Subtask 71-51-43-865-061
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 3DA1, 3DA2, 3DA3, 4DA1, 4DA2, 4DA3, 5DA1, 5DA2, 5DA3, 1DB1, 1DB2, 4DG1, 4DG2, 1JH, 3801GX, 3802GX, 3803GX, 7TU, 2RK, 4RK FOR 1000EM1 2KS1, 4KS1, 2JH1, 3JH1, 1WE1, 2WE1, 7WD1, 8WD1, 2XU1 FOR 1000EM2 2KS2, 4KS2, 2JH2, 3JH2, 1WE2, 2WE2, 7WD2, 8WD2, 2XU2
Subtask 71-51-43-861-050
C. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002) Subtask 71-51-43-860-054
D. Aircraft Maintenance Configuration
(1) Do the EIS start procedure (for the lower display of the ECAM system only).
E. Do the EIS start procedure (for the lower display of the ECAM system only).
(1) Pressurize the aircraft pneumatic system with a (Ref. TASK 31-60-00-860-001) or through the APU.
Subtask 71-51-43-869-050
E. Do this test
(1) Start the engine. Let it become stable at the idle speed. (Ref. TASK 71-00-00-710-003).
(2) On the ECAM control panel, get the ELEC page. On the lower display unit of the ECAM system:
(a) make sure that the voltage and frequency are correct.
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(3) Stop the engine. (Ref. TASK 71-00-00-710-028).
5. Close-up
________ Subtask 71-51-43-860-055
A. Do the EIS stop procedure (Ref. TASK 31-60-00-860-002) Subtask 71-51-43-862-050
B. De-energize the aircraft circuits (Ref. TASK 24-41-00-862-002) Subtask 71-51-43-869-051
C. Depressurize the pneumatic system. Subtask 71-51-43-410-053
D. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other items.
(2) Close the fan cowl doors: (Ref. TASK 71-13-00-410-040)
FOR 1000EM1
437AL, 438AR
FOR 1000EM2
447AL, 448AR
(3) Remove the access platform(s).
(4) Remove the warning notice(s).
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TASK 71-51-43-000-044
Removal of the Thrust Reverser (Channel A and B) Harness (4200KS)
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
No specific protective covers
No specific warning notice
No specific access platform 1 m (3 ft. 3 in.)
B. Referenced Information -------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
71-13-00-010-040 Opening of the Fan Cowl Doors
R **ON A/C 001-049, 051-099, 101-149, 151-152, 154-199, 201-299, 301-399, R 401-499, 71-51-43-991-302 Fig. 403 **ON A/C 153-153,
71-51-43-991-302-A Fig. 403A
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**ON A/C ALL
3. Job Set-up
__________
Subtask 71-51-43-941-054
A. Safety Precautions
(1) On the center pedestal, on the ENG panel 115VU:
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure.
(3) 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.
(b) Put a warning notice to tell persons not to energize the FADEC 1(2).
Subtask 71-51-43-865-062
B. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU ENGINE/1 AND 2/IGN/SYS A 1JH A03 49VU ANTI ICE/PROBES/AOA/1 4DA1 D04 49VU ANTI ICE/PROBES/PITOT/1 3DA1 D02 49VU COM/CVR/SPLY 2RK E14 49VU COM/CVR/CTL 4RK E13
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,
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本文链接地址：A320飞机维护手册 AMM 动力装置 POWER PLANT 2(19)
