE MESSAGES ................................................8

RAFT HISTORY ..................................................................10

TEST ....................................................................................12

RIGGING .............................................................................12

EM PARAMETERS .............................................................14

INDEX ..................................................................................14

INDEX/OPERATIONS .........................................................14

SETUP ................................................................................15

FIGURATION DATA ............................................................15

DIAGNOSTICS ....................................................................16

RT DOWNLOAD ................................................................18

T DATA DOWNLOAD TO DISK ...........................................18


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45 -Copyright © Bombardier Inc. For Training Purposes Only



49 - Auxiliary Power UnitCopyrigh 1 June 2005

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INTRODCONTR

APU

APU

APU

APU

APU CO APU CAIR INLEXHAUOIL SYSFUEL SSTART

APU

APU

APU AISUR

APU


TABLE OF CONTENTS

UCTION ................................................................2OLLER / PANELS / DISPLAYS..............................4ELECTRONIC CONTROL UNIT ............................................4

CONTROL PANEL ................................................................4

INDICATIONS ........................................................................4

EMERGENCY SHUTDOWN SWITCHES .............................6

NSTRUCTION.......................................................8ONTROL AND MONITORING..............................10ET DOOR.............................................................12ST SYSTEM .........................................................13TEM ....................................................................14

YSTEM.................................................................16 AND IGNITION SYSTEMS ..................................18START .................................................................................20

STOP ...................................................................................20

R SYSTEM............................................................22GE CONTROL PROTECTION .............................................22

BLEED AIR CONTROL / DISTRIBUTION ...........................22


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52 - DoorsCopyrigh 1 June 2005

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INTRODCONTR

PRO

EICA

PASSEEMERG

OVE

CRE

SERVICGALL

MAIN

AFT

CARGOFOR

AFT


TABLE OF CONTENTS

UCTION ................................................................2OLLERS AND DISPLAYS......................................4

XIMITY SENSOR ELECTRONICS UNIT ...............................4

S DOORS INDICATIONS...................................................... 5

NGER DOOR..........................................................6ENCY EXITS .........................................................8

RWING EMERGENCY EXITS ................................................8

W ESCAPE HATCH ............................................................... 9

E DOORS............................................................10EY SERVICE DOOR ...........................................................10

AVIONICS COMPARTMENT DOOR .................................12

EQUIPMENT COMPARTMENT DOOR............................... 13

DOORS...............................................................14WARD / CENTER BAGGAGE BAY DOOR ..........................14

BAGGAGE BAY DOOR ....................................................... 16


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56 - WindowsCopyrigh 1 June 2005

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INTRODFLIGHTPASSESERVICEMERG


TABLE OF CONTENTS

UCTION ................................................................2 COMPARTMENT WINDOWS...............................3NGER COMPARTMENT WINDOWS .....................4E DOOR WINDOW................................................5ENCY EXIT DOOR WINDOW ...............................6


56 - Windows1 June 2005

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INTRODCOWLIENGINEENGINE

FUEL

FUEL

FUEL

FUEL

FULL

PERM

FAN

ENG

THRO

FUEL

STARTSTAR

AIR T

STAR

IGNIT

STAT

IGNIT

IGNIT

AIR SYCOM

COM

....................................................36

..........................................37................................................... 38

................................................... 39

E .............................................. 40

ING SYSTEM ...........................41

..........................................42................................................ 43

ATION .......................................44

ION ............................................46

..........................................50NT ...........................................50

....................................................54

....................................................58


TABLE OF CONTENTS

UCTION ................................................................2NG...........................................................................4

CONSTRUCTION ................................................6 FUEL AND POWER CONTROL ........................10 PUMP .................................................................................10

/OIL HEAT EXCHANGER ...................................................10

METERING UNIT ...............................................................10

MANIFOLD AND FUEL INJECTORS ................................12

AUTHORITY DIGITAL ENGINE CONTROL ...................... 13

ANENT MAGNET ALTERNATOR..................................... 14

INLET TEMPERATURE SENSOR (T2)............................... 15

INE CONFIGURATION PLUG CF34-8C5 ........................... 16

TTLE QUADRANT .............................................................16

CONTROL/POWER MANAGEMENT OPERATION ..........18

AND IGNITION.....................................................28T/IGNITION CONTROL PANEL .........................................28

URBINE STARTER .............................................................29

TER CONTROL VALVE .....................................................29

ION EXCITERS ..................................................................30

IC INVERTER .....................................................................30

ION LEADS ........................................................................30

ERS ....................................................................................30

STEM ....................................................................32BUSTION/TURBINE COOLING ..........................................32

PRESSOR AIRFLOW CONTROL .......................................34

SUMP PRESSURIZATION ......

ENGINE INDICATING ............N1 FAN SPEED ........................

N2 COMPRESSOR SPEED .....

INTERTURBINE TEMPERATUR

ENGINE VIBRATION MONITOR

THRUST REVERSER ............CONTROLS AND INDICATIONS

THRUST REVERSER INSTALL

THRUST REVERSER ACTUAT

ENGINE OIL SYSTEM ...........STORAGE AND REPLENISHME

ENGINE OIL DISTRIBUTION ..

OIL INDICATING ......................


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Documents

CRJ700/900 Technical Familiarization Manual - ANTN … · INDEX Chapter AG - Aircraft General Chapter 21 - Air Conditioning Chapter 22 - Autoflight Chapter 23 - Communication Chapter