CRJ700/900 Technical Familiarization Manual

Transcription

CSP B-026TECHNICAL FAMILIARIZATION MANUALFOR TRAINING PURPOSES ONLY1 June 2005

Copyright 1999 - 2005 Bombardier Inc. or its subsidiaries. All rights reserved.Bombardier Inc., by its groups, divisions or its corporate subsidiary Learjet Inc.,provides this information to the government in confidence. This is proprietaryconfidential information, which we consider excluded from the application of theAccess to information Act and may also be a trade secret of our company. Publicrelease of this information would be harmful to Bombardier Inc. or its corporatesubsidiary Learjet Inc. Any intention to disclose such information, or part thereof,must be indicated in advance and in writing to the Vice-President Legal Services,Corporate Office.It is understood that this documentation, comprising technical data and otherinformation in any media shall not be reproduced or disclosed in whole or in partwithout Bombardier's written authorization, and is proprietary and confidential toBombardier or its corporate subsidiary Learjet Inc. and that all rights and patent,copyright, trademark, trade secret and other intellectual property rights thereinbelong to Bombardier or its corporate subsidiary Learjet Inc. Such documentation,technical data and other information shall not be modified, translated, reverseassembled, reverse engineered or decompiled and shall be used solely fortraining purposes only.FOR TRAINING PURPOSES ONLY1 June 2005

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

TECHNICAL TRAINING MANUALTABLE OF CONTENTSDESIGN FEATURES .2INTRODUCTION .2AIRFRAME STRUCTURE .8SERVICING/TOWING/TAXIING .10BAGGAGE/CARGO & EQUIPMENT COMPARTMENTS 18AFT CARGO/BAGGAGE COMPARTMENT .18FORWARD BAGGAGE COMPARTMENT .19AVIONICS EQUIPMENT COMPARTMENTS .21FLIGHT COMPARTMENT .24PASSENGER COMPARTMENT .34PASSENGER SEATS .34FLIGHT ATTENDANT SEATS .36GALLEY COMPARTMENTS .37CLOSETS AND PARTITIONS .39LAVATORY .41EMERGENCY EQUIPMENT .4201 - AIRCRAFT GENERALCopyright Bombardier Inc.For Training Purposes Only1 June 2005Pg 01-i

TECHNICAL TRAINING MANUALTHIS PAGE IS INTENTIONALLY LEFT BLANK01 - AIRCRAFT GENERALCopyright Bombardier Inc.For Training Purposes Only1 June 2005Pg 01-ii

TECHNICAL TRAINING MANUALAIRCRAFT GENERAL01 - AIRCRAFT GENERALCopyright Bombardier Inc.For Training Purposes Only1 June 2005Pg 01-1

TECHNICAL TRAINING MANUALDESIGN FEATURESHISTORY OF CRJ700, CRJ900 AND CRJ705INTRODUCTIONThe 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-600-2D15General 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.The CL-600-2C10 aircraft is the first variant of the CRJ200.Product improvements include but are not limited to a longerfuselage, FADEC-controlled engines, a new wing with leadingedge slats, a forward cargo compartment, and upgradedautomated aircraft systems. This aircraft is marketed as theCRJ700 (68 seats), the CRJ701 (70 seats) and the CRJ702 (77seats). It is available in a standard or extended range version.The CL-600-2D24 aircraft is the second variant of the CRJ200.Product improvements (compared to the CRJ200 series aircraft)include but are not limited to a longer fuselage, FADEC-controlledengines, a new wing with leading edge slats, a forward cargocompartment, and upgraded automated aircraft systems. Thisaircraft is marketed as the CRJ900 (up to 90 seats). It, too, isavailable in standard or extended range versions.Later, short field takeoff and landing performance improvementswere introduced. Performance improvements consisted of alarger wingspan due to bigger winglets, software changes, newslat/flap relationship with an added selection of Flap 20, and anoptional long range version.The CL-600-2D15 aircraft is the third CRJ200 variant. This variantis identical to the improved CL-600-2D24 series 900 aircraftexcept that it is only certified for a maximum of 75 passengersand is marketed as the CRJ705 (75 seats).01 - AIRCRAFT GENERALCopyright Bombardier Inc.For Training Purposes Only1 June 2005Pg 01-2

