B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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)
C. 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 57-55-11-000-004 Removal of the Flap Track Fairings Nos. 2, 3 and 4 57-55-11-400-004 Installation of the Flap Track Fairings Nos. 2, 3 and
4 NTM 57-53-09 PART 9 ASRM 575300 (for corrective action) 57-53-00-991-030 Fig. 626
3. Job Set-up
__________
Subtask 57-53-00-941-083
A. Safety Precautions
(1)
Put a warning notice on the flap/slat control lever (panel 114VU) to tell persons not to operate the flaps.
(2)
Put the safety barriers in position.
Subtask 57-53-00-860-056
B. 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) Extend the flaps fully (Ref. TASK 27-50-00-866-008).
1EFF : 301-399, 1 57-53-00Page A683 1 1 Nov 01/04R 1 1 1CES 1
(2) Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is installed on the flap/slat control lever on the panel 114VU.
Subtask 57-53-00-865-113
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 57-53-00-010-077
D. Get Access
(1)
Put the access platform in position below the flap track 3 at zone 532(632).
(2)
Remove the access panel 532AT (632AT) and the flap track 3 fairing 532CB (632CB) (Ref. TASK 57-55-11-000-004).
(3)
Remove the access panel 587AB (687AB), in the bottom skin at track 3.
(4)
Put the spark-proof lamp adjacent to the inspection area.
4. Procedure
_________ (Ref. Fig. 626/TASK 57-53-00-991-030) 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.
Subtask 57-53-00-110-081
A. Preparation for Inspection
(1) Use a MISCELLANEOUS (Material No. 19-003), made moist with CLEANING AGENTS (Material No. 11-026) to clean internal support fitting at track 3, inboard and outboard Rib 5 and Rib 6, attachment bracket and drive bracket.
1EFF : 301-399, 1 57-53-00Page A684 1 1 Nov 01/04R 1 1 1CES 1
Outboard Flap -Track 3 Support Attachments - Inspection Area
Figure 626/TASK 57-53-00-991-030
1EFF : 301-399, 1 57-53-00Page A685 1 1 Nov 01/04R 1 1 1CES 1
Subtask 57-53-00-280-062
B. Inspection
(1) Do a special detailed inspection (Ref. NTM 57-53-09 PART 9) of:
-
the internal support fitting at Track 3
-
the inboard and outboard Rib 5 and Rib 6
-
the attachment bracket
-
the drive bracket.
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. ________
5. Close-up
Subtask 57-53-00-410-076
A. Close Access
(1)
Remove the spark-proof lamp from the inspection area.
(2)
Install the access panel 587AB (687AB).
(3)
Install the flap track 3 fairing 532CB (632CB) and the access panel 532AT (632AT) (Ref. TASK 57-55-11-400-004).
中國航空網 m.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(11)
