Subtask 57-53-00-865-133

 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
 Subtask 57-53-00-010-087
 D. Get Access
 (1)
 Put the access platform in position below the flap track 4 at zone 587(687).

 (2)
 Remove the access panel 533AT (633AT) and the flap track 4 fairing 533CB (633CB) (Ref. TASK 57-55-11-000-004).

 (3)
 Put the spark-proof lamp adjacent to the inspection area.

 4. Procedure
_________ (Ref. Fig. 636/TASK 57-53-00-991-040) Subtask 57-53-00-110-091
 A. Preparation for Inspection
 (1) Use a MISCELLANEOUS (Material No. 19-003), made moist with CLEANING AGENTS (Material No. 11-026) to clean the outboard double slotted flap, tab articulation at track 4, LH/RH.
 Subtask 57-53-00-280-066
 B. Inspection
 (1) Do a special detailed inspection of the tab articulation components and the internal surface of the tab at track 4 RH/LH. Refer to the (Ref. NTM 575341 PART 9), for the inspection procedure.
 NOTE : If necessary, refer to the ASRM (Ref. ASRM 575300) for the
____ correct repair procedure. If the defect is not included in this repair, you must request a procedure from Airbus Industrie.

 Outboard Flap - Tab Articulation at Track 4 - Inspection Area
 Figure 636/TASK 57-53-00-991-040

 5. Close-up
________

 Subtask 57-53-00-410-086
 A. Close Access
 (1)
 Remove the spark-proof lamp from the inspection area.

 (2)
 Install the flap track 4 fairing 533CB (633CB) and the access panel 533AT (633AT) (Ref. TASK 57-55-11-400-004).

 (3)
 Make sure that the work area is clean and clear of tool(s) and other items.

 Subtask 57-53-00-865-134
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV.
 Subtask 57-53-00-860-077
 C. Aircraft Maintenance Configuration
 (1) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever.
 (2) Fully retract the flaps (Ref. TASK 27-50-00-866-009). panel 114VU. Subtask 57-53-00-942-090
 D. Removal of Equipment
 (1)
 Remove the access platform(s).

 (2)
 Remove the safety barriers.

 (3)
 Remove the warning notice(s).

 (4)
 Make sure that the work area is clean and clear of tool(s) and other items.

 TASK 57-53-00-220-020
 Special Detailed Inspection of Outboard Double Slotted Flap, Rib 2, 9 and 12, LH/RH
 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: 575343-01
 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 spark-proof lamp No specific warning notice No specific access platform 2.5 m (8 ft. 2 in.)

 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 08-061A D DAN 220
 ALUMINIUM FOIL ADHESIVE TAPE (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)
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM WINGS 機翼5(26)