TECHNICAL TRAINING MANUALGENERAL AIRCRAFT DATAThe following table provides a general comparison of the CRJ700series and CRJ705/900 series aircraft, as well as the extendedrange (ER) and long range (LR) model configurations.Maximum Take-off Weight(MTOW)Maximum Landing Weight 0 LR72,750 lb(33,000 kg)75,000 lb(34,019 kg)80,500 lb(36,514 kg)82,500 lb(37,421 kg)84,500 lb(38,329 kg)67,000 lb (30,391 kg)Maximum Usable Fuel(@ 6.75 lbs/US gallon)Range (@ Mach 0.74)75,100 lb(34,065 kg)19,595 lb (8,888 kg)1685 nm(3121 km)1985 nm(3767 km)Maximum Operating AltitudeStandard Seating Capacity73,500 lb (33,340 kg)1479 nm(2739 km)1706 nm(3160 km)1940 nm(3593 km)41,000 ft (12,500 m)68 to 7874 or 75 - CRJ705, up to 90 - CRJ90001 - AIRCRAFT GENERALCopyright Bombardier Inc.For Training Purposes Only1 June 2005Pg 01-3

TECHNICAL TRAINING MANUALAIRCRAFT DIMENSIONSThe following table offers quick reference to dimensionaldifferences between the aircraft series.LengthWingspanTailspanHeightMain Wheel TrackNose to MainCRJ700106 ft, 8 in32.51 m76 ft, 3 in23.25 m28 ft8.53 m24 ft, 10 in7.57 m13 ft, 6 in4.11 m37 ft, 5 in11.43 mCRJ705119 ft, 4 in36.4 m81 ft, 7 in24.9 m28 ft8.53 m24 ft, 7 in7.5 m13 ft, 6 in4.11 m48 ft, 4 in14.73 mCRJ900119 ft, 4 in36.4 m76 ft, 3 in23.25 m28 ft8.53 m24 ft, 7 in7.5 m13 ft, 6 in4.11 m48 ft, 4 in14.73 mFIGURE 1 - CABIN CROSS SECTION01 - AIRCRAFT GENERALCopyright Bombardier Inc.For Training Purposes Only1 June 2005Pg 01-4

TECHNICAL TRAINING MANUAL13 ft, 6 in.(4.11 m)76 ft, 3 in. (23.25 m)28 ft(8.54 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/CGMFIGURE 2 - AIRCRAFT DIMENSIONS - CRJ70001 - AIRCRAFT GENERALCopyright Bombardier Inc.For Training Purposes Only1 June 2005Pg 01-5

TECHNICAL TRAINING MANUAL13 ft, 6 in.(4.11 m)81 ft, 7 in. (24.87 m)28 ft.(8.54 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)56 ft, 9 in. (17.29 m)118 ft, 11 in. (36.4 m)CR9/AG-09-00-0002/CGMFIGURE 3 - AIRCRAFT DIMENSIONS - CRJ705/90001 - AIRCRAFT GENERALCopyright Bombardier Inc.For Training Purposes Only1 June 2005Pg 01-6

TECHNICAL TRAINING MANUALTHIS PAGE IS INTENTIONALLY LEFT BLANK01 - AIRCRAFT GENERALCopyright Bombardier Inc.For Training Purposes Only1 June 2005Pg 01-7

TECHNICAL TRAINING MANUALAIRFRAME STRUCTUREThe 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 midcenter fuselage ‘D’ shaped. This provides an area external to thepressure zone where the wing attaches to the fuselage.CRJ705/900: the dorsal strake is not installed on the aircraft,however ventral fins are installed on the base of the fuselage. Thefins increase the directional stiffness of the aircraft. Relative to theCRJ700, the ventral fins offset the effects of the fuselage stretchand eliminates the need for the fuselage upper strake.The single piece wing is an all-metal structure consisting ofmachined upper and lower aluminum alloy planks with integralstringers covering the spar, ribs and a central box structure.CRJ705/900: a new winglet is installed which increases thewingspan by 5 ft, 4 in.The auxiliary rear spar provides structural support for the mainlanding gear trunnion. The main landing gear retracts into the aftsection of the center box structure. The wing has provisions forthe installation of ailerons, slats, two-section slotted flaps, groundspoilers, multifunction flight spoilers and space for fuel storage.The vertical stabilizer is a fully-cantilevered, swept-back designwith a swept-back horizontal stabilizer mounted on the top edge.The leading edges of the wing, slats, vertical and horizontalstabilizers are fabricated using aluminum alloy.Composite materials are used in the aircraft secondary structuressuch as the radome, winglets, belly fairings, landing gear doorsand empennage top fairings.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.01 - AIRCRAFT GENERALCopyright Bombardier Inc.For Training Purposes Only1 June 2005Pg 01-8

