航线CRJElectricalSystem学习教案

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1、会计学1航线航线CRJElectricalSystem第一页，编辑于星期三：点 二十二分。2第1页/共104页第二页，编辑于星期三：点 二十二分。3n 1 AC Ground Power ReceptaclenPower Receptacle ACDC第2页/共104页第三页，编辑于星期三：点 二十二分。4FLIGHT DECK SWITCHES第3页/共104页第四页，编辑于星期三：点 二十二分。5No Reconnect第4页/共104页第五页，编辑于星期三：点 二十二分。6第5页/共104页第六页，编辑于星期三：点 二十二分。7第6页/共104页第七页，编辑于星期三：点 二十二分。8第7

2、页/共104页第八页，编辑于星期三：点 二十二分。9SYSTEM第8页/共104页第九页，编辑于星期三：点 二十二分。10IDG Disconnect* Low oil pressure* High oil tempAutomaticGen Over tempOver torque - Shears the shaft No Reconnect第9页/共104页第十页，编辑于星期三：点 二十二分。11No Reconnect第10页/共104页第十一页，编辑于星期三：点 二十二分。12No Reconnect第11页/共104页第十二页，编辑于星期三：点 二十二分。13No Reconnect

3、第12页/共104页第十三页，编辑于星期三：点 二十二分。14No Reconnect第13页/共104页第十四页，编辑于星期三：点 二十二分。15第14页/共104页第十五页，编辑于星期三：点 二十二分。16SERVICE BUS第15页/共104页第十六页，编辑于星期三：点 二十二分。17SERVICE BUSGROUND POWER0000第16页/共104页第十七页，编辑于星期三：点 二十二分。18Flight Deck switchpowers all AC第17页/共104页第十八页，编辑于星期三：点 二十二分。19POWER HAS NOT BEEN CONNECTED OR P

4、OWER HASWRONG VOLTAGEOUT OF PHASEWRONG FREQUENCYNo Reconnect第18页/共104页第十九页，编辑于星期三：点 二十二分。20POWER HAS BEEN CHECKED BY ONBOARD COMPUTER AND THE VOLTAGE, PHASE, FREQUENCY OF THE POWER SOURCE ARE ALL OK BUT POWER HAS BEEN CONNECTED TO AIRCRAFT SYSTEMNo Reconnect第19页/共104页第二十页，编辑于星期三：点 二十二分。21第20页/共104页第

5、二十一页，编辑于星期三：点 二十二分。22第21页/共104页第二十二页，编辑于星期三：点 二十二分。23CABIN CREW STATIONEXTERNAL STATION12第22页/共104页第二十三页，编辑于星期三：点 二十二分。24CABIN CREW STATIONEXTERNAL STATION12第23页/共104页第二十四页，编辑于星期三：点 二十二分。25nPowers SERVICE onlyGalleyTHIS SWITCH OPENS THE NOSE GEAR DOORS TO PERMIT THE CREW TO REMOVE/INSTALL THE IDG LO

6、CK PIN AND INSPECT THE NOSE WHEEL WELL.第24页/共104页第二十五页，编辑于星期三：点 二十二分。26nPowers SERVICE N onlyBUSESGalleyPRESSING THIS BUTTON WITH EITHER APU-AC GEN OR AC GROUND POWER SHUTS DOWN ALL BUSES EXCEPT A)AC SERVICE BUS VACUUM CLEANERS & TOILET PUMPB)AC UTILITY BUS - GALLEY & BATTERY CHARGERSAVAILIN USE第25页

7、/共104页第二十六页，编辑于星期三：点 二十二分。27nPowers SERVICE N onlyBUSESGalleyWHEN PRESSED SIGNALS LIGHT AT CAPTAINS STATION INDICATING GROUND PERSONNEL WANT TO TALK.CALL第26页/共104页第二十七页，编辑于星期三：点 二十二分。28nPowers SERVICE N onlyBUSESGalleyWHEN PRESSED IT SHUTS DOWN THE APU.第27页/共104页第二十八页，编辑于星期三：点 二十二分。29nPowers SERVICE

8、 onlyGalleyWHEN LIGHTED IT INDICATES THAT THE BATTERY MASTER SWITCH IN THE COCKPIT IS ON.第28页/共104页第二十九页，编辑于星期三：点 二十二分。30nPowers SERVICE N onlyGalleyWHEN LIGHTED IT INDICATES THAT THE PARKING BRAKE IS ON.第29页/共104页第三十页，编辑于星期三：点 二十二分。31nPowers SERVICE onlyBUSESGalleyWHEN PRESSED IT CHECKS THE “BATT-O

