A320飞机维护手册 AMM 动力装置 POWER PLANT 1(50)

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 FOR 1000EM2
 49VU ENGINE/2/FADEC A/AND EIU 2 2KS2 A05 121VU ENGINE/ENG2/OIL/PRESS 2EN2 N42 121VU ENGINE/ENG2/OIL/QTY 1EN2 N41 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 71-00-00-865-067
 D. 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
R  **ON A/C 001-049, 051-052, 054-056, 058-059, 061-099, 101-101, 103-149,
R  151-199, 201-299, 301-399, 401-499, Post SB 30-1037 For A/C 001-049,051-052,054-056,
 49VU ANTI ICE/RAIN/RPLNT/CAPT  1DB1 D01
 **ON A/C ALL
 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
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 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------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
R **ON A/C 001-049, 051-052, 054-056, 058-059, 061-099, 101-101, 103-149, R 151-199, 201-299, 301-399, 401-499, Post SB 30-1037 For A/C 001-049,051-052,054-056,
 122VU ANTI ICE/RAIN/RPLNT/F/O 1DB2 W11
 **ON A/C ALL
 Subtask 71-00-00-869-100
 E. Continue to prepare for test
 (1) Do the EIS start procedure (Ref. TASK 31-60-00-860-001).

 (2) Make sure that fire fighting personnel is there.

 (3) On the lower ECAM display unit:

 CAUTION : MAKE SURE THAT THE HYDRAULIC RESERVOIR PRESSURE IS IN THE
_______ CORRECT OPERATION RANGE BEFORE YOU START THE ENGINE. THE HYDRAULIC FLUID IS NECESSARY TO LUBRICATE THE HYDRAULIC PUMPS THAT THE ENGINE OPERATES.
 (a) Get the HYDRAULIC page.

 (b) Make sure that the pressure of the Green reservoir for the engine 1 (Yellow reservoir for the engine 2) is correct.

 (c) Make sure that the reservoir fluid level is correct.

 (4) Make sure that the engine 1(2) pump is serviceable (on the HYD/FUEL panel 40VU, the OFF legend of the ENG 1(2) PUMP pushbutton switch must be off).
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 Subtask 71-00-00-710-076

 F. Do the operational test of the engine fire and overheat detection (loop/squib) (Ref. TASK 26-12-00-710-001).
 Subtask 71-00-00-869-101
 G. Continue to prepare for test
 (1) On the RUD TRIM/PARKING BRK panel 110VU:

 (a) Make sure that the parking-brake control switch is set to ON.

 (2) On the ENG panel 115VU:

 (a) Make sure that the ENG/MASTER 1(2) control switch is set to OFF.

 (3) Make sure that the throttle control lever of the engine 1(2) is in the idle stop position (zero on the graduated sector).

 (4) On the center instrument panel 400VU, make sure that:

 (a) The brake pressure indication on the brake Yellow-pressure triple-indicator is correct. If necessary, pressurize the brake accumulator with Yellow pump (Ref. TASK 29-10-00-863-002).

 (b) The landing-gear normal control-lever is in the DOWN position.

 

 (5) Make sure that the interphone system operates correctly.

 (6) Make sure that the aircraft is cleared and that nobody remains in the dangerous areas.

 (7) On the lower ECAM display unit:

 (a) Get the FUEL page. Make sure that there is the correct quantity of fuel in the fuel tanks to run the engine.

 (8) On the HYD/FUEL panel 40VU:

 (a) Push all the FUEL/PUMPS pushbutton switches (the OFF legends of these pushbutton switches go off).

 (9) Supply the aircraft pneumatic system from a HP ground power unit or the APU (Ref. TASK 36-12-00-860-001) or (Ref. TASK 36-12-00-860-002).

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