TECHNICAL TRAINING MANUALHORIZONTAL STABILIZERTIP STRUCTUREVERTICALSTABILIZERTIP FAIRINGVERTICAL STABILIZERLEADING EDGESTRUCTUREDORSALFAIRINGRAM AIRINLET DUCTVENTRAL FINS(CRJ705/900)TAIL CONEWINGLETPYLONTRAILING EDGESTRUCTUREDORSAL STRAKE(CRJ700 ONLY)PLUGS(CRJ705/900)WING LEADINGEDGE SLATSCORE COWLFAN COWLDOORSPYLON LEADINGEDGE STRUCTUREWING TOFUSELAGEFAIRINGSWING TOFUSELAGEFAIRINGSMAINLANDINGGEAR1LIPSKINWING TRAILINGEDGE OSE LANDINGGEAR DOORSThe wing trailing edge primary structureincludes the support structure for theflaps, ailerons and spoilers.PRIMARY STRUCTURESECONDARY STRUCTUREFIGURE 4 - GENERAL CONSTRUCTION01 - AIRCRAFT GENERALCopyright Bombardier Inc.For Training Purposes Only1 June 2005Pg 01-9

TECHNICAL TRAINING MANUALSERVICING / TOWING / TAXIINGTypical 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.01 - AIRCRAFT GENERALCopyright Bombardier Inc.For Training Purposes Only1 June 2005Pg 01-10

TECHNICAL TRAINING MANUALOXYGENREFILLREFUEL / DEFUELCONTROL PANELFORWARDPOTABLEWATERADG PUMPADGSINGLE-POINTREFUEL/DEFUELGROUND AIRCONDITIONING AIRGROUNDPOWEREXTERNALSERVICESFORWARDLAVATORYWASTE DRAINENGINE OILSERVICING#3 HYDRAULICSYSTEMAPU#1 & #2HYDRAULICSYSTEMSAFT LAVATORYWASTE DRAINOVERWING GRAVITYFUEL FILLERENGINE STARTHIGH-PRESSURE AIRLAVATORYPOTABLE WATEROVERWING GRAVITYFUEL FILLERBRAKEACCUMULATORSCR7/52-45-00-0001/CGMFIGURE 5 - AIRCRAFT SERVICING LOCATIONS01 - AIRCRAFT GENERALCopyright Bombardier Inc.For Training Purposes Only1 June 2005Pg 01-11

TECHNICAL TRAINING MANUALUPPERTORQUELINK (ARM)QUICKDISCONNECTMECHANISMLOWERTORQUELINK (ARM)TOW BARLESS TOWINGMETAL EYETOW BARTOW BARAXLEENGAGEMENTPINCR7/AG-09-00-0001/CGMFIGURE 6 - TOW BAR / TOW-BARLESS TOWING01 - AIRCRAFT GENERALCopyright Bombardier Inc.For Training Purposes Only1 June 2005Pg 01-12

TECHNICAL TRAINING MANUAL48 ft, 5 in.(14.75 m)55 ft, 3 in.(16.84 m)57 ft.(17.61m)MAXIMUMTOWINGANGLE 70 118 ft.(35.9 m)49 ft, 7 in.(15.11 m)MAXIMUMTAXIINGANGLE 80 TURNINGCENTERS MAXIMUM TOWING / TURNINGRADIUS WITH TORQUE ARMS CONNECTEDOR DISCONNECTED TURNING RADII SHOWN REPRESENTS THETHEORETICAL GEOMETRIC TURNING CENTERS TOWING BASED ON MAXIMUM AIRCRAFT WEIGHTCR7/AG-09-00-0002/CGMFIGURE 7 - TURNING RADIUS - CRJ70001 - AIRCRAFT GENERALCopyright Bombardier Inc.For Training Purposes Only1 June 2005Pg 01-13

