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)
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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 | | | | | |
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|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).
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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 -------------------------------------------------------------------------------
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