R D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
52-30-00-860-001 52-30-00-860-002 52-32-00-720-001 52-32-11-820-002 Open the FWD or AFT Cargo-Compartment Door with the Yellow Electric PumpClose the FWD or AFT Cargo-Compartment Door with the Yellow Electric PumpFunctional Test of the AFT Cargo-Compartment DoorAdjustment of the Door Mechanism
R **ON A/C 106-149, 221-299, 301-399,
52-32-21-991-019-B Fig. 403A
R **ON A/C 401-499,
R 52-32-21-991-019-C Fig. 403C
R **ON A/C 106-149, 221-299, 301-399,
52-32-21-991-021 Fig. 416
R **ON A/C 401-499,
R 52-32-21-991-021-A Fig. 416A
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R **ON A/C 106-149, 221-299, 301-399, 401-499,
3. Job Set-up__________
R **ON A/C 106-149, 221-299, 301-399,
Subtask 52-32-21-860-065
A. Aircraft Maintenance Configuration (Ref. Fig. 403A/TASK 52-32-21-991-019-B)
(1) Make sure that the AFT cargo-compartment door (referred to as cargo door) is open and safetied with the actuator safety locks (Ref. TASK 52-30-00-860-001).
(2) Make sure that the ACCESS PLATFORM 2M (6 FT) is in position below the opened cargo door.
(3) Make sure that the access panel 826AR is removed from the cargo door.
R **ON A/C 401-499,
R Subtask 52-32-21-860-065-A
R R A. Aircraft Maintenance Configuration (Ref. Fig. 403C/TASK 52-32-21-991-019-C)
R R R (1) Make sure that the AFT cargo-compartment door (referred to as cargo door) is open and safetied with the actuator safety locks (Ref. TASK 52-30-00-860-001).
R R (2) Make sure that the ACCESS PLATFORM 2M (6 FT) is in position below the opened cargo door.
R R (3) Make sure that the access panels 826AR, 826BR and 826CR are removed from the cargo door.
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R **ON A/C 106-149, 221-299, 301-399, 401-499,
Subtask 52-32-21-865-087
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 52-32-21-910-062
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 the COMMON GREASE (Material No. 04-004) to all the movable parts.
Subtask 52-32-21-420-074
B. Installation of the Sequence Shaft Assembly
R **ON A/C 106-149, 221-299, 301-399,
(Ref. Fig. 416/TASK 52-32-21-991-021)
R **ON A/C 401-499,
R (Ref. Fig. 416A/TASK 52-32-21-991-021-A)
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R **ON A/C 106-149, 221-299, 301-399, 401-499,
(1)
Install the sequence shaft (400) in the cargo door structure as follows:
(a)
Move the sequence shaft (400) slowly through the cargo door structure.
(b)
During this movement, assemble the lock cam (399) on the locking shaft (400).
(c)
Refer to the marks you made during the removal procedure and assemble the lock cam (399) in its correct position on the locking shaft (400).
(d)
Make sure that the attachment holes align.
