(Ref. Fig. 403A/TASK 52-32-21-991-019-B)
 **ON A/C 001-049, 053-099, 101-149, 201-299, 301-399,

 (1)
 Make sure that the AFT cargo-compartment door (referred to as cargo door) is opened and safetied with the actuator safety locks (Ref. TASK 52-30-00-860-001).

 (2)
 Make sure that the access panel 826AR is removed from the cargo door.

 (3)
 Put the access platform in position below the opened cargo door.

R 1EFF : 001-049, 053-099, 101-149, 151-199, 1 52-32-21Page B424 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1

 (4) Make sure that the access panel (1) is removed from the inner skin of

 the cargo door.
 (5) Make sure that the protection plug (5) is removed from the edge member at FR56. 
R  **ON A/C 151-199, 401-499,
 Subtask 52-32-21-860-061-A
 A. Aircraft Maintenance Configuration 
R  **ON A/C 151-199,
 (Ref. Fig. 403B/TASK 52-32-21-991-019-A) 
R  **ON A/C 401-499, 
R  (Ref. Fig. 403C/TASK 52-32-21-991-019-C) 
R  **ON A/C 151-199, 401-499,
 (1) Make sure that the AFT cargo-compartment door (referred to as cargo door) is opened and safetied with the actuator safety locks (Ref. TASK 52-30-00-860-001).
 (2) Make sure that the access panel 826AR is removed from the cargo door.
 (3) Put the access platform in position below the opened cargo door.
 (4) Make sure that the access panel (1) is removed from the inner skin of the cargo door.
 (5) Make sure that the protective plug (13) is removed from the edge member at FR59. 

R 1EFF : 001-049, 053-099, 101-149, 151-199, 1 52-32-21Page B425 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1

R  **ON A/C 001-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 Subtask 52-32-21-865-075
 B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------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_________
 **ON A/C 001-049, 053-099, 101-105, 201-220,
 (Ref. Fig. 413/TASK 52-32-21-991-014) **ON A/C 106-149, 221-299, 301-399,
 (Ref. Fig. 413A/TASK 52-32-21-991-014-B) **ON A/C 151-199,
R  (Ref. Fig. 413B/TASK 52-32-21-991-014-A) **ON A/C 401-499, 
R R  (Ref. Fig. 413C/TASK 52-32-21-991-014-C) **ON A/C 001-049, 053-099, 101-105, 201-220,
 (Ref. Fig. 414/TASK 52-32-21-991-015) **ON A/C 106-149, 221-299, 301-399,
 (Ref. Fig. 414A/TASK 52-32-21-991-015-B) 

R 1EFF : 001-049, 053-099, 101-149, 151-199, 1 52-32-21Page B426 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1

 **ON A/C 151-199,
 (Ref. Fig. 414B/TASK 52-32-21-991-015-A) R **ON A/C 401-499,
R (Ref. Fig. 414C/TASK 52-32-21-991-015-C) **ON A/C 001-049, 053-099, 101-105, 151-199, 201-220,
 Subtask 52-32-21-910-058
 A. Preparation for Installation
 (1)
 Make sure that the parts retained from the removed component are clean and in the correct condition.

 (2)
 Clean the component interface and/or the adjacent area.

 (3)
 Do an inspection of the component interface and/or the adjacent area.

 (4)
 Apply a layer of COMMON GREASE (Material No. 04-004) to

 -
the mating surface of the serrated shaft (31) and its splined ends

 -
the shaft of the spring bolt (19)

 -
the shaft of the bolts (39), (44), (49), (56) and (58)

 -
the pins (24).

 (5)
 Apply a layer of COMMON GREASE (Material No. 04-017) to mating surface of the Maltese-cross latch (32), the the roller lever (33) and Maltese-cross lock (34)

 (6)
 Apply a layer of SEALANTS (Material No. 09-018) to the mating surface of the mounting bracket (68).

R 1EFF : 001-049, 053-099, 101-105, 151-199, 1 52-32-21Page B427 1201-220, 401-499, 1Aug 01/05 1 1 1CES 1R **ON A/C 106-149, 221-299, 301-399, 401-499,

 Subtask 52-32-21-910-058-A
 A. Preparation for Installation
 (1)
 Make sure that the parts retained from the removed component are clean and in the correct condition.

 (2)
 Clean the component interface and/or the adjacent area.

 (3)
 Do an inspection of the component interface and/or the adjacent area.
　
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(131)