(2)
 Install the access panel 825AR.

 (3)
 Remove the actuator safety locks and close the cargo door (Ref. TASK 52-30-00-860-002).

 (4)
 Remove the access platform(s).

R 1EFF : 151-199, 401-499, 1 52-32-11Page 652 1 1 Aug 01/05 1 1 1CES 1 TASK 52-32-11-200-010

 Detailed Visual Inspection of AFT Cargo Compartment Door (Internal Hinge Fitting Attachment Area)
 1. Reason for the Job
__________________
 Refer to the MPD TASK: 523217-01
 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 3.5 m (11 ft. 6 in.)
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
51-75-12-300-001 Repair of Major Paint Damage on Light Alloy and Composite Material 52-30-00-860-001 Open the FWD or AFT Cargo-Compartment Door with the Yellow Electric Pump 52-30-00-860-002 Close the FWD or AFT Cargo-Compartment Door with the
 Yellow Electric Pump 52-32-13-000-001 Removal of the Lining and Insulation 52-32-13-400-001 Installation of the Lining and Insulation SRM 51-73-00 SRM 51-74-00 SRM 52-30-00 52-32-11-991-026 Fig. 607
R 1EFF : 151-199, 401-499, 1 52-32-11Page 653 1 1 Aug 01/05 1 1 1CES 1

 3. Job Set-up
__________ Subtask 52-32-11-010-068
 A. Aircraft Maintenance Configuration
 (1)
 Open the AFT cargo door and safety it with the actuator safety locks (Ref. TASK 52-30-00-860-001).

 (2)
 Put the access platform in position below the opened cargo door.

 (3)
 Remove the lining and the insulation of the cargo door (Ref. TASK 52-32-13-000-001).

 Subtask 52-32-11-865-078
 B. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
121VU HYDRAULIC/HYD POWER/Y 3803GX N30 122VU DOORS/CARGO 1MJ T12 123VU Y HYD/ELEC/PUMP 3802GX AB06 123VU Y HYD/ELEC/ELEC PUMP/NORM 3801GX AB03
 4. Procedure
_________ Subtask 52-32-11-210-062
 A. Visual Inspection of the inner Attachment Area of the Piano Hinge
 Fittings
 (Ref. Fig. 607/TASK 52-32-11-991-026)

 (1) Examine the upper door structure from the inner side for corrosion and cracks.
 (a) If you find corrosion,
 -determine the extent of the corroded area (Ref. SRM 52-30-00),
 -remove the damage when it is less than the limit (Ref. SRM 51-74-00).
 NOTE : When the corroded area is larger than the limit, repair
____ the affected internal attachment area.
 (b) If you find a crack, repair it immediately (Ref. SRM 51-73-00).
R 1EFF : 151-199, 401-499, 1 52-32-11Page 654 1 1 Aug 01/05 1 1 1CES 1

 Inspection of Internal Attachment Area of the Piano Hinge Fittings
 Figure 607/TASK 52-32-11-991-026

R 1EFF : 151-199, 401-499, 1 52-32-11Page 655 1 1 Aug 01/05 1 1 1CES 1

 (2)
 Make sure that the Hi-Lok rivets are correctly tightened.

 (3)
 Make sure that the attachment screws and nuts of the piano hinge fittings are correctly tightened and not damaged.

 (4)
 Make sure that the paint coat in the internal attachment area is in the correct condition (Ref. TASK 51-75-12-300-001).

 5. Close-up
________ Subtask 52-32-11-865-077
 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1MJ, 3801GX, 3802GX, 3803GX
 Subtask 52-32-11-410-068
 B. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Install the lining and the insulation of the cargo door (Ref. TASK 52-32-13-400-001).

 (3)
 Remove the actuator safety locks and close the AFT cargo door (Ref. TASK 52-30-00-860-002).

 (4)
 Remove the access platform(s).

R 1EFF : 151-199, 401-499, 1 52-32-11Page 656 1 1 Aug 01/05 1 1 1CES 1 **ON A/C 051-052,

 TASK 52-32-11-220-001
　
中國航空網 m.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(56)