(5) Close the cargo door (Ref. TASK 52-30-00-860-002). R **ON A/C 001-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
Subtask 52-31-11-220-056-A
D. Dimensional Check
(1) Make sure that the clearances of latching hooks (3) and the roller
(4) between FR25A and FR27 are correct.
NOTE : The permitted clearance is 0.2 mm (0.0078 in.)
____
(2)
Install the access panel(s) 825AR.
(3)
Make sure that the applicable access panel is in line with the fuselage contour of the door sill area.
NOTE : The permitted tolerance of the skin offset is -1.5 mm (-0.0590
____
in.).
(4)
Measure the gap "G" between the applicable access panel and the door sill edge of the fuselage.
(5)
Make sure that the subsequent clearances are correct (Ref. TASK 52-31-00-710-001) during the cargo door starts to open:
-between the latching hooks and the door frame fittings,
-between the latching hooks and the door sill.
**ON A/C 051-052,
Subtask 52-31-11-220-056
D. Dimensional Check
(1) Make sure that the clearances of locking hooks (3) and the roller (4) between FR25A and FR27 are correct.
NOTE : The permitted clearance is 0.2 mm (0.0078 in.)
____
(2) Install the access panel(s) 825AR.
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(3) Make sure that the applicable access panel is in line with the fuselage contour of the door sill area.
NOTE : The permitted tolerance of the skin offset is -1.5 mm (-0.0590
____
in.).
(4)
Measure the gap "G" between the applicable access panel and the door sill edge of the fuselage.
(5)
Make sure that the subsequent clearances are correct (Ref. TASK 52-31-00-710-001) during the cargo door starts to open:
-between the locking hooks and the door frame fittings,
-between the locking hooks and the door sill. **ON A/C ALL
5. Close-up
________ Subtask 52-31-11-410-072
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the access platform(s).
(3)
Make sure that the applicable cargo door is correctly closed and locked (Ref. TASK 52-30-00-860-002).
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TASK 52-31-11-820-002
Adjustment of the Door Mechanism
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
No specific mounting nut (e.g. NAS 509-4)
R No specific access platform 3.5 m (11 ft. 6 in.)
R 98D52307525000 1 ADJUSTMENT TOOL - CARGO DOORS
R 98D52308308000 1 PIN - RIGGING, CARGO COMPARTMENT DOOR
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
No specific lockwire, corrosion resistant steel, 0.8 mm (0.032 in.) Material No. 09-003 C Z-16.115 SEALANT,POLYSULFIDE (USE 09-018) (Ref. 20-31-00)
Material No. 19-010 USA AMS 5687
LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
(Ref. 20-31-00)
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C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
1 cotter pin 52-31-21 03 -420 8 tab washer 52-31-21 03 -350 14 tab washer 52-31-21 02 -140
R 17 tab washer 52-31-21 02 -140 30 cotter pin 52-31-21 19 -010 35 cotter pin 52-31-21 16 -010 42 cotter pin 52-31-21 16 -050 43 cotter pin 52-31-21 16 -050 50 cotter pin 52-31-21 16 -010 55 tap washer 52-31-21 20B-100 60 cotter pin 52-31-21 20B-010 66 cotter pin 52-31-21 20B-010 68 tab washer 52-31-21 20B-100 103 tab washer 52-31-21 15 -080
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本文鏈接地址：A320飛機維護手冊 AMM DOORS 艙門4(51)
