(b)
Attach the drive cable (1) to the sliding panel with the screw (2).
(c)
Make sure that the DIM A between the drive trunnion and the sliding panel is 6 mm (0.2362 in.) +/- 3 mm (0.1181 in.).
(d)
Torque tighten the screw (2) to between 0.40 and 0.45 m.daN
(35.39 and 39.82 lbf.in).
(2)
Make sure that the work area is clean and clear of tool(s) and other items.
R 1EFF : 001-001, 051-052, 1 27-54-00Page A613 1 1 May 01/05 1 1 1CES 1
(3) Remove the spark-proof lamp from the inspection area.
(4) Remove the access platform(s). Subtask 27-54-00-865-066
B. Make sure that this(these) circuit breaker(s) is(are) closed:
6CV, 8CV.
Subtask 27-54-00-860-055
C. Aircraft Maintenance Configuration WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
_______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
(1)
Close the MLG doors (Ref. TASK 32-12-00-410-001).
(2)
Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever.
(3) Retract the flaps fully (Ref. TASK 27-50-00-866-009). Subtask 27-54-00-942-066
D. Removal of Equipment
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the safety barriers.
(3)
Remove the warning notice(s).
(4)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
R 1EFF : 001-001, 051-052, 1 27-54-00Page A614 1 1 May 01/05 1 1 1CES 1 **ON A/C ALL
TASK 27-54-00-220-006
Detailed Inspection of Inboard Flap Drive Trunnions in the Sliding Panel Hook Area For Wear.
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
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
__________________
Refer to the MPD TASK: 275100-07
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers
No specific spark-proof lamp
No specific warning notice
No specific access platform 3 m (9 ft. 10 in.)
R No specific Torque Wrench : range 0.00 to 1.20 m.daN
R (0.00 to 9.00 lbf.ft)
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 09-013 Material No. 11-026 Material No. 19-003 Material No. 19-010 USA MIL-PRF-81733 TYPE I CLASS A CORROSION INHIBITING BRUSH CONSISTENCY (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)USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-34-24-869-002 27-50-00-866-008 27-50-00-866-009 27-54-00-710-001 32-12-00-010-001 32-12-00-410-001 53-35-11-000-001 53-35-11-400-001 Aircraft Grounding for the Maintenance OperationsExtension of the Flaps on the GroundRetraction of the Flaps on the GroundOperational Test of the Flap SystemOpen the Main Gear Doors for AccessClose the Main Gear Doors after AccessRemoval of the Wing-to-Fuselage FairingsInstallation of the Wing-to-Fuselage Fairings
R **ON A/C ALL
R Post SB 27-1117 For A/C 001-001,051-052,
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