B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
71-13-00-010-040 Opening of the Fan Cowl Doors 71-73-49-000-005 Removal of the Turbine Rear Frame TRF Drain Tube 78-30-00-481-041 Make the Thrust Reverser Unserviceable for
Maintenance
78-36-00-010-040 Opening of the Thrust Reverser Doors
R **ON A/C 001-049, 054-099, 101-149, 152-199, 211-299, 401-499,
78-11-11-991-301 Fig. 401
**ON A/C 051-053, 151-151, 201-210,
78-11-11-991-301-A Fig. 401A
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REFERENCE DESIGNATION
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**ON A/C 301-399,
78-11-11-991-301-B Fig. 401B R **ON A/C 001-049, 054-099, 101-149, 152-199, 211-299, 301-399, 401-499,
78-11-11-991-302 Fig. 402
**ON A/C 051-053, 151-151, 201-210,
78-11-11-991-302-A Fig. 402A
**ON A/C ALL
3. Job Set-up
__________
Subtask 78-11-11-941-051
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).
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Subtask 78-11-11-010-051
B. Get Access
(1) Open the fan cowl doors: (Ref. TASK 71-13-00-010-040) FOR 1000EM1 437AL, 438AR FOR 1000EM2 447AL, 448AR
(2) Put the access platform in position
Subtask 78-11-11-040-050
C. Make the thrust reverser unserviceable (Ref. TASK 78-30-00-481-041).
Subtask 78-11-11-010-052
D. Open the thrust reverser doors: (Ref. TASK 78-36-00-010-040)
FOR 1000EM1
451AL, 452AR
FOR 1000EM2
461AL, 462AR
4. Procedure
_________
R **ON A/C 001-049, 054-099, 101-149, 152-199, 211-299, 401-499,
(Ref. Fig. 401/TASK 78-11-11-991-301)
**ON A/C 051-053, 151-151, 201-210,
(Ref. Fig. 401A/TASK 78-11-11-991-301-A)
**ON A/C 301-399,
(Ref. Fig. 401B/TASK 78-11-11-991-301-B)
R **ON A/C 001-049, 054-099, 101-149, 152-199, 211-299, 301-399, 401-499,
(Ref. Fig. 402/TASK 78-11-11-991-302)
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Core Nozzle Assembly
Figure 401/TASK 78-11-11-991-301
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Core Nozzle Assembly
Figure 401A/TASK 78-11-11-991-301-A
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R Core Chevron Nozzle Assembly
R Figure 401B/TASK 78-11-11-991-301-B
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Parts That Attach The Core Nozzle Assembly
Figure 402/TASK 78-11-11-991-302
F 『R EEFF : 001-049, 054-099, 101-149, 152-199, E Page 40778-11-11 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機維護手冊 AMM EXHAUST 1(14)