9、N”, “PKG BRK-ON”, ” EXT AC PUSH” LIGHTS BY TURNING THEM ON.第30页/共104页第三十一页，编辑于星期三：点 二十二分。32nPowers SERVICE N onlyGalleyTHIS IS WHERE THE GROUND CREW CONNECT THEIR HEADSET FOR GROUND COCKPIT COMMUNICATIONS.第31页/共104页第三十二页，编辑于星期三：点 二十二分。33第32页/共104页第三十三页，编辑于星期三：点 二十二分。34AC BUS 1IDG 1, then APU GEN, th

10、en IDG 2, then EXTERNAL POWERAC BUS 2IDG 2, then APU GEN, then IDG 1, then EXTERNAL POWER: WHEN AIRCRAFT GENERATORS ARE OPERATIONAL; EXTERNAL POWER IS AUTOMATICALLY DISCONNECTED FROM THE AIRCRAFT.第33页/共104页第三十四页，编辑于星期三：点 二十二分。35第34页/共104页第三十五页，编辑于星期三：点 二十二分。36EXTENDEDRETRACTED第35页/共104页第三十六页，编辑于星期三：

11、点 二十二分。37EXTENDEDRETRACTED第36页/共104页第三十七页，编辑于星期三：点 二十二分。38After ADG is deployed, if any other AC Generator becomesoperational, load is automatically transferred from ADG to operatingenerator.AFTER THE ADG IS DEPLOYED SHOULD A GENERATOR BE BROUGHT BACK ON-LINE THE ELECTRICAL LOAD IS AUTOMATICALLY TRA

12、NSFERRED FROM THE ADG TO THE OPERATING GENERATOR.PRESSING THE “ PWR TXFR OVERRIDE “ WILL THIS FROM HAPPENING.第37页/共104页第三十八页，编辑于星期三：点 二十二分。39第38页/共104页第三十九页，编辑于星期三：点 二十二分。40第39页/共104页第四十页，编辑于星期三：点 二十二分。41AUTOMATIC LOAD SHEDDINGSHOULD THE IDG DISCONNECT THE ELECTRICAL SYSTEM WILL AUTOMATICALLY SHED U

13、TILITY BUS 1 AND UTILITY BUS 2 AND WILL BE SHOWN AS INDICATED TO THE LEFT DISPLAY.FOR SOME REASON THE IDG HAS DISCONNECTED GEN 1 FROM THE ENGINE第40页/共104页第四十一页，编辑于星期三：点 二十二分。42AUTOMATIC LOAD SHEDDINGSHOULD THE IDG DISCONNECT THE ELECTRICAL SYSTEM WILL AUTOMATICALLY SHED UTILITY BUS 1 AND UTILITY BUS

14、 2 AND WILL BE SHOWN AS INDICATED TO THE LEFT DISPLAY.IDG HAS BEEN DISCONNECT THEN UTILITY BUS 1 & 2 ARE SHEDDED第41页/共104页第四十二页，编辑于星期三：点 二十二分。43No Reconnect第42页/共104页第四十三页，编辑于星期三：点 二十二分。44第43页/共104页第四十四页，编辑于星期三：点 二十二分。45No Reconnect第44页/共104页第四十五页，编辑于星期三：点 二十二分。46AC ESS XFER1.AC ESS BUS IS POWERED B

15、Y AC BUS 1No Reconnect第45页/共104页第四十六页，编辑于星期三：点 二十二分。47POWERAC ESS XFER1.AC ESS BUS NOT POWERED BY AC BUS 12.And is now powered by BUS 2No Reconnect第46页/共104页第四十七页，编辑于星期三：点 二十二分。48AC ESS XFERAC ESS BUS IS POWERED BY AC BUS 1第47页/共104页第四十八页，编辑于星期三：点 二十二分。49AC ESS XFERAC ESS BUS NOT POWERED BY AC BUS 1

16、第48页/共104页第四十九页，编辑于星期三：点 二十二分。50AC ESS XFERWHEN POWER LOSS FROM BUS 1 IS DETECTED A AUTOMATIC TRANSFER WILL BE INITIATED TO BUS 2.HOWEVER WHAT IF YOU DO NOT WANT THE ESS BUS POWERED?PRESSFAILOFFAUTOXFERAuto xfer has been turned off第49页/共104页第五十页，编辑于星期三：点 二十二分。51AC ESS XFERWHEN POWER LOSS FROM BUS 1

