R (e) Remove the push-fit covers (55).
R (f) Remove and discard the lockwire from the bolts (54).
R (g) Support the movable fairing, and remove the bolts (54) and the
R splined fittings (53).
R (h) Remove the movable fairing.
R (5) Remove the adjusters (52).
TASK 57-55-11-400-004
Installation of the Flap Track Fairings Nos. 2, 3 and 4
WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______
NOTICES ARE IN POSITION.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific plastic spatula
No specific warning notices R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft)
No specific Torque Wrench : range 0.20 to 3.60 m.daN
(2.00 to 26.00 lbf.ft) No specific Torque Wrench : range 1.00 to 10.00 m.daN
(8.00 to 75.00 lbf.ft)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 05-002 USA MIL-P-8116 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00) Material No. 05-064 GB ABP1-4053 RELEASE AGENT (Ref. 20-31-00)
Material No. 09-016 USA MIL-PRF-81733D TYPE II CLASS B
CORROSION INHIBITING FILLET CONSISTENCY
(Ref. 20-31-00)
Material No. 09-018 USA AMS 3267/3
CORROSION INHIBITING LOW ADHESION SEALANT
(Ref. 20-31-00)
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R Material No. 09-019 USA AMS 3267/3
R LOW ADHESION CORROSION INHIBITING SEALANT
R (Ref. 20-31-00)
R Material No. 11-004 USA MIL-T-81533
R 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM)
R (Ref. 20-31-00)
R Material No. 19-003 USA AMS 3819
R LINT-FREE COTTON CLOTH (Ref. 20-31-00)
R Material No. 19-010 USA AMS 5687
R LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
R (Ref. 20-31-00)
R C. Expendable Parts
R -------------------------------------------------------------------------------R FIG.ITEM |DESIGNATION |IPC-CSN R -------------------------------------------------------------------------------
R 19 packer(s) 57-55-05 20D-065
R D. Referenced Information
R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R 20-28-00-912-004 R R R 27-50-00-866-009 R 27-54-00-710-001 R 57-55-11-000-004 R 57-55-11-991-010 R 57-55-11-991-011 R 57-55-11-991-013 R 57-55-11-991-012 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)-Retraction of the Flaps on the Ground Operational Test of the Flap System Removal of the Flap Track Fairings Nos. 2, 3 and 4 Fig. 409 Fig. 410 Fig. 411 Fig. 412
R 3. Job Set-up__________
R Subtask 57-55-11-941-065
R A. Safety Precautions
R (1) Make sure that the warning notices are in position in the cockpit to
R tell persons not to operate the flaps or slats
R (2) Make sure that the safety barriers are in position.
R Subtask 57-55-11-860-055
R B. Aircraft Maintenance Configuration
R (1) Make sure that the flaps are in the fully retracted position
R (Ref. TASK 27-50-00-866-009).
R (2) Make sure that the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER is
R installed on the flap/slat control-lever.
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