TECHNICAL TRAINING MANUAL55 ft, 3 in.(16.84 m)61 ft, 4 in.(18.7 m)65 ft.(19.8 m)MAXIMUMTOWINGANGLE 70 21 ft.(6.4 m)MAXIMUMTAXIINGANGLE 80 126 ft, 5 in.(38.2 m)59 ft.(18 m)TURNINGCENTERS MAXIMUM TOWING / TURNINGRADIUS WITH TORQUE ARMS CONNECTEDOR DISCONNECTED TURNING RADII SHOWN REPRESENTS THETHEORETICAL GEOMETRIC TURNING CENTERS TOWING BASED ON MAXIMUM AIRCRAFT WEIGHTCR9/AG-09-00-0001/CGMFIGURE 8 - TURNING RADIUS - CRJ705/90001 - AIRCRAFT GENERALCopyright Bombardier Inc.For Training Purposes Only1 June 2005Pg 01-14

TECHNICAL TRAINING MANUALCR7/AG-10-20-0008/CGMFIGURE 9 - MAIN AND NOSE GEAR LOCKPIN LOCATIONS01 - AIRCRAFT GENERALCopyright Bombardier Inc.For Training Purposes Only1 June 2005Pg 01-15

TECHNICAL TRAINING MANUALGROUNDINGLUGGROUNDINGLUGALLIGATORCLAMPGROUND STUDRECEPTACLEGROUND LUG(HERE)GROUNDSTUDCR7/AG-10-20-0002/CGMFIGURE 10 - AIRCRAFT GROUNDING01 - AIRCRAFT GENERALCopyright Bombardier Inc.For Training Purposes Only1 June 2005Pg 01-16

TECHNICAL TRAINING MANUALTHIS PAGE IS INTENTIONALLY LEFT BLANK01 - AIRCRAFT GENERALCopyright Bombardier Inc.For Training Purposes Only1 June 2005Pg 01-17

TECHNICAL TRAINING MANUALBAGGAGE / CARGO AND EQUIPMENTCOMPARTMENTSThe 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 COMPARTMENTFS959.50The 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.OUTERSKINCARGOLINERSFS992.00BULKHEADCARGO DOORRESTRAINT CR7/25-50-00-0005/CGMFIGURE 11 - AFT CARGO COMPARTMENT01 - AIRCRAFT GENERALCopyright Bombardier Inc.For Training Purposes Only1 June 2005Pg 01-18

TECHNICAL TRAINING MANUALTABLE OF CONTENTSINTRODUCTION .2CONTROLLERS / PANELS / DISPLAYS .3AIR CONDITIONING SYSTEM/CABIN PRESSURECONTROLLERS .3AIR CONDITIONING CONTROL PANEL . 4CABIN PRESSURE CONTROL PANEL . 5AVIONICS COOLING PANEL. 6GALLEY PANEL .6EICAS ECS INDICATIONS. 7DISTRIBUTION.8FLIGHT COMPARTMENT DISTRIBUTION .10PASSENGER COMPARTMENT DISTRIBUTION . 11VENTILATION. 12GALLEY HEATING .12AVIONICS EQUIPMENT/DISPLAY COOLING .14AFT CARGO COMPARTMENT CONDITIONED AIR .16COOLING .18FLOW CONTROL AND PRE-COOLER .20RAM AIR SYSTEM .20AIR CONDITIONING UNITS (PACKS) .22TEMPERATURE CONTROL .24PRESSURIZATION CONTROL.2621 - Air ConditioningCopyright Bombardier Inc.For Training Purposes Only1 June 2005Pg 21-i

TECHNICAL TRAINING MANUALTHIS PAGE IS INTENTIONALLY LEFT BLANK21 - Air ConditioningCopyright Bombardier Inc.For Training Purposes Only1 June 2005Pg 21-ii