17、IS DETECTED A AUTOMATIC TRANSFER WILL BE INITIATED TO BUS 2.HOWEVER WHAT IF YOU DO NOT WANT THE ESS BUS POWERED?PRESSFAILOFFAUTOXFERAuto xfer has been turned off第50页/共104页第五十一页，编辑于星期三：点 二十二分。52第51页/共104页第五十二页，编辑于星期三：点 二十二分。53第52页/共104页第五十三页，编辑于星期三：点 二十二分。54NOTE:BOTH BATTERIES ARE LOCATED IN THE AFT

18、EQUIPMENT BAY.第53页/共104页第五十四页，编辑于星期三：点 二十二分。55第54页/共104页第五十五页，编辑于星期三：点 二十二分。56第55页/共104页第五十六页，编辑于星期三：点 二十二分。57第56页/共104页第五十七页，编辑于星期三：点 二十二分。58DECK LIGHTS第57页/共104页第五十八页，编辑于星期三：点 二十二分。59第58页/共104页第五十九页，编辑于星期三：点 二十二分。60第59页/共104页第六十页，编辑于星期三：点 二十二分。61nMax 100 Amps each第60页/共104页第六十一页，编辑于星期三：点 二十二分。62nM

19、ax 100 Amps each第61页/共104页第六十二页，编辑于星期三：点 二十二分。63nMax 100 Amps each第62页/共104页第六十三页，编辑于星期三：点 二十二分。64nMax 100 Amps each第63页/共104页第六十四页，编辑于星期三：点 二十二分。65nMax 100 Amps each第64页/共104页第六十五页，编辑于星期三：点 二十二分。66nMax 100 Amps each第65页/共104页第六十六页，编辑于星期三：点 二十二分。67第66页/共104页第六十七页，编辑于星期三：点 二十二分。68第67页/共104页第六十八页，编辑于星

20、期三：点 二十二分。69第68页/共104页第六十九页，编辑于星期三：点 二十二分。70TIE 1 & 2 Automatic. ESS manual-only.第69页/共104页第七十页，编辑于星期三：点 二十二分。71No ReconnectDC BUS TIE COCKPIT SWITCHESLTS OFF = OPEN第70页/共104页第七十一页，编辑于星期三：点 二十二分。72No ReconnectDC BUS TIE COCKPIT SWITCHESLTS ON = CLOSED第71页/共104页第七十二页，编辑于星期三：点 二十二分。73TIE 1 & 2 Automat

21、ic. ESS manual-only.第72页/共104页第七十三页，编辑于星期三：点 二十二分。74TIE 1 & 2 Automatic. ESS manual-only.第73页/共104页第七十四页，编辑于星期三：点 二十二分。75TIE 1 & 2 Automatic. ESS manual-only.第74页/共104页第七十五页，编辑于星期三：点 二十二分。76TIE 1 & 2 Automatic. ESS manual-only.第75页/共104页第七十六页，编辑于星期三：点 二十二分。77第76页/共104页第七十七页，编辑于星期三：点 二十二分。78第77页/共104

22、页第七十八页，编辑于星期三：点 二十二分。79EMERG BUSBATT BUSAPU BATTDIR BUSSERVICE BUSESS BUS第78页/共104页第七十九页，编辑于星期三：点 二十二分。80EMERG BUSBATT BUSAPU BATTDIR BUSSERVICE BUSESS BUS第79页/共104页第八十页，编辑于星期三：点 二十二分。81EMERG BUSBATT BUSAPU BATTDIR BUSSERVICE BUSESS BUS第80页/共104页第八十一页，编辑于星期三：点 二十二分。82EMERG BUSBATT BUSAPU BATTDIR BUS

23、SERVICE BUSESS BUS第81页/共104页第八十二页，编辑于星期三：点 二十二分。83第82页/共104页第八十三页，编辑于星期三：点 二十二分。84第83页/共104页第八十四页，编辑于星期三：点 二十二分。85EMER PWR ONLY Msg1. ADG manual deploy handle PULLWhen ADG power is established:2. STAB TRIM CH 2 .ENGAGE3. Engine Instruments VERIFY N1, N2, & ITTBoth engines confirmed failed If Yes 4.

