4. Procedure
_________
Subtask 05-51-24-210-050
A. General
NOTE : You can do non-destructive tests (refer to the Aircraft
____
Non-destructive Testing Manual) if:
-You think it is necessary.
-The Airworthiness Authority tells you to.
-Airbus Industrie tell you to.
All the inspections are visual unless you get other instructions.
Subtask 05-51-24-210-053
B. Inspection of the Fuselage
-------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Fuselage bottom-surface | | | | | | | | | | | | | | | | A.| | Externally examine all the bottom-| X | | | | | | | | surface of the fuselage for dents, | | | | | | | | | distortion, cracks, pulled or torn | | | | | | | | | fasteners and damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Internally examine at and adjacent| | X | | | | | | | to the damaged area, all the | | | | | | | | | frames, stringers, joints and | | | | | | | | | cleats for damage. | | | | | | | | | (2) Inspect all the components, pipes,| | X | | | | | | | ducts and cables adjacent to the | | | | | | | | | damaged area for damage or | | | | | | | | | leakage. | | | | | | | | | | | | | | | |2. | | NLG Doors | | | | | | | | | | | | | | | | A.| | Examine the NLG doors for holes, | X | | | | | | | | delamination, cracked or flaking | | | | | | | | | paint, loose fasteners and correct | | | | | | | | | attachment. | | | | | | | | | | | | | | | |3. | | MLG Doors | | | | | | | | | | | | | | | | A.| | Examine the MLG doors for holes, | X | | | | |
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|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | delamination, cracked or flaking | | | | | | | | | paint, loose fasteners and correct | | | | | | | | | attachment. | | | | | | | | | | | | | | | |4. | | Belly Fairing | | | | | | | | | | | | | | | | A.| | Examine the belly fairing panels for | X | | | | | | | | holes, delamination, cracked or | | | | | | | | | flaking paint, loose fasteners and | | | | | | | | | correct attachment. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove the panels and internally | | X | | | | | | | examine the belly fairing | | | | | | | | | structure for bucklings, cracks | | | | | | | | | and damaged paintwork. | | | | | | | | | (2) Examine the pipes, ducts, | | X | | | | | | | electrical looms and their | | | | | | | | | supports for: | | | | | | | | | - fluid leakage, distortion, | | | | | | | | | rupture, breaks, cracks, correct | | | | | | | | | attachment and the condition of | | | | | | | | | the safety devices. | | | | | | | | | | | | | | | | B.| | Examine the air-conditioning pack | X | | | | | | | | intakes for unwanted material and | | | | | | | | | damage from hits. | | | | | | | | | | | | | | | |5. | | APU Intake | | | | | | | | | | | | | | | | A.| | Examine the APU intake for unwanted | X | | | | | | | | material and damage from hits. | | | | | | -------------------------------------------------------------------------------
Subtask 05-51-24-210-054
C. Inspection of the Landing Gears (Ref. TASK 07-11-00-581-003) (Ref. TASK 07-11-00-586-001) (Ref. TASK 12-14-32-614-004) (Ref. TASK 32-21-00-200-005) (Ref. TASK 32-31-00-720-003) (Ref. TASK 32-21-11-000-002) (Ref. TASK 32-21-11-400-002) (Ref. TASK 32-21-17-000-001) (Ref. TASK 32-21-17-400-001) (Ref. TASK 32-21-16-000-002) (Ref. TASK 32-21-16-400-002) (Ref. TASK 32-31-22-000-001) (Ref. TASK 32-31-22-400-001) (Ref. TASK 32-41-12-000-001)
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(Ref. TASK 32-41-12-400-001) (Ref. TASK 32-41-12-000-002) (Ref. TASK 32-41-12-400-002) (Ref. TASK 32-21-13-000-001)
(Ref. TASK 32-21-13-400-001) (Ref. TASK 32-21-00-200-006) (Ref. TASK 07-11-00-581-001) (Ref. TASK 07-11-00-586-002) (Ref. TASK 32-11-00-200-003)
(Ref. TASK 32-11-00-200-005) (Ref. TASK 32-31-00-720-002) (Ref. TASK 32-33-00-720-001) (Ref. TASK 32-11-11-000-001)
(Ref. TASK 32-11-11-400-001) (Ref. TASK 32-11-16-000-001) (Ref. TASK 32-11-16-400-001) (Ref. TASK 32-11-17-000-001) (Ref. TASK 32-11-17-400-001)
(Ref. TASK 32-11-21-000-001) (Ref. TASK 32-11-21-400-001) (Ref. TASK 32-31-46-000-001) (Ref. TASK 32-31-46-400-001)
(Ref. TASK 32-11-00-200-006) (Ref. TASK 05-51-16-200-001) (Ref. TASK 32-11-13-000-001) (Ref. TASK 32-11-13-400-001) (Ref. TASK 32-11-00-220-004)
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