(b)
 Remove the bolt (159).

 (c)
 Remove and discard the tabwasher (160).

 (d)
 Remove the retainer (161).

 (e)
 Remove the locknut (162).

 (f)
 Remove and discard the tabwasher (158).

 (g)
 Remove the toothplate (157).

 (h)
 Remove the eccentric bush (163). If necessary, carefully lift the flap with the hoist and the sling to release the weight from the eccentric bush (163).

 (i)
 Lift the flap with the hoist until it is clear of the flap track carriage at the track 2 position.

 (j)
 Move the outboard end of the flap aft, until it is clear of the wing.

 (k)
 Pull the flap outboard until the flap drive trunnion (165) is clear of the flap track carriage (169).

 (l)
 Remove the spacer (164).

 (6)
 Remove the flap from the wing. CAUTION : MAKE SURE THAT THE FLAP DOES NOT HIT THE AIRCRAFT

_______
 STRUCTURE.

 CAUTION : MAKE SURE THAT THE SUPPORT STRUCTURE IS CLEAN AND DOES NOT
_______
 HAVE ANY SHARP POINTS.

 (a) Move the inboard flap with the hoist and lower it onto the support structure.
 1EFF : 301-399, 1 27-54-61Page A415 1 1 Aug 01/05R 1 1 1CES 1

 Flap to Flap Carriage Connection (Track 1) Figure 425/TASK 27-54-61-991-022-A
 1EFF : 301-399, 1 27-54-61Page A416 1 1 Aug 01/05R 1 1 1CES 1

 (7) Put covers, where necessary, over the disconnected items of the flap.
 Subtask 27-54-61-080-051
 B. Removal of Equipment
 (1) If necessary, remove:
 -
the hoisting sling from the inboard flap (Ref. TASK 27-50-00-000-002)

 -
the EXTRACTOR - PIN TRACKS 2 AND 3 from the carriage bolt (132). (Ref. Fig. 423/TASK 27-54-61-991-015)

 1EFF : 301-399, 1 27-54-61Page A417 1 1 Aug 01/05R 1 1 1CES 1

 TASK 27-54-61-400-003
 Installation of the Inboard Double-Slotted Flap
 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 adhesive tape No specific pneumatic wrench No specific safety barriers No specific warning notice No specific warning notice(s) No specific access platform 3.0 m (9 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 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) No specific Torque Wrench : range 2.00 to 20.00 m.daN
 (15.00 to 150.00 lbf.ft) 98D27504083000 1 EXTRACTOR - PIN TRACKS 2 AND 3 98D27504095000 1 SPANNER - TRUNNION NUT, TRACK 1 98D27504114000 2 DISTANCE GAUGES 98D27504118000 1 SPANNER-FLAP ADJUST 98D27604000000 1 COLLAR-SAFETY, SPOILER
 1EFF : 301-399, 1 27-54-61Page A418 1 1 Aug 01/05R 1 1 1CES 1

 -------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
98D27804001000 1 ADAPTOR-DRIVE, SLAT (AND FLAP)
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-022 USA MIL-PRF-81322 GRADE 2
 SYNTHE.HYDROCARBON GREASE HIGH PRESSURE
 (Ref. 20-31-00) Material No. 08-004A USA MIL-A-46106 TYPE I
 ADHESIVE SEALANT (Ref. 20-31-00) Material No. 11-026 GB DEF-STAN 68-148/1
 SOLVENT GENERAL PURPOSE (Ref. 20-31-00) Material No. 19-003 USA AMS 3819
 LINT-FREE COTTON CLOTH (Ref. 20-31-00) Material No. 19-010 USA AMS 5687
 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
　
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