24、Double Engine Failure procedure (See Pge EMERG 1-5)ACCOMLISHBoth engines confirmed failed If no4. Cabin altitude.MONITOR5. Descent.AS REQUIREDAirplanes SN 7002 thru 73046. Airspeed.MAX 250 KIASAirplanes 7305 and subsequent第84页/共104页第八十五页，编辑于星期三：点 二十二分。86EMER PWR ONLY Msg6. No airspeed restrictions w

25、ith ADG deployedAirplanes 7002 thru 7304 With the ADG deployed during a windmilling start, an airspeed of 330 knots is permitted for 12 minutes or an airspeed of 335 knots is permitted for 4 minutes 7. GEN 1 and GEN .RESET/ON8. APU (30,000 feet & below).START9. APU GEN.ON After ADG deploy or APU GEN

26、 switching, check and reset QNH, ALT preselector, V-speed, and speed bug.Any generator comes on-line if YesRe-establish normal power10. ADG manual deploy handle.STOW11. ADG PWR TXFR.OVERRIDE第85页/共104页第八十六页，编辑于星期三：点 二十二分。87EMER PWR ONLY MsgAny generator comes on-line if Yes (Contd)12. CAS messagesREV

27、IEW13. Affected systems.RESTORE-END-Any generator comes on-line if NOContinue flight on emergency power only:10. DescentCONTINUE to 10,000 feet or lowest safe altitude11. RAM AIR.OPEN12. WING ANTI-ICESTBY if wing anti-ice is required13. Leave icing conditions14. Land at nearest suitable airport (con

28、td)第86页/共104页第八十七页，编辑于星期三：点 二十二分。88EMER PWR ONLY MsgThe following significant systems are not available when on emergency power only:Air-conditioning and pressurizationYaw damper 2 and AutopilotFlaps, flight and ground spoilersStab Trim channel 1, Mack Trim, aileron & rudder trimHyd pumps 1B, 2B, &

29、3ACopilots PFD, MFD, navigation and communications systemsDME 1 and 2Copilots instrument lights, NAV lights, and L&R landing and taxi lightsRight probe heaters and ice detectorsWindshield wipersBoth windshield & right window heaters Anti-skid systems and nosewheel steering第87页/共104页第八十八页，编辑于星期三：点 二十

30、二分。89EMER PWR ONLY MsgNOTE1.When the airplane is in battery power only (ADG inop), all electrical power may be lost after 30 minutes.2.Hydr pump 3B will be inop when on batt power only.Prior to Landing15. ANTI SKID switchOFF16. N/W STRG switchOFF17. GRND PROX, FLAP or GPWS/FLAP OVRD.OVRD18. Final ap

31、proach speed.VREF (Flaps +45) Vref + (flaps 0 ) 30 kts (flaps 8) 18 kts (flaps 20) 12 kts (flaps 30) 8 kts第88页/共104页第八十九页，编辑于星期三：点 二十二分。90EMER PWR ONLY Msg19. Actual landing distance is increased by a factor of:FlapsW/O Thrust ReverseWith Thrust reverse03.30 (230%)2.60 (160%)8 3.00 (200%)2.40 (140%)

32、20 2.65 (165%)2.10 (110%)30 2.55 (155%) 2.00 (100%)45 2.20 (120%) 1.80 (80%)With HYD PUMP 3B caution message on:20. Landing gear Manual Extension Procedure (See ABNORM 13-5)ACCOMPLISH-END-第89页/共104页第九十页，编辑于星期三：点 二十二分。91No. 2第90页/共104页第九十一页，编辑于星期三：点 二十二分。92EMER PWR ONLY Msg1. ADG manual deploy handle

33、 PULLWhen ADG power is established:2. STAB TRIM CH 2 .ENGAGE3. Engine Instruments VERIFY N1, N2, & ITTBoth engines confirmed failed If Yes 4. Double Engine Failure procedure (See Pge EMERG 1-5)ACCOMLISHBoth engines confirmed failed If no4. Cabin altitude.MONITOR5. Descent.AS REQUIREDAirplanes SN 700

34、2 thru 73046. Airspeed.MAX 250 KIASAirplanes 7305 and subsequent第91页/共104页第九十二页，编辑于星期三：点 二十二分。93EMER PWR ONLY Msg6. No airspeed restrictions with ADG deployedAirplanes 7002 thru 7304 With the ADG deployed during a windmilling start, an airspeed of 330 knots is permitted for 12 minutes or an airspeed

35、 of 335 knots is permitted for 4 minutes 7. GEN 1 and GEN .RESET/ON8. APU (30,000 feet & below).START9. APU GEN.ON After ADG deploy or APU GEN switching, check and reset QNH, ALT preselector, V-speed, and speed bug.Any generator comes on-line if YesRe-establish normal power10. ADG manual deploy hand

36、le.STOW11. ADG PWR TXFR.OVERRIDE第92页/共104页第九十三页，编辑于星期三：点 二十二分。94EMER PWR ONLY MsgAny generator comes on-line if Yes (Contd)12. CAS messagesREVIEW13. Affected systems.RESTORE-END-Any generator comes on-line if NOContinue flight on emergency power only:10. DescentCONTINUE to 10,000 feet or lowest safe

