C. Expendable Parts
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FIG.ITEM |DESIGNATION |IPC-CSN
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R 6 cotter pin 52-31-21 22A-040 6 cotter pin 52-31-21 42 -020
R 11 tab washers 52-31-21 22A-200 14 cotter pin 52-31-21 42 -150 14 cotter pin 52-31-21 42B-150 16 tab washers 52-31-21 42B-210
R 17 cotter pin 52-31-21 22A-080 19 cotter pin 52-31-21 42 -100 19 cotter pin 52-31-21 42B-100
R 20 cotter pin 52-31-21 22A-010 91 cotter pin 52-31-21 42 -150 91 cotter pin 52-31-21 42B-150 96 cotter pin 52-31-21 42 -100 96 cotter pin 52-31-21 42B-100 367 cotter pin 52-31-21 42 -020 371 tab washers 52-31-21 42 -200
D. Referenced Information
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REFERENCE DESIGNATION
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52-30-00-860-002 Close the FWD or AFT Cargo-Compartment Door with the Yellow Electric Pump 52-71-00-820-003 Adjustment of the Proximity Switches 30WV and 32WV of the Cargo Compartment Door Threshold
R **ON A/C 001-049, 053-099, 101-105, 151-199, 201-220,
R 52-31-21-991-009 Fig. 411
R **ON A/C 051-052,
R 52-31-21-991-009-B Fig. 411A
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REFERENCE DESIGNATION
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R **ON A/C 106-149, 221-299, 301-399, 401-499,
52-31-21-991-009-A Fig. 411B
**ON A/C ALL
3. Job Set-up
__________ R **ON A/C 001-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
Subtask 52-31-21-860-063
A. Aircraft Maintenance Configuration
(1)
Make sure that the access platform(s) in position below the closed cargo door.
(2)
Make sure that the door handle is moved away from the recess of the door structure up to the 65 degree position.
(3) Make sure that the access panel 825AR is removed from the cargo door. **ON A/C 051-052,
Subtask 52-31-21-860-063-A
A. Aircraft Maintenance Configuration
(1)
Make sure that the access platform(s) in position below the closed cargo door.
(2)
Make sure that the locking handle is moved away from the recess of the handle flap but not in the UNLOCKED position.
(3)
Make sure that the access panel 825AR is removed from the cargo door.
1EFF : ALL 1 52-31-21Page A453 1 1 Aug 01/05 1 1 1CES 1 **ON A/C ALL
4. Procedure
_________
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-220,
Subtask 52-31-21-910-060
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 COMMON GREASE (Material No. 04-004) to the bolt (23), the threaded pin of the shaft (18) and the contact area of the support fitting (9).
R **ON A/C 106-149, 221-299, 301-399, 401-499,
Subtask 52-31-21-910-060-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.
(4)
Apply the COMMON GREASE (Material No. 04-004) to the bolts (10) and (23), and the mating surfaces of the support fitting (9) and the target lever (3).
1EFF : ALL 1 52-31-21Page A454 1 1 Aug 01/05 1 1 1CES 1 1EFF : 001-049, 053-099, 101-105, 151-199, 1 52-31-21Page A455 1201-220, 1May 01/05 1 1 1CES 1 1EFF : 001-049, 053-099, 101-105, 151-199, 1 52-31-21Page A456 1201-220, 1May 01/05 1 1 1CES 1 1EFF : 001-049, 051-099, 101-105, 151-199, 1 52-31-21Page A457 1201-220, 1May 01/05 1 1 1CES 1 1EFF : 051-052, 1 52-31-21Page A458 1 1 May 01/05 1 1 1CES 1
