(19) Open the line blocks (15) and (25) at station 158.
(20) If necessary, remove the rubber supports from the line blocks (15) and (25).
(21) Remove the harness (5) from the rubber supports.
(22) Remove the bolt, clamps and anti-rotation lug (27) that attaches the harness (5) to the bracket at station 158.
(23) Remove the bolt and clamp (32) that attaches the harness (5) to the bracket at station 167.
END SPIB NO. CFM02255MW1
(24) Disconnect the electrical connector 4000WD1-A from the fire detector loop A.
(25) Remove the electrical harness (5) from the engine.
(26) Put protective covers on the electrical connectors.
F 『 EEFF : ALL E Page A47971-51-43
E E Feb 01/05 ERE
ECES E
F 『
E C F M E
E E
E 56-5B E
E E
TASK 71-51-43-400-002
Installation of the Fire Detector (Channel A) Harness (4202KS)
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific warning notice
No specific access platform 1 m (3 ft. 3 in.)
R No specific Torque Wrench : range 5.00 to 35.00 lbf.in
R (0.05 to 0.40 m.daN)
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power
26-12-00-710-001 Operational Check of Loop/Squib
31-60-00-860-001 EIS Start Procedure
31-60-00-860-002 EIS Stop Procedure
70-60-00-910-041 Nacelle Maintenance Practices
71-13-00-010-040 Opening of the Fan Cowl Doors
71-13-00-410-040 Closing of the Fan Cowl Doors
71-51-43-991-310 Fig. 416
F 『 EEFF : ALL E Page A48071-51-43
E E May 01/05 E E ECES E
F 『
E C F M E
E E
E 56-5B E
E E
3. Job Set-up
__________
Subtask 71-51-43-860-081
A. Aircraft Maintenance Configuration
(1) On the center pedestal, on the ENG panel 115VU, make sure that a warning notice is in position to tell persons not to start the engine.
(2) On the overhead maintenance panel 50VU, make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off. Make sure that a warning notice is in position to tell persons not to energize the FADEC 1(2).
(3) Make sure that the access platform is in position.
Subtask 71-51-43-010-076
B. Get Access
(1) Make sure that the fan cowls are open: (Ref. TASK 71-13-00-010-040) FOR 1000EM1 437AL, 438AR FOR 1000EM2 447AL, 448AR
Subtask 71-51-43-865-084
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------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,
49VU ANTI ICE/RAIN/RPLNT/CAPT 1DB1 D01
F 『 EEFF : ALL E Page A48171-51-43
E E Aug 01/05 E E ECES E -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------**ON A/C ALL
F 『
E C F M E
E E
E 56-5B E
E E
121VU RCDR/DFDR 7TU K16 121VU HYDRAULIC/HYD POWER/Y 3803GX N30 122VU ANTI ICE/WINDOWS/R 4DG2 W14 122VU ANTI ICE/WINDOWS/L 4DG1 X14 122VU ANTI ICE/PROBES/2/PITOT 3DA2 Y14 122VU ANTI ICE/PROBES/2/AOA 4DA2 Y13 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
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(62)
