(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): 
　
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