(1) Remove the connection rod (76) from the intermediate shaft (71) as follwos:
(a)
Remove and discard the cotter pin (72) from the nut (73).
(b)
Remove the nut (73), the washers (74), the bush (75) and the bolt (78).
(c)
Remove the upper eye-end of the connection rod (76) from the shaft lever (145).
(d)
If required, remove the bush (77) from the shaft lever (145).
1EFF : 301-399, 1 52-22-22Page 421 1 1 May 01/04 1 1 1CES 1
Intermediate Shaft
Figure 403/TASK 52-22-22-991-003
1EFF : 301-399, 1 52-22-22 Page 422
1 1 May 01/04
1 1
1CES 1
(2)
Remove the link rod (88) from the fork lever (83) as follows:
(a)
Remove and discard the cotter pin (90) from the nut (91).
(b)
Remove the nut (91), the washers (84), the bush (89) and the bolt (85).
(c)
Remove the eye-end of the link rod (88) from the fork lever (83).
(d)
If required, remove the bush (89) from the fork lever (83).
(3)
Remove the intermediate shaft assemblly (71) from the door structure as follows:
(a)
Remove the nut (82), the washers (81) and the bolt (86) from the fork lever (83).
(b)
Disassemble the fork lever (83) from the end of the intermediate shaft (141)
(c)
Remove the circlip (80) and the washers (79) from the
intermediate shaft (141).
(d)
Remove the nuts (148), the washers (147) and the bolts (149) from the actuation lever (146).
(e)
Remove the nut (144), the washers (143) and the bolt (142) from the shaft lever (145).
(f)
Remove the nuts (96), the washers (97) and the bolts (99) from the bearing bracket (98).
(g)
Move the intermediate shaft (141) rearward and remove the bearing bracket (98) and the bearing (100) from the intermediate shaft (141).
(h)
If required, remove the shaft lever (145) and the actuation shaft
(146) from the intermediate shaft (141).
(i)
Remove the intermediate shaft (141) from the structure.
(4)
If required, remove the nuts (92), the washers (93), the bolts (95) and the stop fitting (94) from the structure.
1EFF : 301-399, 1 52-22-22Page 423 1 1 May 01/04 1 1 1CES 1
TASK 52-22-22-400-003 Installation of the Intermediate Shaft Assembly
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 3.2 m (10 ft. 6 in.)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-004 USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
72 cotter pin 52-22-22 05 -110 90 cotter pin 52-22-22 04 -100
1EFF : 301-399, 1 52-22-22Page 424 1 1 May 01/04 1 1 1CES 1
D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
25-23-47-000-012 Removal of the Door Linings of the LH FWD Emergency Exit Door, zone 231
25-23-47-000-013 Removal of the Door Linings of the RH FWD Emergency Exit Door at zone 251 or RH AFT at zone 252 or LH AFT at zone 232.
25-23-47-400-012 Installation of the Door Linings of the LH FWD Emergency Exit Door, zone 231
25-23-47-400-013 Installation of the Door Linings of the RH FWD Emergency Exit Door at zone 251, or RH AFT at zone 252, or LH AFT at zone 232.
52-22-00-010-001 Opening of the Emergency Exit Doors from the Passenger Compartment 52-22-00-410-001 Closing of the Emergency Exit Doors from the Passenger Compartment
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3(140)
