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Fit and Clearances of the Handle Flap Mechanism
Figure 609/TASK 52-32-11-991-002
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| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS | | DETAIL |---------------------------------------|----------------------------| | AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. | | ITEM | MM (IN.) | MM (IN.) | MM (IN.) | ALLOW. | | NO. |-------------------|-------------------|---------|---------| CLEAR. | | | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |MM (IN.)| |--------|---------|---------|---------|---------|---------|---------|--------| | D-D | 6.336 | 6.345 | | | 6.323 | | | | OD 3 |(0.2494) |(0.2498) | | |(0.2489) | | | | | | | 0.005 | 0.029 | | | 0.063 | | | | | (0.0001)| (0.0011)| | |(0.0024)| | D-D | 6.350 | 6.365 | | | | 6.386 | | | ID 4 |(0.2500) |(0.2505) | | | |(0.2514) | | -------------------------------------------------------------------------------
Subtask 52-32-11-220-054
E. Measurement of the Hinge Pins and the Piano Hinges
(Ref. Fig. 610/TASK 52-32-11-991-003)
-------------------------------------------------------------------------------| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS | | DETAIL |---------------------------------------|----------------------------| | AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. | | ITEM | MM (IN.) | MM (IN.) | MM (IN.) | ALLOW. | | NO. |-------------------|-------------------|---------|---------| CLEAR. | | | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |MM (IN.)| |--------|---------|---------|---------|---------|---------|---------|--------| | B-B | 10.857 | 10.900 | | | 10.400 | | | | OD 1 |(0.4274) |(0.4291) | | |(0.4094) | | | | | | | 0.300 | 0.386 | | | 1.100 | | | | | (0.0118)| (0.0151)| | |(0.0433)| | B-B | 11.200 | 11.243 | | | | 11.500 | | | ID 2 |(0.4409) |(0.4426) | | | |(0.4527) | | -------------------------------------------------------------------------------
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Fit and Clearances of the Piano Hinges and the Hinge Pins
Figure 610/TASK 52-32-11-991-003
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5. Close-up
________ Subtask 52-32-11-860-058
A. Put the aircraft back to the serviceable condition.
(1)
Assemble the locking handle mechanism to the locking shaft (Ref. TASK 52-32-21-400-001).
(2)
Install the handle flap mechanism on the cargo door (Ref. TASK 52-32-21-400-002).
(3)
Prepare the cargo door as follows:
(a)
Install the hinge pins and the related end fittings in the piano hinge area (Ref. TASK 52-32-11-400-001).
(b)
Disconnect the crane from the cargo door (Ref. TASK 52-32-11-400-001).
(4)
Install the access panel 826AR on the cargo door.
(5)
Make sure that the AFT cargo compartment door (referred to as cargo door) is closed and locked (Ref. TASK 52-30-00-860-001).
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TASK 52-32-11-200-011
General Visual Inspection of Aft Cargo Compartment Door Skin, External Surface
1. Reason for the Job
__________________
Refer to the MPD TASK: 523111-01
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific 1 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION
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ASRM 52320010100
ASRM 51730000100 (for corrective action)
ASRM 52320020100 (for corrective action)
CMM 523112 (for corrective action)
CMM 523115 (for corrective action)
51-73-11-300-001 Repair of Minor Damage on Aluminum Clad Components
(for corrective action) 51-73-11-300-003 Repair of Dents in Skin Panels (for corrective action) 51-75-12-300-001 Repair of Major Paint Damage on Light Alloy and Composite Material (for corrective action) 51-75-12-300-003 Repair of Minor Paint Damage (Topcoat Only) (for corrective action) 中國航空網 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5(58)
