F 『
E C F M E
E E
E 56-5B E
E E
R (26) Attach the harness (30) to the bracket with the clamp (50) and the bolt (45).
R (27) TORQUE the bolt (45) to between 20 and 25 lbf.in (0.22 and 0.28 m.daN).
R (28) Put the harness into the flip-lock clamps (5) and tighten the captive screws.
**ON A/C ALL
Subtask 71-51-43-865-064
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 71-51-43-861-051
C. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002) Subtask 71-51-43-860-057
D. Do the EIS start procedure (for the lower display of the ECAM system only). (Ref. TASK 31-60-00-860-001).
Subtask 71-51-43-710-050
E. Do an operational test of the thrust reverser system (Ref. TASK 78-31-00-710-042) .
5. Close-up
________
Subtask 71-51-43-862-051
A. De-energize the aircraft circuits (Ref. TASK 24-41-00-862-002)
F 『 EEFF : ALL E Page 43671-51-43
E E Feb 01/04 E E ECES E Subtask 71-51-43-410-054
F 『
E C F M E
E E
E 56-5B E
E E
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other items.
(2) Close the fan cowls: (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).
F 『 EEFF : ALL E Page 43771-51-43
E E Feb 01/04 ERE
ECES E
F 『
E C F M E
E E
E 56-5B E
E E
TASK 71-51-43-000-045
Removal of the IDG Control and Anti-Ice Harness (4215KS)
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 71-51-43-991-303 Fig. 404 71-51-43-991-304 Fig. 405
3. Job Set-up
__________ Subtask 71-51-43-941-055
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.
F 『 EEFF : ALL E Page 43871-51-43
E E Feb 01/04 ERE
ECES E
F 『
E C F M E
E E
E 56-5B E
E E
(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 71-51-43-865-065
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,
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:A320飞机维护手册 AMM 动力装置 POWER PLANT 2(25)