(5)
If necessary, replace the bushes (4) on the forward and aft hinge frames.
R 1EFF : 106-149, 221-221, 224-224, 228-228, 1 52-33-11Page 405 1 1 May 01/05 1 1 1CES 1R **ON A/C 001-049, 051-099, 101-149, 221-221, 224-224, 228-228,
TASK 52-33-11-400-001
Installation of the Bulk Cargo-Compartment Door
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 2.10 m (6 ft. 11 in.)
No specific access platform 2.30 m (7 ft. 7 in.)
R No specific Torque Wrench : range 0.00 to 1.20 m.daN
R (0.00 to 9.00 lbf.ft) No specific Torque Wrench : range 1.00 to 10.00 m.daN
(8.00 to 75.00 lbf.ft)
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
Material No. 04-011 USA MIL-G-4343
SILICONE GREASE PNEUMATIC SYST AND SEALS
(Ref. 20-31-00)
Material No. 05-027 USA MIL-L-81309
RUST INHIBITOR(FOR CORROSION USE 15-004)
(Ref. 20-31-00)
Material No. 09-016 USA MIL-PRF-81733D TYPE II CLASS B
CORROSION INHIBITING FILLET CONSISTENCY
(Ref. 20-31-00)
R 1EFF : 001-049, 051-099, 101-149, 221-221, 1 52-33-11Page 406 1224-224, 228-228, 1May 01/05 1 1 1CES 1
C. Expendable Parts -------------------------------------------------------------------------------
FIG.ITEM --------- |DESIGNATION ---------------------------------------- |IPC-CSN------------------------------
1 cotter pins 52-33-04 01 -130
1 cotter pins 52-33-04 01A-130
18 cotter pin 52-33-04 01 -070
18 cotter pin 52-33-04 01A-070
D. Referenced Information
------------------REFERENCE -------------------------------DESIGNATION ------------------------------
-------------------------------------------------------------------------------
20-28-00-912-001 Electrical Bonding of Components with Rivets 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 52-30-00-860-008 Close the Bulk Cargo-Compartment Door 52-30-00-860-011 Close the Deactivated Bulk Cargo-Compartment Door 52-33-11-820-001 Adjustment of the Bulk Cargo-Compartment Door 52-33-11-820-002 Adjustment of the Locking Mechanism of the Bulk
Cargo-Compartment Door 52-33-11-820-003 Adjustment of the Balance Mechanism 52-33-11-991-001 Fig. 401
3. Job Set-up
__________
(Ref. Fig. 401/TASK 52-33-11-991-001)
Subtask 52-33-11-860-055
A. Aircraft Maintenance Configuration
(1)
Make sure that the AFT cargo-compartment door is opened (Ref. TASK 52-30-00-860-001).
(2)
Make sure that the access platform 2.10 m (6.88 ft.) is in position below the AFT cargo-compartment door.
(3)
Make sure that the access platform 2.30 m (7.54 ft.) is in position below the Bulk door.
R 1EFF : 001-049, 051-099, 101-149, 221-221, 1 52-33-11Page 407 1224-224, 228-228, 1May 01/05 1 1 1CES 1
(4)
Make sure that the divider net between the AFT/Bulk cargo compartment at FR59 is removed.
(5)
Make sure that the door net from the opening of the Bulk cargo compartment is removed.
(6)
Make sure that the insulation packs from the fuselage around the forward and aft hinge frames is removed.
4. Procedure
_________
(Ref. Fig. 401/TASK 52-33-11-991-001) Subtask 52-33-11-910-056
A. Preparation for Installation
(1)
Make sure that the bushes (4) are in the correct condition.
(2)
Make sure that the forward and aft hinge frames are clean and in the correct condition.
(3)
Make sure that the sleeve (17) and the bush (16) are in the correct condition.
(4)
Apply COMMON GREASE (Material No. 04-011) to the contact surfaces of the bushes (4),(16) and the sleeve (17).
(5)
Apply COMMON GREASE (Material No. 04-011) to the bolts (5), the single shims of the shim set (12) and the spacers (11),(14).
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6(30)
