(5)
Remove the safety barriers.
(6)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-51-00Page A622 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 **ON A/C 301-399,
TASK 57-51-00-200-009- 01
R Detailed Inspection of Outer Wing, Bottom Skin Lower Surface, Aft of Rear Spar, R Under Flap Track 2 and Flap Tab Drive 1A Fairing
1. Reason for the Job
__________________
Refer to the MPD TASK: 575165-01
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 warning notices
No specific access platform 2.5 m (8 ft. 2 in.)
98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER
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 -------------------------------------------------------------------------------
57-55-11-000-004 Removal of the Flap Track Fairings Nos. 2, 3 and 4 57-55-11-000-005 Removal of the Inboard and Outboard Flap Tab Hinge-Fairings ASRM 575100 (for corrective action)
R 3. Job Set-up__________
R Subtask 57-51-00-941-081
R A. Safety Precautions
R (1) Put warning notices in the cockpit to tell persons not to operate the
R flaps or slats.
R (2) Put the safety barriers in position.
R (3) Install the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001)
R on the flap/slat control lever.
R Subtask 57-51-00-865-107
R B. Open, safety and tag this(these) circuit breaker(s):
R -------------------------------------------------------------------------------
R PANEL DESIGNATION IDENT. LOCATION
R -------------------------------------------------------------------------------
R 49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07
R 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
R Subtask 57-51-00-010-084
R C. Get Access
R (1) Put the access platform below the applicable wing to get access to
R the:
R - flap track 2 fairings, zone 531(631)
R - flap tab hinge 1A fairing, zone 535(635).
R (2) Remove the applicable fairing access panels (Ref. TASK 57-55-11-000-
R 004) and (Ref. TASK 57-55-11-000-005):
R - for the left wing, remove 531CB, 531EB, 535AB, 535BB
R - for the right wing, remove 631CB, 631EB, 635AB, 635BB.
R 1EFF : 301-399, 1 57-51-00Page A624 1 1 May 01/04 1 1 1CES 1
R 4. Procedure
_________
R Subtask 57-51-00-110-091
R A. Preparation for Inspection
R (1) Use a MISCELLANEOUS (Material No. 19-003), made moist with CLEANING
R AGENTS (Material No. 11-026) to clean:
R - the lower surface of the bottom skin in the area of the outer wing
R under the flap track 2 fairing.
R Subtask 57-51-00-210-072
R B. Inspection
R (1) Examine the lower surface of the bottom skin in the area of the outer
R wing:
R - under the flap track 2 fairing
R - under the flap tab drive 1A fairing.
R (2) Make sure that:
R - there is no damage
R - there is no corrosion
R - the surface protection is in the correct condition.
R NOTE : If necessary, refer to the ASRM (Ref. ASRM 575100) for the____
R correct repair procedure.
R 5. Close-up________
R Subtask 57-51-00-410-085
R A. Close Access
R (1) Install the applicable fairing access panels (Ref. TASK 57-55-11-000-
R 004) and (Ref. TASK 57-55-11-000-005):
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3(109)
