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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