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R  - THE LANDING GEAR AND THE RELATED DOORS 
R  - COMPONENTS THAT MOVE. 
R  1. Reason for the Job__________________ 
R  Self Explanatory 
R  2. Job Set-up Information______________________ 
R  A. Fixtures, Tools, Test and Support Equipment 
R  -------------------------------------------------------------------------------
R  REFERENCE  QTY DESIGNATION 
R  -------------------------------------------------------------------------------
R  No specific  non-metallic scraper 
R  No specific  safety barriers 
R  No specific  warning notice 
R  No specific  access platform 3.2 m (10 ft. 6 in.) 
R  B. Consumable Materials 
R  -------------------------------------------------------------------------------
R  REFERENCE  DESIGNATION 
R  -------------------------------------------------------------------------------
R  Material No. 05-013A  C  Z-24.223 
R  RELEASE AGENT (Ref. 20-31-00) 
R  Material No. 09-005  USA MIL-S-81733  CLASS C 
R  CORROSION INHIBITIVE INTERFAY SEALANT (Ref. 20-31-00) 
R  Material No. 11-026  GB  DEF-STAN  68-148/1 
R  SOLVENT GENERAL PURPOSE (Ref. 20-31-00) 
R  Material No. 19-003  USA AMS 3819 
R  LINT-FREE COTTON CLOTH (Ref. 20-31-00)

 

R C. Referenced Information

R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R  27-80-00-866-004  Extending the Slats on the Ground 
R  27-80-00-866-005  Retracting the Slats on the Ground 
R  57-41-37-991-028  Fig. 406 
R  3. Job Set-up__________ 
R  Subtask 57-41-37-941-073 
R  A. Safety Precautions 

R  (1) Make sure that the safety barriers are in position. 
R  Subtask 57-41-37-860-068 
R  B. Aircraft Maintenance Configuration 
R  (1) Make sure that the slats are fully extended (Ref. TASK 27-80-00-866-
R  004). 
R  (2) Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is 
R  installed on the flap/slat control lever. 
R  (3) Make sure that the warning notice is in position in the cockpit to 
R  tell persons not to operate the slats. 
R  (4) Make sure that the access platform is in position below the 
R  applicable access panel 521BT(621BT). 
R  Subtask 57-41-37-865-088 
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/SLT/CTL AND MONG/SYS1  5CV  B06 
R  121VU FLIGHT CONTROLS/SLT/CTL/SYS2  7CV  R21

R 4. Procedure
_________

R  (Ref. Fig. 406/TASK 57-41-37-991-028) 
R  Subtask 57-41-37-210-063 
R  A. Preparation for Installation 
R  WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THE SPECIAL_______ 
R  MATERIAL. 
R  THIS MATERIAL IS DANGEROUS. 
R  (1) Do an inspection of the component interface and/or the adjacent area. 
R  (2) Use a non-metallic scraper and a MISCELLANEOUS (Material No. 19-003) 
R  made moist with CLEANING AGENTS (Material No. 11-026) to clean: 
R  - the interface of the aircraft structure 
R  - the mating surfaces of the access panel (3). 
R  (3) Apply SEALANTS (Material No. 09-005) to the interface of the aircraft 
R  structure. 
R  (4) Apply SPECIAL MATERIALS (Material No. 05-013A) to the mating surfaces 
R  of the access panel (3). 
R  (5) Make sure that the work area is clean and clear of tool(s) and other 
R  items. 
R  Subtask 57-41-37-420-063 
R  B. Installation of the Access Panel 521BT(621BT) 
R  CAUTION : MAKE SURE THAT THE ACCESS PANEL SCREWS ARE INSTALLED IN THEIR_______ 
R  CORRECT POSITIONS. INCORRECT INSTALLATION OF THE SCREWS CAN 
R  CAUSE DAMAGE TO THE SLATS DURING SLAT MOVEMENT. 
　
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