B. Consumable Materials
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REFERENCE DESIGNATION
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Material No. 04-024 AIB AIMS 09-06-001
SYNTHETIC GREASE FOR FLAP & SLAT MECHANISM
(Ref. 20-31-00)
Material No. 11-026 GB DEF-STAN 68-148/1 R 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
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REFERENCE DESIGNATION
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27-50-00-866-008 Extension of the Flaps on the Ground
27-50-00-866-009 Retraction of the Flaps on the Ground
ASRM 575100 (for corrective action)
57-52-00-991-001 Fig. 601
3. Job Set-up
__________
Subtask 57-52-00-941-050
A. Safety Precautions
(1)
Put warning notices in the cockpit to tell persons not to operate the flaps or slats.
(2)
Put the safety barriers in position.
Subtask 57-52-00-860-077
B. Aircraft Maintenance Configuration
(1)
Fully extend the flaps (Ref. TASK 27-50-00-866-008).
(2)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) is installed on the flap/slat control lever.
(3)
Put the access platform below the applicable wing trailing edge at flap track 2, zone 531 (631).
Subtask 57-52-00-865-050
C. Open, safety and tag this(these) circuit breaker(s):
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PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
R 49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 6CV 8CV B07Q21
4. Procedure_________
(Ref. Fig. 601/TASK 57-52-00-991-001)
R R R R R R 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 57-52-00-110-050
A. Preparation for Inspection
(1) Use a MISCELLANEOUS (Material No. 19-003), made moist with CLEANING AGENTS (Material No. 11-026) to clean: - the rollers (1), (2) and (5) of the flap track carriage assembly (4) - the component interface and the adjacent area.
Subtask 57-52-00-210-050
B. Inspection
(1) Examine the rollers (1), (2) and (5) of the carriage assembly (4), to make sure that: - there is no corrosion - there are no cracks - the rollers are correctly attached - the rollers are symmetrical - there is no distortion of the rollers or their attachment pivot bolts - there is not too much wear of the rollers (1), (2) and (5) or signs of grooves or marks on the flap track (3).
Flap-track 2 Rollers
Figure 601/TASK 57-52-00-991-001
1EFF : ALL 1 57-52-00 Page 604
1 1 Feb 01/98
1 1
1CES 1
NOTE : If necessary, refer to the ASRM (Ref. ASRM 575100) for the
____
correct repair procedure.
5. Close-up
________
Subtask 57-52-00-640-050
A. Lubrication
(1) Use COMMON GREASE (Material No. 04-024) to lubricate the flap-track rollers through the greasers until the new grease comes out.
Subtask 57-52-00-865-051
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
R 49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 122VU FLIGHT CONTROLS/WTB/FLP/SYS1 10CV S07
Subtask 57-52-00-860-078
C. Aircraft Maintenance Configuration
(1) Make sure that the work area is clean and clear of tool(s) and other items.
(2) Retract the flaps fully (Ref. TASK 27-50-00-866-009).
Subtask 57-52-00-942-050
D. Removal of Equipment 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM WINGS 机翼4(13)
