-
FLP LH PROX SNSR 2 OR WIRING TO
LGCIU 2
-
FLP RH PROX SNSR 2 MISADJUSTMENT and FLP RH PROX SNSR 1 OR WIRING TO LGCIU 1
-
FLP RH PROX SNSR 1 OR WIRING TO
LGCIU 1
-
FLP RH PROX SNSR 2 OR WIRING TO
LGCIU 2.
E. Aircraft Maintenance Configuration
(1)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is
installed on the flap/slat control lever.
(2)
Install the upper and lower kink-seals (1) and (2) to the inboard and the outboard flaps (Ref. TASK 27-54-61-400-006).
(3)
Make sure that the flaps are fully retracted (Ref. TASK 27-50-00-866-009).
1EFF : ALL 1 27-51-44Page 614 1 1 May 01/04R 1 1 1CES 1
Subtask 27-51-44-710-053
F. Test
(1) Do an operational test of the flap system (Ref. TASK 27-54-00-710-001).
Subtask 27-51-44-942-054
G. 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.
1EFF : ALL 1 27-51-44Page 615 1 1 May 01/04R 1 1 1CES 1
TASK 27-51-44-960-001
Replacement of the Flap Interconnecting Strut Rod-End
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
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
No specific safety barriers
No specific warning notice(s)
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) 98D27504031000 1 PIN-SETTING 98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
1EFF : ALL 1 27-51-44Page 616 1 1 May 01/04R 1 1 1CES 1
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-026 GB DEF-STAN 68-148/1 SOLVENT GENERAL PURPOSE (Ref. 20-31-00)
Material No. 15-007 AIB TN 10138 TYPE II GRADE 1 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (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 (Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM --------- |DESIGNATION ---------------------------------------- |IPC-CSN------------------------------
9 rod end. 27-51-44 01 -010
9 rod end. 27-51-44 01 -010A
9 rod end. 27-51-44 01A-010A
14 cotter pin 27-51-05 01 -100
14 cotter pin 27-51-05 01A-100
D. Referenced Information
------------------REFERENCE -------------------------------DESIGNATION ------------------------------
-------------------------------------------------------------------------------
27-50-00-866-008 Extension of the Flaps on the Ground 27-50-00-866-009 Retraction of the Flaps on the Ground 27-51-00-710-002 Operational Test of the Flap Interconnecting Strut
and the Flap-Attachment Failure-Detection Sensors 27-51-00-820-003 To Do a Check of the Flap Rigged Position (With the
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱4(120)
