(1)
Install the bushes (5), (4) and (7).
(2)
Put the door (1) in position opposite the hinges.
(3)
Install the pins (6).
(4)
Install the washer (8) and the nuts (3) and tighten the nuts.
(5)
Install the new cotter pins (2).
(6) Connect the bonding leads (9). Subtask 52-41-13-220-051
B. Check and Adjustment of the Out-of-flush Clearance Between the Door (11) and the Fuselage (Ref. Fig. 402/TASK 52-41-13-991-003)
(1)
Keep the door against the stop and measure the out-of-flush clearance J1 between the door (11) and the fuselage. The clearance J1 must be 0 -0.8 +0.8 mm (0.0000 -0.0314 +0.0314 in.).
(2)
If the out-of-flush clearance J1 is not in the tolerances:
(a)
Open the door (11).
(b)
Remove the two self-locking nuts (12), the two screws (13) and the washers (14)
(c)
Put a new set of washers (14) and install the two screws (13) and the two self-locking nuts (12).
(d)
Close the door and make sure that the clearance J2 is 0.2 mm (0.0078 in.) minimum.
(e)
TORQUE the self-locking nuts (12) to between 0.35 and 0.45 daN
(0.78 and 1.01 lbf).
(f)
Close the door (11).
1EFF : ALL 1 52-41-13Page 406 1 1 Feb 01/98 1 1 1CES 1 Subtask 52-41-13-220-052
C. Check of the Load on the Locking Handle
(1)
Close the door
(2)
Measure the load on the door handle with a dynamometer and make sure that the load is to between 8 and 15 daN (17.98 and 33.72 lbf).
Subtask 52-41-13-710-050
D. Test
(1) Do an operational test of the door warning system (Ref. TASK 52-71-00-710-001).
5. Close-up
________ Subtask 52-41-13-865-052
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 46WV
Subtask 52-41-13-410-050
B. Close Access
(1)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(2)
Close the door 822.
(3)
Remove the access platform(s).
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Avionics-Compartment Lateral-Right Door - Check of Clearance Figure 402/TASK 52-41-13-991-003- 12 (SHEET 1)
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Avionics-Compartment Lateral-Right Door - Check of Clearance Figure 402/TASK 52-41-13-991-003- 22 (SHEET 2)
1EFF : ALL 1 52-41-13Page 409 1 1 Feb 01/98 1 1 1CES 1 DOOR - AVIONICS COMPARTMENT, LATERAL RIGHT - INSPECTION/CHECK
_____________________________________________________________
TASK 52-41-13-200-001
Detailed Inspection of Lateral Right Avionics Compartment Access Door, Internal Structure
1. Reason for the Job
__________________
Refer to the MPD TASK: 524131-01
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 1.80 m (5 ft. 11 in.)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific masking paper Material No. 08-074 MASKING TAPE (Ref. 20-31-00)
Material No. 11-004 USA MIL-T-81533 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM) (Ref. 20-31-00)
Material No. 15-005 AIB TN 10138 TYPE I GRADE 2 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
Material No. 15-006 AIB TN 10138 TYPE I GRADE 3 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
Material No. 19-003 USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
1EFF : ALL 1 52-41-13Page 601 1 1 Feb 01/04R 1 1 1CES 1
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
52-41-00-010-002 52-41-00-410-002 SRM 511100 P.Block 001 SRM 512200 P.Block 001 52-41-13-991-002
3. Job Set-up
__________Open the Avionics Compartment Doors for AccessClose the Avionics Compartment Doors after Access(for corrective action)(for corrective action)Fig. 601
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