(2)
Open the access door 312AR of the accessory compartment.
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4. Procedure
_________ Subtask 52-41-16-020-050
A. Removal of the Accessory Compartment Door
(Ref. Fig. 401/TASK 52-41-16-991-001)
(1)
Disconnect the bonding jumper (12) from the access door (6).
(2)
Remove the nut (9), the screw (11) and the washer (10).
(3)
Hold the access door (6) and remove the nuts (1), the screws (4) and the washers (2).
(4)
Remove the access door (6) with the hinge assemblies (5).
(5)
Remove the shims (3) if installed.
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Accessory Compartment Access Door 312AR
Figure 401/TASK 52-41-16-991-001
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1 1 Feb 01/98
1 1
1CES 1
TASK 52-41-16-400-001
Installation of the Accessory Compartment Access Door 312AR
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific access platform(s) 2.8 m (9 ft. 2 in.)
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
Material No. 05-002 USA MIL-P-8116 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00)
Material No. 05-027 USA MIL-L-81309
R RUST INHIBITOR(FOR CORROSION USE 15-004)
R (Ref. 20-31-00) Material No. 09-013 USA MIL-PRF-81733 TYPE I CLASS A CORROSION INHIBITING BRUSH CONSISTENCY (Ref. 20-31-00) Material No. 09-018 USA AMS 3267/3 CORROSION INHIBITING LOW ADHESION SEALANT (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
20-28-00-912-004 Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage and in the Wings (this does not includes the tanks)-
51-75-13-916-001 Repair to a layer of Moisture-Removing Oil
52-41-16-991-001 Fig. 401
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3. Job Set-up
__________ Subtask 52-41-16-860-050
A. Aircraft Maintenance Configuration
(1)
Make sure that the access platform(s) in position.
(2)
Make sure that the access door 312AR is opened.
4. Procedure
_________
(Ref. Fig. 401/TASK 52-41-16-991-001) Subtask 52-41-16-560-050
A. Preparation of the Replacement Components
(1)
Lock the latch assemblies (7).
(2)
Adjust the set screws (8) of the latch assemblies (7) to come up to a dimension of 6.2 mm (0.2440 in.).
(3)
Unlock the latch assemblies (7). NOTE : To get the correct door gaps A and C, you can install a
____ maximum of two shims (3) at each hinge assembly (5).
(4)
Apply SEALANTS (Material No. 09-013) to the mating surface of the shims (3) if installed.
(5) Install the shims (3) as required. Subtask 52-41-16-910-050
B. Preparation for Installation
WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL
_______ MATERIALS ONLY WITH A GOOD SUPPLY OF AIR. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED. 中國航空網(wǎng) m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機(jī)維護(hù)手冊 AMM DOORS 艙門6(153)
