(2)
 Open the door 824.

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 4. Procedure
_________ Subtask 52-41-14-020-050
 A. Removal of the Avionics Compartment Aft Door (Ref. Fig. 401/TASK 52-41-14-991-001)
 (1)
 Remove and discard the cotter pin (2).

 (2)
 Remove the nut (3) and the washer (4).

 (3)
 Remove the actuator (5) and the washer (6).

 (4)
 Disconnect the bonding leads (7).

 (5)
 Remove and discard the cotter pins (9).

 (6)
 Remove the nuts (8) and the washer (14).

 (7)
 Hold the access door (1).

 (8)
 Remove the pins (12).

 (9)
 Remove the door (1).

 (10) Remove the bushes (11), (13), and (10).
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 Avionics-Compartment Aft Door
 Figure 401/TASK 52-41-14-991-001
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1  1  Feb 01/98
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 1CES  1

 TASK 52-41-14-400-001
 Installation of the Avionics-Compartment Aft 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) R No specific Torque Wrench : range 0.62 to 0.75 daN R (1.39 to 1.68 lbf)
 B. Consumable Materials
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
Material No. 04-004  USA MIL-PRF-23827 TYPE I
 SYNTH.ESTER BASED GREASE HIGH PRESSURE
 (Ref. 20-31-00)

 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
 -------------------------------------------------------------------------------
2 cotter pin 52-41-01 04 -030 9 cotter pins 52-41-01 04 -120
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 D. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R  52-41-00-410-002 52-71-00-710-001 52-41-14-991-001 52-41-14-991-003 52-41-14-991-005  Close the Avionics Compartment Doors after AccessOperational Test of the Door Warning SystemFig. 401Fig. 402 Fig. 403
 3. Job Set-up__________
 Subtask 52-41-14-860-050
 A. Aircraft Maintenance Configuration
 (1) Make sure that the access platform is in position.
 Subtask 52-41-14-865-051
 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 52-41-14-916-050
 C. Preparation for Installation 
R R  (1) Clean the aircraft structure which touches the door seal, with CLEANING AGENTS (Material No. 11-004). 
R R  (2) Apply COMMON GREASE (Material No. 04-012) on the surface of the seal which touches the aircraft structure.

 4. Procedure_________
 Subtask 52-41-14-420-050
 A. Installation of the Avionics-Compartment Aft Door (Ref. Fig. 401/TASK 52-41-14-991-001)
 (1) Install the bushes (11), (10) and (13).
 (2) Put the door (1) in position opposite the hinges.
 (3) Install the pins (12).
 (4) Install the washer (14) and the nuts (8) and tighten the nuts.
　
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