(4)
Move the carriage (6) to get access to the bolt (18) through the access hole in pocket 4 of the flap track beam (25).
(5)
Loosen the bolt (18).
(6)
Remove the bolt (18) through the access hole in pocket 4.
(7)
Remove the roller (14) and the washer (15) through the lower side of the flap track beam (25).
(8)
Remove the nut (11), the washer (12) and the lockplate (13) from the lower side of the carriage (6). Discard the lockplate (13).
(9)
Move the carriage as necessary and remove the bolt (1), the roller
(2) and the washer (3) from the top side of the carriage (6).
(10)
Remove the retaining ring (4) and the washer (5) from the bolt (17).
(11)
Remove the bolt (17) and the lockplate (16) from the carriage (6) through the lower side of the flap track beam (25). Discard the lockplate (16).
(12)
Remove the pendulum (7) from the carriage (6).
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Installation of the Pendulum of the No. 1 Flap Track Carriage
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.
CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:
_______
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
-MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers No specific warning notice No specific access platform 2.4 m (7 ft. 10 in.) No specific Torque Wrench : range 0.00 to 1.20 m.daN
(0.00 to 9.00 lbf.ft) No specific Torque Wrench : range 1.00 to 10.00 m.daN
(8.00 to 75.00 lbf.ft)
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-54-46Page 448 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-004 USA MIL-PRF-23827 TYPE I
SYNTH.ESTER BASED GREASE HIGH PRESSURE
Material No. 05-002 (Ref. 20-31-00)USA MIL-P-8116
Material No. 06-011 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00)GB ABR 1-4055
Material No. 09-013 SOLID FILM LUBRICANT (Ref. 20-31-00)USA MIL-PRF-81733 TYPE I CLASS A
CORROSION INHIBITING BRUSH CONSISTENCY
Material No. 09-018 (Ref. 20-31-00)USA AMS 3267/3 CORROSION INHIBITING LOW ADHESION SEALANT
Material No. 11-026 Material No. 19-003 (Ref. 20-31-00)GB DEF-STAN 68-148/1 SOLVENT GENERAL PURPOSE (Ref. 20-31-00)USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
7 lockplate 27-54-46 01 -030
7 lockplate 27-54-46 01A-030
8 lockplate 27-54-46 01 -030
8 lockplate 27-54-46 01A-030
13 lockplate 27-54-46 01 -030
13 lockplate 27-54-46 01A-030
16 lockplate 27-54-46 01 -140
16 lockplate 27-54-46 01A-140
17 lockplate 27-54-46 01 -140
17 lockplate 27-54-46 01A-140
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D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-50-00-866-009 27-54-61-400-001 32-00-00-481-002 32-12-00-010-001 27-54-46-991-004 27-54-46-991-006 Retraction of the Flaps on the GroundInstallation of the Inboard FlapInstallation of the Safety Devices on the Landing Gear DoorsOpen the Main Gear Doors for AccessFig. 403Fig. 404
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