B. Consumable Materials

 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
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
 -------------------------------------------------------------------------------
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
 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):
 -------------------------------------------------------------------------------
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
　
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