(2)
Open the door 822.
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4. Procedure
_________ Subtask 52-41-13-020-050
A. Removal of Avionics-Compartment Lateral-Right Door
(Ref. Fig. 401/TASK 52-41-13-991-001)
(1)
Disconnect the bonding leads (9).
(2)
Remove and discard the cotter pins (2).
(3)
Remove the nuts (3), then the washer (8).
(4)
Hold the lateral-right avionics-compartment door (1).
(5)
Remove the pins (6) then the bushes (7), (5) and (4).
(6)
Remove the lateral-right avionics-compartment door (1).
(7)
Remove the bushes (7), (4) and (5).
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Avionics-Compartment Lateral-Right Door
Figure 401/TASK 52-41-13-991-001
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1 1 Feb 01/98
1 1
1CES 1
TASK 52-41-13-400-001
Installation of the Avionics-Compartment Lateral-Right Door
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific dynamometer 20 daN (44.9617 lbf)
No specific Torque Wrench : range 0.35 to 0.45 daN
(0.78 to 1.01 lbf) No specific Torque Wrench : range 8 to 15 daN
(17.98 to 33.72 lbf)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-012 USA VV-P-236 PURE MINERALVASELINE OR PETRO- LATUM (Ref. 20-31-00)
Material No. 11-004 USA MIL-T-81533 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM) (Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
cotter pins 52-41-01 03 -030
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-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
52-71-00-710-001 Operational Test of the Door Warning System 52-41-13-991-001 Fig. 401 52-41-13-991-003 Fig. 402
3. Job Set-up
__________ Subtask 52-41-13-860-050
A. Aircraft Maintenance Configuration
(1) Make sure that the access platform is in position. Subtask 52-41-13-865-051
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
121VU EIS/SDAC1 AND 2/DOOR/DET/AVNCS 46WV P02
Subtask 52-41-13-916-050
C. Preparation for Installation
(1)
Clean the aircraft structure in contact with the door seal with CLEANING AGENTS (Material No. 11-004).
(2)
Apply COMMON GREASE (Material No. 04-012) on the surface of the seal in contact with the aircraft structure
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4. Procedure
_________ Subtask 52-41-13-420-050
A. Installation of the Avionics-Compartment Lateral-Right Door
(Ref. Fig. 401/TASK 52-41-13-991-001)
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