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时间:2011-03-27 17:14来源:蓝天飞行翻译 作者:航空
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 31-60-00-860-001  EIS Start Procedure
 31-60-00-860-002 71-13-00-010-040 71-13-00-410-040 FOR FIN 1000EM1 EIS Stop ProcedureOpening of the Fan Cowl DoorsClosing of the Fan Cowl Doors
 29-23-00-863-001 29-23-00-864-001 FOR FIN 1000EM2 Pressurize the Green Hydraulic System from the Yellow Hydraulic System through the PTU with the Electric PumpDepressurize the Green and Yellow Hydraulic Systems after Operation of the PTU
 29-24-00-863-001 29-24-00-864-001  Pressurize the Yellow Hydraulic System with the Electric PumpDepressurize the Yellow Hydraulic System

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 3. Job Set-up__________
 Subtask 78-31-00-860-055
 A. On the fuel control panel 40VU, make sure that:
 WARNING : MAKE SURE THAT THE PUMPS CAN NOT OPERATE AUTOMATICALLY. THIS IS
_______ TO PREVENT INJURY TO PERSONS WHEN YOU ENERGIZE THE AIRCRAFT ELECTRICAL CIRCUITS.
 (1) The OFF legend of the HYD/BLUE/ELEC PUMP pushbutton switch is on.

 (2) The ON legend of the HYD/YELLOW/ELEC PUMP pushbutton switch is off.


 Subtask 78-31-00-861-051
 B. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
 Subtask 78-31-00-865-051
 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU ANTI ICE/PROBES/AOA/1 4DA1 D04 49VU ANTI ICE/PROBES/PHC/1 2DA1 D03 49VU ANTI ICE/PROBES/PITOT/1 3DA1 D02 122VU ANTI ICE/WINDOWS/R 4DG2 W14 122VU ANTI ICE/WINDOWS/L 4DG1 X14 122VU ANTI ICE/PROBES/PHC/3 2DA3 Y16 122VU ANTI ICE/PROBES/2/TAT 1DA2 Y15 122VU ANTI ICE/PROBES/2/PITOT 3DA2 Y14 122VU ANTI ICE/PROBES/2/AOA 4DA2 Y13 122VU ANTI ICE/PROBES/2/PHC 2DA2 Y12 122VU ANTI ICE/PROBES/2/STATIC 5DA2 Y11 122VU ANTI ICE/PROBES/3/PITOT 3DA3 Z16 122VU ANTI ICE/PROBES/3/AOA 4DA3 Z15 122VU ANTI ICE/PROBES/3/STATIC 5DA3 Z14 122VU ANTI ICE/PROBES/1/STATIC 5DA1 Z13 122VU ANTI ICE/PROBES/1/TAT 1DA1 Z12 123VU ANTI ICE/L/WHSLD 1DG1 AF10 123VU ANTI ICE/R/WHSLD 1DG2 AF03
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 D. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU ENGINE/1 AND 2/IGN/SYS A 1JH A03 49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08 121VU HYDRAULIC/SOL VALVES/G/Y/B/LEAK/TST 1881GP N35
 FOR 1000EM1 49VU ENGINE/1/FADEC A/AND EIU 1 2KS1 A04 121VU ENGINE/IGN/ENG1/SYS B 3JH1 P41 121VU ENGINE/IGN/ENG1/SYS A BAT 2JH1 P39 121VU ENGINE/ENG1/FADEC B/AND EIU 1 4KS1 R41
 FOR 1000EM2 49VU ENGINE/2/FADEC A/AND EIU 2 2KS2 A05 121VU ENGINE/IGN/ENG2/SYS B 3JH2 P42 121VU ENGINE/IGN/ENG2/SYS A BAT 2JH2 P40 121VU ENGINE/ENG2/FADEC B 4KS2 Q40
 Subtask 78-31-00-860-056
 E. Aircraft Maintenance Configuration
 (1) On the overhead maintenance panel 50VU:

 (a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off (the pushbutton switch is pushed in).

 (2) Do the EIS start procedure (ECAM display units only). (Ref. TASK 31-60-00-860-001).


 Subtask 78-31-00-010-050
 F. Open the fan cowl doors: (Ref. TASK 71-13-00-010-040)
 FOR 1000EM1
 437AL, 438AR
 FOR 1000EM2
 447AL, 448AR

 Subtask 78-31-00-020-050
 G. On the accessory gearbox of the engine 1(2):
 (1) Disconnect the two connectors (channel A and channel B) from the N2 speed sensor.
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 H. Install a Low Frequency Generator:
 WARNING : MAKE SURE THAT THE LOW FREQUENCY GENERATOR AND ITS WIRING ARE
_______ NOT IN THE DEPLOYMENT RANGE OF THE THRUST REVERSERS.
 (1) Connect a low frequency generator, (sinusoidal waveform, output voltage 10/15 volts) across the terminals 2(+) and 1(-).
 4. Procedure
_________
 Subtask 78-31-00-710-051
 A. Do this test:
 WARNING : MAKE SURE THAT THE TRAVEL RANGE OF THE THRUST REVERSER IS CLEAR
 
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