R (2) Remove the bonding jumpers (8) from the upper fuselage at FR27A and
R FR25 as follows:
R (a) Remove the screws (6), the washers (7) from the upper door frame.
R (b) Remove the bonding jumpers (8) from the upper door frame.
R (3) Disconnect the door actuators from the cargo door as follows:
R (a) Remove the nut (9), the washer (11), the bolt (12) and the
R bonding jumper (10) from the actuator attachment fitting (13).
R (b) Remove the cotter pin (17), the nut (16) and the washer (15) from
R the bolt (14).
R (c) Hold the piston eye end (18) so that it cannot fall when you
R remove the bolt (14).
R (d) Remove the bolt (14) with the washer (15) and disconnect the
R piston eye end (18) from the actuator attachment fitting (13).
R (e) If necessary, remove the bushes (22) and (23) from the actuator
R attachment fitting (13).
R (4) Remove the screws (31) and the end fittings (30) with the shims (29)
R from the piano hinge area.
R (5) Apply masking material to the adjacent fuselage area to prevent
R damage during the removal of the hinge pins (24).
R (6) Make sure that the sling (5) is tight and that there is no load on
R the hinge pins (24).
R (7) Remove the SUPPORT STRUT - CARGO DOORS (98D52307524000) from the
R cargo door.
R (8) Remove the hinge pins (24) and the washers (25 thru 28) from the
R piano hinge area with EXTRACTOR - HINGE PINS, CARGO DOOR
R (98D52307523000).
R (9) Carefully remove the cargo door from the fuselage and put it in an
R applicable fixture.
R 1EFF : 051-052, 1 52-31-11Page 409 1 1 May 01/05 1 1 1CES 1R **ON A/C ALL
5. Close-up
________
Subtask 52-31-11-942-066
A. Preparation of the Cargo Door for the Stowage
(1)
Remove the sling (5) from the cargo door.
(2)
Remove the hoisting lugs (2) from the cargo door and install the plastic caps (6) again.
1EFF : ALL 1 52-31-11Page 410 1 1 May 01/05 1 1 1CES 1 TASK 52-31-11-400-002
Installation of the FWD Cargo-Compartment 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 crane with a minimum capacity 130.0 kg (286.6 lb)
No specific access platform 3.5 m (11 ft. 6 in.)
No specific Torque Wrench : range 0.20 to 3.60 m.daN
(2.00 to 26.00 lbf.ft) 98A52307529001 1 SLING - CARGO DOORS 98D52307523001 1 EXTRACTOR - HINGE PINS, CARGO DOOR 98D52307524000 1 SUPPORT STRUT - CARGO DOORS
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-011 USA MIL-G-4343
SILICONE GREASE PNEUMATIC SYST AND SEALS
(Ref. 20-31-00)
Material No. 05-027 USA MIL-L-81309
RUST INHIBITOR(FOR CORROSION USE 15-004)
(Ref. 20-31-00)
Material No. 09-005 USA MIL-S-81733 CLASS C
CORROSION INHIBITIVE INTERFAY SEALANT (Ref. 20-31-00) R Material No. 09-013 USA MIL-PRF-81733 TYPE I CLASS A R CORROSION INHIBITING BRUSH CONSISTENCY R (Ref. 20-31-00)
Material No. 09-016 USA MIL-PRF-81733D TYPE II CLASS B
CORROSION INHIBITING FILLET CONSISTENCY
(Ref. 20-31-00)
1EFF : ALL 1 52-31-11Page 411 1 1 May 01/05 1 1 1CES 1
C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
cotter pin 52-36-02 03 -080
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
20-28-00-912-004 Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage and in the Wings (this does not include the tanks)-
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