Subtask 05-51-12-410-050
K. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Install and/or close all the access doors and the panels applicable to this inspection.
(3)
Remove the warning notice(s).
(4)
Remove the access platform(s).
(5)
Close the main gear doors (Ref. TASK 32-12-00-410-001).
(6)
Close the nose gear doors (Ref. TASK 32-22-00-410-001).
Subtask 05-51-12-210-052
L. Retraction of the Flaps
(1) Make sure the flaps are retracted (Ref. TASK 27-50-00-866-009).
Subtask 05-51-12-700-050
M. Tests of the System (Ref. TASK 32-31-00-720-002) (Ref. TASK 27-54-00-710-001) (Ref. TASK 27-64-00-710-001) (Ref. TASK 32-12-00-710-002) (Ref. TASK 32-69-00-740-001)
-------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----|
R |1. | | If you found damage on the landing | | | | | | | | | gear, the attached parts or the | | | | | | | | | adjacent structure: | | | | | | | | | - Do a functional test of the landing | | X | | | | | | | gear | | | | | | | | | (Ref. TASK 32-31-00-720-002). | | | | | | | | | Make sure that it moves smoothly and| | | | | | | | | freely. | | | | | | | | | | | | | | | |2. | | If you found damage on the doors, | | | | | | | | | their attached parts or the adjacent | | | | | | | | | structure: | | | | | | -------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----|
| | | - Do an operational test of the main | | X | | | | | | | landing gear doors | | | | | | | | | (Ref. TASK 32-12-00-710-002). | | | | | | | | | | | | | | | |3. | | If you found damage on the wing: | | | | | | | | | Do an operational test of the flaps | | X | | | | | | | and the spoilers | | | | | | | | | (Ref. TASK 27-54-00-710-001) | | | | | | | | | (Ref. TASK 27-64-00-710-001). | | | | | | | | | Make sure that they move smoothly and | | | | | | | | | freely. | | | | | | | | | | | | | | | |4. | | Do a BITE test of the proximity | X | | | | | | | | detectors | | | | | | | | | (Ref. TASK 32-69-00-740-001). | | | | | | -------------------------------------------------------------------------------
5. Close-up
________
Subtask 05-51-12-942-050
A. Remove the ground support and maintenance equipment, the special and standard tools and all other items.
1EFF : ALL 1 05-51-12Page 620 1 1 Nov 01/00R 1 1 1CES 1
INSPECTION AFTER FLAP/SLAT LIMITING SPEED EXCEEDED - INSPECTION/CHECK_____________________________________________________________________
TASK 05-51-13-200-001
Inspection after Flap/Slat Extension at more than the Flap/Slat Limiting Speed
1. Reason for the Job__________________
This inspection is necessary after an activation of the overspeed aural warning: - If the overspeed was not more than 10 Kts higher than the value shown on the VFE placard, only an extension and retraction test of the flaps and slats is necessary (refer to the operational test of the Flight Control Surfaces paragraph given in this procedure).
NOTE : If you find unsatisfactory condition(s) during the operational test,____ you must do the full inspection given in this procedure.
R R R R - If the overspeed was more than 10 Kts higher than the value shown on the VFE placard, you must do the full inspection given in this procedure. - If activation of the overspeed warning occurred during movement of the flap and slat control lever from the position 0 to the position 1, it is not necessary to do the inspection and the operational test of the flap system (steps 4.C and 4.E.1 of this procedure).
R R R NOTE : You can get confirmation of the slat and/or flap movement from the____ flight data recorder. If these data are not available, you must do the maintenance actions applicable to the pilot's report.
2. Job Set-up Information______________________
A. Fixtures, Tools, Test and Support Equipment
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REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
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本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM 時(shí)間限制/維護(hù)檢查 4(18)
