Subtask 05-51-27-010-050

 B. Get Access
 (1) Open the fan cowl doors (Ref. TASK 71-13-00-010-040).
 (2) Open the thrust reverser doors (Ref. TASK 78-36-00-010-040).
 (3) Put an adjustable access platform near the damaged engine.
 4. Procedure_________
 Subtask 05-51-27-210-050
 A. Inspection of the Engine
 NOTE : All the necessary inspections are visual unless the text gives____ other instructions. Operators can refer to the Non-destructive Testing Manual (NTM) and use non-destructive procedures. 
R  (Ref. TASK 71-00-00-000-042) (Ref. TASK 71-00-00-400-042)
 -------------------------------------------------------------------------------
R R R R  |ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the cowls after a side | | | | | | | | | impact and damage only to the cowls. | | | | | | | | | | | | | | | |  A.| | Externally examine the fitting related|  X  | | | | | | | | to the cowl with the adjacent area of | | | | | | | | | the pylon: | | | | | | | | | (1) Pylon lateral panels when damage | | | | | | | | | is on the thrust reverser or core | | | | | | | | | cowls. | | | | | | | | | (2) Cantilever structure when damage | | | | | | | | | is on the inlet cowl, fan cowl or | | | | | | | | | thrust reverser. | | | | | | | | | | | | | | | |2. | | Inspection after a side impact and | | | | | | | | | subsequent damage to the engine or the| | | | | | | | | equipment/accessories attached to it. | | | | | | | | | | | | | | | |  A.| | Examine the pylon panels, doors and |  X  | | | | | | | | auxiliary structure for distortion, | | | | | | | | | wrinkles, buckles, tearing of plates | | | | | | | | | at the rivets and stringers attached | | | | | |

 1EFF : ALL 1 05-51-27Page 602

1 1 May 01/05 1 1 1CES 1

 -------------------------------------------------------------------------------
|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| R | | | to the panels. | | | | | | | | | | | | | | | |  B.| | Examine the pylon main frame for |  X  | | | | | R | | | distortion, cracks, cracked or flaking| | | | | | R | | | paint, loose rivets and signs of | | | | | | | | | shearing. | | | | | | | | | If you find damage: | | | | | | | | | (1) Examine the panels and adjacent | |  X  | | | | | | | structure for distortion, | | | | | | R | | | wrinkles, buckles, tearing of | | | | | | | | | plates at the rivets and stringers| | | | | | | | | attached to the panels. | | | | | | | | | (2) Examine the pylon main frame for  | |  X  | | | | | | | distortion and condition of spars | | | | | | | | | and ribs connected to the lateral | | | | | | | | | panels. | | | | | | | | | If you find damage: | | | | | | | | | (a) Remove the engine | | |  X  | | | | | | (Ref. TASK 71-00-00-000-042). | | | | | | | | | (b) Examine the FWD and Aft engine | | |  X  | | | | | | pylon attachments for distortion | | | | | | | | | or cracks. | | | | | | | | | (c) Remove the pylon-to-wing center | | |  X  | | | | | | fillets. | | | | | | | | | (d) Examine the pylon-to-wing attach  | | |  X  | | | | | | fittings for distortion or | | | | | | | | | cracks. | | | | | | | | | (e) Install the engine | | |  X  | | | | | | (Ref. TASK 71-00-00-400-042). | | | | | | -------------------------------------------------------------------------------
5. Close-up
________
 Subtask 05-51-27-410-050
 A. Close Access
 (1)
 Close the thrust reverser doors (Ref. TASK 78-36-00-410-040).

 (2)
 Close the fan cowl doors (Ref. TASK 71-13-00-410-040).

 Subtask 05-51-27-942-050

 B. Put the aircraft back to its initial configuration.
 (1)
 Remove the warning notice(s).

 (2)
 Remove the access platform(s).

 1EFF : ALL 1 05-51-27Page 604 1 1 May 01/05R 1 1 1CES 1

 PROCEDURE AFTER FLUID SPILLAGE - INSPECTION/CHECK
_________________________________________________
 TASK 05-51-28-200-002
 Procedure after Fluid Spillage
 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
R A. Referenced Information
R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護(hù)手冊 AMM 時間限制/維護(hù)檢查 4(111)