2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s) No specific access platform 1.50 m (4 ft. 11 in.)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
52-41-11-991-001 Fig. 401
3. Job Set-up
__________ Subtask 52-41-11-865-050
A. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
121VU EIS/SDAC1 AND 2/DOOR/DET/AVNCS 46WV P02
Subtask 52-41-11-010-050
B. Get Access
(1)
Put an access platform in position at zone 120.
(2)
Open the door 811.
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4. Procedure
_________ Subtask 52-41-11-020-050
A. Removal of Avionics-Compartment Forward Door
(Ref. Fig. 401/TASK 52-41-11-991-001)
(1)
Disconnect the bonding leads (2).
(2)
Remove and discard the cotter pins (3).
(3)
Remove the nuts (4) and the washer (9).
(4)
Hold the avionics-compartment forward door (1).
(5)
Remove the pins (7).
(6)
Remove the avionics-compartment forward door (1).
(7)
Remove the bushes (8), (5) and (6).
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Avionics-Compartment Forward Door
Figure 401/TASK 52-41-11-991-001
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1 1 Feb 01/98
1 1
1CES 1
TASK 52-41-11-400-001
Installation of the Avionics-Compartment Forward 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 -------------------------------------------------------------------------------
3 cotter pin 52-41-01 01 -030 R 3 cotter pin 52-41-01 01B-030
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-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
52-71-00-710-001 Operational Test of the Door Warning System
52-41-11-991-001 Fig. 401
52-41-11-991-003 Fig. 402
3. Job Set-up
__________
Subtask 52-41-11-860-050
A. Aircraft Maintenance Configuration
(1) Make sure that the access platform is in position.
Subtask 52-41-11-865-051
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 52-41-11-916-051
C. Preparation for Installation
R (1) Clean the aircraft structure that touches the door seal with CLEANING AGENTS (Material No. 11-004).
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