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R  20-21-11-911-001 Tightening Torques for Standard Threaded Fasteners 
R  27-50-00-866-009 Retraction of the Flaps on the Ground 
R  57-55-11-400-004 Installation of the Flap Track Fairings Nos. 2, 3 and 
R  4 
R  3. Job Set-up__________ 
R  Subtask 57-55-11-941-072 
R  A. Safety Precautions 
R  (1) Make sure that the warning notices are in position in the cockpit to 
R  tell persons not to operate the flaps or slats. 
R  (2) Make sure that the safety barriers are in position. 
R  Subtask 57-55-11-860-074 
R  B. Aircraft Maintenance Configuration 
R  (1) Make sure that the flaps are in the fully retracted position 
R  (Ref. TASK 27-50-00-866-009). 
R  (2) Make sure that the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER is 
R  installed on the flap/slat control-lever. 
R  Subtask 57-55-11-865-078 
R  C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and 
R  tagged 
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  4. Procedure_________ 
R  Subtask 57-55-11-420-079 
R  A. Preparation for Installation 
R  (1) Use a MISCELLANEOUS (Material No. 19-003), made moist with CLEANING 
R  AGENTS (Material No. 11-026) to clean the component interface and/or 
R  the adjacent area. 
R  (2) Do an inspection of the component interface and/or the adjacent area. 
R  (3) Make sure that the parts retained from the removed component are 
R  clean and in the correct condition. 
R  Subtask 57-55-11-420-078 
R  B. Installation of the Flap Track 2 Fairing Bracket and Link Assembly 
R  (1) Assemble the bracket and link assembly as follows: 
R  (a) Install the sleeve (2) into the bracket (1) and the link assembly 
R  (4). 
R  (b) Install the bolt (3), the washer (5) and the nut (6). 
R  (c) Torque the nut (6) to 0.5 m.daN (44.24 lbf.in). 
R  (d) Safety the nut (6) with a new cotter pin (7). 
R  NOTE : When you install the bracket and link assembly to the____ 
R  wing, make sure you do not move the bracket attachment 
R  bolts. 
R  (2) Apply SEALANTS (Material No. 09-002) between the mating surfaces of 
R  the wing and the bracket and link assembly. 
R  (3) Carefully put the bracket and link assembly in position on the wing. 
R  (4) Install the nuts (8). 
R  (5) Torque the nuts (8) (Ref. TASK 20-21-11-911-001).

 

R  5. Close-up________ 
R  Subtask 57-55-11-410-061 
R  A. Close Access 
R  (1) Install the flap track 2 fixed fairing 531EB (631EB) (Ref. TASK 57-
R  55-11-400-004). 
R  Subtask 57-55-11-865-079 
R  B. Remove the safety clip(s) and the tag(s) and close this(these) circuit 
R  breaker(s): 
R  6CV, 8CV. 
R  Subtask 57-55-11-860-075 
R  C. Aircraft Configuration 
R  (1) Remove the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER from the flap/slat 
R  control-lever. 
R  Subtask 57-55-11-942-062 
R  D. Removal of Equipment 
R  (1) Make sure that the work area is clean and clear of tool(s) and other 
R  items. 
R  (2) Remove the access platform(s). 
R  (3) Remove the warning notice(s). 
R  (4) Remove the safety barriers. 
R  (5) Remove the ground support and maintenance equipment, the special and 
R  standard tools and all other items.

 

 Adjustment of the Hinge 1A Forward Fairing R Figure 418/TASK 57-55-11-991-020
 1EFF : 301-399, 1 57-55-11Page A403 1 1 Aug 01/04 1 1 1CES 1

 FAIRING - FLAPS - INSPECTION/CHECK__________________________________
 TASK 57-55-11-200-001
 Check of the Flap Track Fairing Lateral Movement
 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.
　
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