TECHNICAL TRAINING MANUALTABLE OF CONTENTSINTRODUCTION .2COMPONENTS . 3INTEGRATED AVIONICS PROCESSOR.7FLIGHT DIRECTOR .8FLIGHT DIRECTOR MODES . 10AUTOPILOT.12YAW DAMPER SYSTEM.14FCC DIAGNOSTICS.16REPORT MODE .16INPUT MODE .16OUTPUT MODE .1622 - AutoflightCopyright Bombardier Inc.For Training Purposes Only1 June 2005Pg 22-i

TECHNICAL TRAINING MANUALTHIS PAGE IS INTENTIONALLY LEFT BLANK22 - AutoflightCopyright Bombardier Inc.For Training Purposes Only1 June 2005Pg 22-ii

TECHNICAL TRAINING MANUALTABLE OF CONTENTSINTRODUCTION .2AUDIO INTEGRATING SYSTEM .3AUDIO ELECTRONICS CONTROL UNIT .3AUDIO CONTROL PANEL . 4MAINTENANCE INTERPHONE UNITS. 5MECHANIC CALL SWITCH/LIGHTS .5RADIO TRANSMIT / INTERCOM SWITCH .5MICROPHONES .5SPEAKERS .5PASSENGER ADDRESS AND CABIN INTERPHONE .7PASSENGER BRIEFING SYSTEM.9INTEGRATED AUTOMATIC TUNING.10RADIO TUNING UNITS .10STANDBY TUNING UNIT .12RTU INHIBIT PUSH SWITCHES .12FMS TUNE INHIBIT SWITCH .12VHF COMMUNICATION SYSTEM.13SELECTIVE CALL SYSTEM .15HF COMMUNICATIONS SYSTEM.16COCKPIT VOICE RECORDER SYSTEM .18ARINC COMMUNICATIONS ADDRESSING ANDREPORTING SYSTEM.2023 - CommunicationCopyright Bombardier Inc.For Training Purposes Only1 June 2005Pg 23-i

TECHNICAL TRAINING MANUALTHIS PAGE IS INTENTIONALLY LEFT BLANK23 - CommunicationCopyright Bombardier Inc.For Training Purposes Only1 June 2005Pg 23-ii

TECHNICAL TRAINING MANUALTABLE OF CONTENTSINTRODUCTION .2TRANSFORMER RECTIFIER UNITS .26CONTROLS AND INDICATIONS .4BATTERIES . 27AC POWER GENERATION.8DC POWER CONTROL AND DISTRIBUTION .28INTEGRATED DRIVE GENERATOR .8DC BUSES. 29AUXILIARY (APU) GENERATOR .10AC POWER CONTROL AND DISTRIBUTION.12GENERATOR CONTROL UNITS .12AC POWER CENTER .12AIR DRIVEN GENERATOR POWER CENTER .12AC POWER DISTRIBUTION . 14AC POWER SOURCE SELECTION. 15AUTOTRANSFER INHIBIT . 17AC ESSENTIAL BUS CONTROL . 18AC SERVICE BUS .18EXTERNAL AC POWER .20EMERGENCY AC POWER GENERATION .22AIR DRIVEN GENERATOR .22GENERATOR CONTROL UNIT .22AUTOMATIC DEPLOY CONTROL UNIT .22STOW PUMP .22MANUAL DEPLOYMENT HANDLE .24UPLOCK ASSEMBLY .24EJECTION ACTUATOR .24ADG CONTROL PANEL . 25DC POWER GENERATION .2624 - Electrical Power SystemCopyright Bombardier Inc.For Training Purposes Only1 June 2005Pg 24-i

TECHNICAL TRAINING MANUALTHIS PAGE IS INTENTIONALLY LEFT BLANK24 - Electrical Power SystemCopyright Bombardier Inc.For Training Purposes Only1 June 2005Pg 24-ii

