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.

 1EFF : ALL 1 52-41-11Page 401 1 1 Feb 01/98 1 1 1CES 1

 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).

 1EFF : ALL 1 52-41-11Page 402 1 1 Feb 01/98 1 1 1CES 1

 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
 1EFF : ALL 1 52-41-11Page 404 1 1 May 01/04 1 1 1CES 1 D. Referenced Information

 -------------------------------------------------------------------------------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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