A320飞机维护手册 AMM LANDING GEAR 起落架8(65)

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R  WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING_______ 
R  GEAR. 
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  safety barriers 
R  No specific  warning notice 
R  No specific  Torque Wrench : range 0.00 to 1.20 m.daN 
R  (0.00 to 9.00 lbf.ft) 
R  B. Consumable Materials 
R  -------------------------------------------------------------------------------
R  REFERENCE  DESIGNATION 
R  -------------------------------------------------------------------------------
R  Material No. 04-001  F  AIR-4205 
R  WHEEL BEARING MINERAL GREASE (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)

 1EFF : 051-099, 1 32-49-18Page 404 1 1 May 01/05 1 1 1CES 1R C. Referenced Information

R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R  32-00-00-481-001  Installation of the Safety Devices on the Landing 
R  Gears 
R  32-42-00-720-002  Functional test of the tachometers 
R  32-48-51-000-005  Removal of the Fan Assy (7GS,8GS,9GS,10GS) 
R  32-48-51-400-005  Installation of the Fan Assy (7GS,8GS,9GS,10GS) 
R  32-49-00-710-001  Operational Test of the Tire Pressure Indicating 
R  System (TPIS) 
R  32-49-18-991-001  Fig. 401 
R  3. Job Set-up__________ 
R  Subtask 32-49-18-941-052 
R  A. Safety Precautions 

R  (1) Make sure that the safety barriers are in position. 
R  (2) Make sure that the ground safety locks are on the landing gear 
R  (Ref. TASK 32-00-00-481-001). 
R  (3) On the panel 400VU: 
R  - make sure that the landing-gear control-lever 6GA is in the DOWN 
R  position 
R  - make sure that the warning notice to tell persons not to operate 
R  the landing gear is in position. 
R  Subtask 32-49-18-860-052 
R  B. Aircraft Maintenance Configuration 
R  (1) Make sure that the fan assembly is removed (Ref. TASK 32-48-51-000-
R  005).

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R  Subtask 32-49-18-865-051 
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  121VU HYDRAULIC/TIRE/PRESS 1GV M31 
R  4. Procedure_________ 
R  (Ref. Fig. 401/TASK 32-49-18-991-001) 
R  Subtask 32-49-18-420-050 
R  A. Preparation for Installation 
R  (1) Clean the component interface and/or the adjacent area with a 
R  MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS 
R  (Material No. 11-026). 
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  (4) Apply a thin layer of COMMON GREASE (Material No. 04-001) to these 
R  components: 
R  - the internal surface of the mounting sleeve 
R  - the mounting studs of the rotating mechanism (4) 
R  - the washers (6) 
R  - the nuts (7). 
R  (5) Lightly lubricate the first 100 mm (4.0 in.) of the internal surface 
R  of the axle with COMMON GREASE (Material No. 04-001). 
　
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