**ON A/C 151-199,
52-32-21-991-017-A Fig. 417B R **ON A/C 401-499,
R 52-32-21-991-017-C Fig. 417C
R **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 52-32-21-860-063
A. Aircraft Maintenance Configuration
**ON A/C 001-049, 053-099, 101-105, 201-220,
(Ref. Fig. 403/TASK 52-32-21-991-019)
**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,
(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 platform in position below the opened cargo door.
(3)
Make sure that the access panel 826AR is removed from the cargo door.
R 1EFF : 001-049, 053-099, 101-149, 151-199, 1 52-32-21Page B497 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1
(4) Make sure that the protective plug (6) is removed from the edge member.
R **ON A/C 151-199, 401-499,
Subtask 52-32-21-860-063-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 platform in position below the opened cargo door.
(3) Make sure that the access panels 826AR, 826BR and 826CR are removed from the cargo door.
(4) Make sure that the protection plug (9) or (12) is removed from the edge member.
R 1EFF : 001-049, 053-099, 101-149, 151-199, 1 52-32-21Page B498 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,
Subtask 52-32-21-865-081
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
_________
Subtask 52-32-21-910-060
A. Preparation for the 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 all moveable parts.
(5)
If removed, install the target on the control lever (190) (Ref. TASK 52-35-13-400-002).
**ON A/C 001-049, 053-099, 101-149, 201-299, 301-399,
Subtask 52-32-21-420-070
B. Installation of the Latching Shaft
**ON A/C 001-049, 053-099, 101-105, 201-220,
(Ref. Fig. 417/TASK 52-32-21-991-017)
1EFF : 001-049, 053-099, 101-149, 151-199, 1 52-32-21Page B499 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1 **ON A/C 106-149, 221-299, 301-399,
(Ref. Fig. 417A/TASK 52-32-21-991-017-B)
**ON A/C 001-049, 053-099, 101-149, 201-299, 301-399,
(1)
Install the latching shaft (171) on the cargo door as follows:
(a)
Move the latching shaft (171) through the lateral cutout of the cargo door into the sliding bearing of each frame fork end.
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