(2)
Clean the component interface and/or the adjacent area.
(3)
Do an inspection of the component interface and/or the adjacent area.
1EFF : ALL 1 52-32-31Page 411 1 1 Aug 01/02 1 1 1CES 1
(4)
Apply SEALANTS (Material No. 09-019) to the countersink of the screws
(1),(3),(10) and (12).
(5)
Apply SEALANTS (Material No. 09-019) to the mating surface of the shims (4) and (13) and the X-stops (2) and (11).
**ON A/C 001-049, 051-099, 101-149, 201-299, 301-399,
Subtask 52-32-31-420-051
B. Installation of the X-Stops
(1)
Put the shims (4) and (13) and the X-stops (2) and (11) on the sides of the cargo door and attach them with the screws (1),(10).
(2)
Install the screws (3) and (12) with the washers (6) and (15) and the nuts (5) and (14).
(3)
Remove the actuator safety locks and close the AFT cargo door (Ref. TASK 52-30-00-860-002).
(4)
Measure the gaps between the X-stops of the AFT cargo door and the door frames of the fuselage.
NOTE : The gap
____
-
at FR52A must be between 3.5 mm (0.1377 in.) and 4.5 mm (0.1771 in.)
-
at FR56 must be between 0.3 mm (0.0118 in.) and 1.3 mm (0.0511 in.).
(5) If the gaps are out of the tolerances, add or remove the shim(s) (4) and/or (13) as required.
R **ON A/C 151-199, 401-499,
Subtask 52-32-31-420-051-A
B. Installation of the X-Stops
(1)
Put the shims (4) and (13) and the X-stops (2) and (11) on the sides of the cargo door and attach them with the screws (1),(10).
(2)
Install the screws (3) and (12) with the washers (6) and (15) and the nuts (5) and (14).
1EFF : ALL 1 52-32-31Page 412 1 1 Aug 01/05 1 1 1CES 1 1EFF : ALL 1 52-32-31Page 413 1 1 Aug 01/02 1 1 1CES 1
R R (3) Remove the actuator safety locks and close the AFT cargo door (Ref. TASK 52-30-00-860-002).
R R (4) Measure the gaps between the X-stops of the AFT cargo door and the door frames of the fuselage.
R R R R R NOTE : The gap____ - at FR55A must be between 2.5 mm (0.0984 in.) and 3.5 mm (0.1377 in.) - at FR59 must be between 1.6 mm (0.0629 in.) and 2.6 mm (0.1023 in.).
R R (5) If the gaps are out of the tolerances, add or remove the shim(s) (4) and/or (13) as required.
R **ON A/C ALL
Subtask 52-32-31-916-050
C. Protective Treatment
(1) Apply a bead of SEALANTS (Material No. 09-019) around the shims (4) and (13) and the X-stops (2) and (11).
(2) Apply SEALANTS (Material No. 09-019) to the threaded ends of the screws (3) and (12).
5. Close-up________
Subtask 52-32-31-865-055
A. Make sure that this(these) circuit breaker(s) is(are) closed: 1MJ
Subtask 52-32-31-410-051
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other items.
(2) Install the lateral lining and insulation components on the AFT cargo door (Ref. TASK 52-31-13-400-001).
(3) Install the fairing on the outer skin of the AFT cargo door (Ref. TASK 53-35-13-400-001).
(4)
Install the access panel 826AR.
(5)
Remove the access platform(s).
1EFF : ALL 1 52-32-31Page 414 1 1 Aug 01/02R 1 1 1CES 1
FITTINGS - DOOR FRAME - REMOVAL/INSTALLATION
____________________________________________ TASK 52-32-32-000-001 R Removal of the Lock Fitting Components
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 access platform 2.0 m (6 ft. 7 in.)
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
52-30-00-860-001 Open the FWD or AFT Cargo-Compartment Door with the Yellow Electric Pump 52-32-32-991-001 Fig. 401
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM DOORS 艙門6(19)
