R Subtask 10-12-00-620-093

R  F. Protection 
R  (1) Apply SPECIAL MATERIALS (Material No. 05-027) in all the holes, 
R  specially in the area which can have condensation. On the wings, 
R  apply SPECIAL MATERIALS (Material No. 05-005). 
R  (2) Apply COMMON GREASE (Material No. 04-011) on : 
R  - the sliding tube of the shock absorber 
R  - the actuator rods 
R  - the uplock mechanism. 
R  Subtask 10-12-00-210-075 
R  G. Inspection of the Hydraulic System 
R  (1) Do a check of the reservoir fluid level (Ref. TASK 29-10-00-200-001). 
R  (2) Do a check for corrosion on hydraulic pipes and unions on the landing 
R  gear wells, the wings and the stabilizers. 
R  Subtask 10-12-00-210-076 
R  H. Inspection of the Flight Controls 
R  (1) Check of the condition of the flight control cables in 
R  non-pressurized area and avionics compartment. 
R  (2) Do a check of all the flap tracks for corrosion. 
R  (3) Do a check of the slat tracks for corrosion. 
R  Subtask 10-12-00-210-077 
R  J. Inspection of the Fuel System 
R  (1) Do a check of the fuel level in the tanks: 
R  (a) if necessary refuel the tank(s): 
R  - to 30 % minimum if no contamination occured 
R  - to 90 % minimum if contamination occured. 
R  NOTE : We recommend that you do not mix fuel treated with____ 
R  different biocides.

R Subtask 10-12-00-210-078

R  K. Inspection of the Engines 
R  (1) You must do again the preservation of the engines at one year 
R  interval (Ref. TASK 72-00-00-600-008). 
R  (2) Do a check of the IDG for external corrosion. 
R  5. Close-up________ 
R  Subtask 10-12-00-942-060 
R  A. Put the aircraft back to its initial configuration. 
R  (1) On the overhead panel 25 VU, on the CABIN PRESS section : 
R  - release the DITCHING pushbutton switch to close the avionics 
R  ventilation skin valves and the outflow valve. 
R  (2) Depressurize the aircraft hydraulic systems (Ref. TASK 29-23-00-864-
R  001), (Ref. TASK 29-24-00-864-001), (Ref. TASK 29-10-00-864-003). 
R  (3) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-
R  002). 
R  (4) Install STORAGE PRESERVATION (Material No. 15-002) with new adhesive 
R  tape to prevent film hardening and paint removal. 
R  (5) Remove all the fixtures, tools, test and support equipment used 
R  during this procedure.

R TASK 10-12-00-200-010

R  Periodic Ground Check at 6-month Intervals 
R  1. Reason for the Job__________________ 
R  This procedure prevents the damage of the landing gears seals. 
R  2. Job Set-up Information______________________ 
R  A. Referenced Information 
R  -------------------------------------------------------------------------------
R  REFERENCE  DESIGNATION 
R  -------------------------------------------------------------------------------

R  32-31-00-720-002  Functional Test of the Normal Extension and 
R  Retraction of the Landing Gear 
R  3. Job Set-up__________ 
R  Subtask 10-12-00-860-065 
R  A. Not Applicable 
R  4. Procedure_________ 
R  Subtask 10-12-00-700-050 

R  A. Test of the Landing Gear 
R  (1) Do a test of extension and retraction of the landing gear (Ref. TASK 
R  32-31-00-720-002) 
R  5. Close-up________ 
R  Subtask 10-12-00-942-062 
R  A. Put the aircraft back to its initial configuration. 
R  (1) Remove all the fixtures, tools, test and support equipment used 
R  during this procedure.

 MOORING - MAINTENANCE PRACTICES
_______________________________
 TASK 10-20-00-556-001
 Mooring of the Aircraft
 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
 GEAR.

 WARNING : MAKE SURE THAT THE WHEEL CHOCKS ARE IN POSITION.
_______
 CAUTION : THE LAST FEET OF ALL TAXIING AND TOWING OPERATIONS MUST BE IN A
　
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