A320飞机维护手册 AMM EXHAUST 1(14)

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 TASK 78-11-11-000-041
 Removal of the Core Nozzle Assembly
 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.)
 RSE1133 1 HANDLING SLING

 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
 -------------------------------------------------------------------------------
**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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 E E Aug 01/05 E E ECES E F 『 E C F M E E E E 56-5B E

 

 Core Nozzle Assembly
 Figure 401/TASK 78-11-11-991-301

 F 『R EEFF : 001-049, 054-099, 101-149, 152-199, E Page 40478-11-11
 E E211-299, 401-499, Aug 01/05 E E ECES E F 『 E C F M E E E E 56-5B E

 

 Core Nozzle Assembly
 Figure 401A/TASK 78-11-11-991-301-A

 F 『R EEFF : 051-053, 151-151, 201-210, E Page 40578-11-11
 E E May 01/05 E E ECES E F 『 E C F M E E E E 56-5B E F 『 E C F M E E E

 

R  Core Chevron Nozzle Assembly 
R  Figure 401B/TASK 78-11-11-991-301-B
 F R EEFF :  301-399,  『 E 78-11-11 Page 406 
E  E  Feb 01/05
 E  E
 ECES  E

 

 E 56-5B E

 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
　
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