TECHNICAL TRAINING MANUALTABLE OF CONTENTSINTRODUCTION .2CONTROLLERS AND PANELS .4ENGINE FIRE PROTECTION .6ENGINE FIRE DETECTION .6ENGINE FIRE EXTINGUISHING .7ENGINE FIRE EXTINGUISHING OPERATION. 8APU FIRE PROTECTION.10APU FIRE DETECTION .10APU FIRE EXTINGUISHING . 11APU FIRE EXTINGUISHING OPERATION . 12MAIN LANDING GEAR OVERHEAT DETECTION .14CARGO COMPARTMENT FIRE PROTECTION.16CARGO COMPARTMENT SMOKE DETECTION .16CARGO COMPARTMENT FIRE EXTINGUISHING .17CARGO COMPARTMENT FIRE EXTINGUISHING OPERATION18LAVATORY FIRE PROTECTION .20LAVATORY SMOKE DETECTION .20LAVATORY WASTE BIN FIRE EXTINGUISHING .20PORTABLE FIRE EXTINGUISHERS .2126 - Fire ProtectionCopyright Bombardier Inc.For Training Purposes Only1 June 2005Pg 26-i

TECHNICAL TRAINING MANUALTHIS PAGE IS INTENTIONALLY LEFT BLANK26 - Fire ProtectionCopyright Bombardier Inc.For Training Purposes Only1 June 2005Pg 26-ii

TECHNICAL TRAINING MANUALTABLE OF CONTENTSINTRODUCTION .2ELEVATOR CONTROL .26CONTROLLERS/PANELS/DISPLAYS .4PITCH DISCONNECT OPERATION .28SPOILER/STABILIZER CONTROL UNIT .4PITCH FEEL OPERATION .30SLAT/FLAP ELECTRONIC CONTROL UNIT . 5HORIZONTAL STABILIZER TRIM CONTROL.32STALL PROTECTION COMPUTER . 6STALL PROTECTION SYSTEM .34CONTROL WHEEL SWITCHES .7SPOILER SYSTEM .36PITCH AND ROLL DISCONNECT HANDLES .7SLAT / FLAP SYSTEM .40SPOILER CONTROL PANEL .7SPOILER CONTROL LEVER .7SLAT/FLAP CONTROL LEVER .7STABILIZER/MACH TRIM CONTROL PANEL. 8AILERON/RUDDER CONTROL PANEL .8YAW DAMPER CONTROL PANEL .8EMERGENCY FLAP SWITCH .8STALL PROTECTION CONTROL SWITCH. 9STALL PROTECTION SWITCH/LIGHT .9ROLL PRIORITY SWITCH/LIGHTS .9FLIGHT CONTROL INDICATIONS. 10AILERON CONTROL.12ROLL DISCONNECT OPERATION .14AILERON TRIM OPERATION .16RUDDER CONTROL .18RUDDER ANTI-JAM OPERATION .20YAW DAMPER/RUDDER TRIM OPERATION .22RUDDER TRAVEL LIMITER .2427 - Flight ControlsCopyright Bombardier Inc.For Training Purposes Only1 June 2005Pg 27-i

TECHNICAL TRAINING MANUALTHIS PAGE IS INTENTIONALLY LEFT BLANK27 - Flight ControlsCopyright Bombardier Inc.For Training Purposes Only1 June 2005Pg 27-ii

TECHNICAL TRAINING MANUALTABLE OF CONTENTSINTRODUCTION .2CONTROLLERS / PANELS / DISPLAYS .4FUEL QUANTITY GAUGING COMPUTER .4FUEL CONTROL PANEL. 5REFUEL/DEFUEL CONTROL PANEL . 6EICAS FUEL INDICATIONS . 7FUEL STORAGE .8FUEL TANKS .8TANK VENTING .10FUEL LOAD MANAGEMENT .12FUEL SCAVENGE .12FUEL TRANSFER .12POWER CROSS-FLOW .14GRAVITY CROSS-FLOW .14FUEL DISTRIBUTION .17MOTIVE FLOW SYSTEM .17ENGINE FUEL FEED SYSTEM. 18STANDBY FUEL FEED SYSTEM .20APU FUEL FEED SYSTEM

forward pressure bulkhead, forwar d avionics bay, main passenger entrance and support mountings for the nose landing gear. The center fuselage contains the passenger compartment, main avionics bay, forward cargo compartment, and the structural wing attachment. CRJ705/9