37、 altitude11. RAM AIR.OPEN12. WING ANTI-ICESTBY if wing anti-ice is required13. Leave icing conditions14. Land at nearest suitable airport (contd)第93页/共104页第九十四页，编辑于星期三：点 二十二分。95EMER PWR ONLY MsgThe following significant systems are not available when on emergency power only:Air-conditioning and pres

38、surizationYaw damper 2 and AutopilotFlaps, flight and ground spoilersStab Trim channel 1, Mack Trim, aileron & rudder trimHyd pumps 1B, 2B, & 3ACopilots PFD, MFD, navigation and communications systemsDME 1 and 2Copilots instrument lights, NAV lights, and L&R landing and taxi lightsRight probe heater

39、s and ice detectorsWindshield wipersBoth windshield & right window heaters Anti-skid systems and nosewheel steering第94页/共104页第九十五页，编辑于星期三：点 二十二分。96EMER PWR ONLY MsgNOTE1.When the airplane is in battery power only (ADG inop), all electrical power may be lost after 30 minutes.2.Hydr pump 3B will be in

40、op when on batt power only.Prior to Landing15. ANTI SKID switchOFF16. N/W STRG switchOFF17. GRND PROX, FLAP or GPWS/FLAP OVRD.OVRD18. Final approach speed.VREF (Flaps +45) Vref + (flaps 0 ) 30 kts (flaps 8) 18 kts (flaps 20) 12 kts (flaps 30) 8 kts第95页/共104页第九十六页，编辑于星期三：点 二十二分。97EMER PWR ONLY Msg19.

41、 Actual landing distance is increased by a factor of:FlapsW/O Thrust ReverseWith Thrust reverse03.30 (230%)2.60 (160%)8 3.00 (200%)2.40 (140%)20 2.65 (165%)2.10 (110%)30 2.55 (155%) 2.00 (100%)45 2.20 (120%) 1.80 (80%)20.Maximum landing weight.DETERMINENOTEBattery only operations with cabin altitude

42、s greater than 10,000 feet will result in the posting of the CABIN ALT warning message.第96页/共104页第九十七页，编辑于星期三：点 二十二分。98EMER PWR ONLY MsgFlaps position between 0 to 7 degreesOATAirport Pressure Altitude (Feet)CF1000110001200013000-40-4021085201401921018310-20-0419105182201736516545 003217390165801579

43、515040 257715590148551414513465Wind Corrections:HW increase landing weight for max ture speed by 2200 lbs per 10 kts HWTW decrease landing weight for max tire speed by 9500 lbs per 10 kts TWNOTEThe actual landing weight must not exceed the corrected maximum landing weight due to tire speed第97页/共104页

44、第九十八页，编辑于星期三：点 二十二分。99EMER PWR ONLY MsgFlaps position between 8 to 19 degreesOATAirport Pressure Altitude (Feet)CF1000110001200013000-40-4023610230502232521375-20-0422440215002059019710 003220800199251907018230 257718850180401725516500Wind Corrections:HW increase landing weight for max ture speed by

45、 2200 lbs per 10 kts HWTW decrease landing weight for max tire speed by 9500 lbs per 10 kts TWNOTEThe actual landing weight must not exceed the corrected maximum landing weight due to tire speed第98页/共104页第九十九页，编辑于星期三：点 二十二分。100EMER PWR ONLY MsgFlaps position between 20 to 29 degreesOATAirport Pressu

46、re Altitude (Feet)CF1000110001200013000-40-4024000240002356023000-20-0423700231002215521240 003222410214952061519765 257720580197401892518125Wind Corrections:HW increase landing weight for max ture speed by 2200 lbs per 10 kts HWTW decrease landing weight for max tire speed by 9500 lbs per 10 kts TW

47、NOTEThe actual landing weight must not exceed the corrected maximum landing weight due to tire speed第99页/共104页第一百页，编辑于星期三：点 二十二分。101EMER PWR ONLY MsgFlaps position between 30 to 44 degreesOATAirport Pressure Altitude (Feet)CF1000110001200013000-40-4024000240002400023875-20-0424000239602323022290 003

48、223495225602165520780 257721680208151997019160Wind Corrections:HW increase landing weight for max ture speed by 2200 lbs per 10 kts HWTW decrease landing weight for max tire speed by 9500 lbs per 10 kts TWNOTEThe actual landing weight must not exceed the corrected maximum landing weight due to tire speed-END-第100页/共104页第一百零一页，编辑于星期三：点 二十二分。102nMin 22 Volts required for dispatch第101页/共104页第一百零二页，编辑于星期三：点 二十二分。103第102页/共104页第一百零三页，编辑于星期三：点 二十二分。