R **ON A/C 401-499,
R 52-32-21-991-019-C Fig. 403C **ON A/C 001-049, 053-099, 101-105, 201-220,
52-32-21-991-017 Fig. 417 **ON A/C 106-149, 221-299, 301-399,
52-32-21-991-017-B **ON A/C 151-199, Fig. 417A
R 52-32-21-991-017-A **ON A/C 401-499, Fig. 417B
R R 52-32-21-991-017-C Fig. 417C **ON A/C 001-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
3. Job Set-up__________ **ON A/C 001-049, 053-099, 101-149, 201-299, 301-399,
Subtask 52-32-21-010-063 A. Get Access **ON A/C 001-049, 053-099, 101-105, 201-220,
(Ref. Fig. 403/TASK 52-32-21-991-019)
R 1EFF : 001-049, 053-099, 101-149, 151-199, 1 52-32-21Page B482 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1
**ON A/C 106-149, 221-299, 301-399,
(Ref. Fig. 403A/TASK 52-32-21-991-019-B) **ON A/C 001-049, 053-099, 101-149, 201-299, 301-399,
R (1) Open the AFT cargo-compartment door (referred to as cargo door) and safety it with the actuator safety locks (Ref. TASK 52-30-00-860-001). (2) Put the access platform in position at the cargo door. (3) Remove the access panel 826AR from the cargo door. (4) Remove the protection plug (6) from the lateral cutout of the edge member as required. **ON A/C 151-199, 401-499,
Subtask 52-32-21-010-063-A
A. Get Access
R **ON A/C 151-199,
R (Ref. Fig. 403B/TASK 52-32-21-991-019-A) **ON A/C 401-499,
R R (Ref. Fig. 403C/TASK 52-32-21-991-019-C) **ON A/C 151-199, 401-499,
(1) Open the AFT cargo-compartment door (referred to as cargo door) and safety it with the actuator safety locks (Ref. TASK 52-30-00-860-001). (2) Put the access platform in position at the cargo door. (3) Remove the access panels 826AR, 826BR and 826CR from the cargo door.
R 1EFF : 001-049, 053-099, 101-149, 151-199, 1 52-32-21Page B483 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1
(4) Remove the protection plugs (9) or (12) from the lateral cutout of the edge member as required.
R **ON A/C 001-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
Subtask 52-32-21-865-080
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 52-32-21-020-069
A. Removal of the Latching Shaft
**ON A/C 001-049, 053-099, 101-105, 201-220,
(Ref. Fig. 417/TASK 52-32-21-991-017)
**ON A/C 106-149, 221-299, 301-399,
(Ref. Fig. 417A/TASK 52-32-21-991-017-B)
**ON A/C 151-199,
(Ref. Fig. 417B/TASK 52-32-21-991-017-A) R **ON A/C 401-499,
R (Ref. Fig. 417C/TASK 52-32-21-991-017-C)
R 1EFF : 001-049, 053-099, 101-149, 151-199, 1 52-32-21Page B484 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1R **ON A/C 001-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
NOTE : Identify the installation position of the link lever, shaft
____ levers, the control lever and the interlock cam with a mark.
(1)
Disconnect the shaft lever (175) from the link rod (181) of each latching unit as follows:
(a)
Turn the latching shaft (171) so that you can remove the bolts
(178) thru the mounting holes of the door frame.
(b)
Remove and discard the cotter pin (172) from the nut (173).
(c)
Remove the nut (173), the washers (179), the bushes (180) and
(182) and the bolt (178) from the shaft levers (175).
(d)
Remove the eye-end of the link rod (181) from the fork- end of the shaft lever (175).
(2)
Disconnect the link lever (40) from the connection rod (44) follows:
(a)
Turn the latching shaft (171) so that you can remove the bolts
(45) thru the mounting holes of the door frame.
(b)
Remove and discard the cotter pin (41) from the nut (42).
(c)
Remove the nut (42), the washers (43) and the bolt (45) from the link rod (44).
(d)
Remove the fork-end of the link rod (44) from the link lever (40).
(3)
Remove the locking shaft (171) from the cargo door as follows:
(a)
Remove the nuts (177), the sleeves (176) and the tapered pins
(174) from each shaft levers (175).
(b)
Remove the nuts (185), the sleeves (184) and the tapered pins
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM DOORS 艙門6
