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REFERENCE DESIGNATION
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R  72-00-00-600-008 Preservation Renewal Requirements. 
R  3. Job Set-up__________ 
R  Subtask 10-12-00-941-055 
R  A. Get Access 
R  (1) Put an ACCESS PLATFORM 15M (49 FT) - ADJUSTABLE in position near the 
R  aircraft. 
R  4. Procedure_________ 
R  Subtask 10-12-00-210-073 
R  A. Visual Inspection 
R  (1) Do a visual inspection of the aircraft for impacts by foreign 
R  objects, bird nests, fluid leakages, (hydraulic fluid, fuel), missing 
R  parts, obstruction and corrosion of: 
R  (a) the upper and the lower surface of the wing 
R  (b) the nacelles and the pylons 
R  (c) the external surfaces of the fuselage 
R  (d) the flight control surfaces 
R  (e) the leading and the trailing edge of the horizontal and vertical 
R  stabilizers 
R  (f) the external skin of: 
R  - the passenger/crew doors 
R  - the cargo doors 
R  - the frame around the doors 
R  (g) the external handle of the passenger/crew doors 
R  (h) the drains: 
R  1 In the lower fuselage (Ref. TASK 53-59-00-210-001)._

R  2 On the pylons (Ref. TASK 54-50-00-200-001)_ 
R  3 In all other locations._ 
R  (i) the toilet areas 
R  (j) all steel parts for corrosion. 
R  (2) If you find corrosion, remove it (Ref. TASK 51-74-11-300-001). 
R  Subtask 10-12-00-615-056 
R  B. Cleaning of the Aircraft 
R  (1) Remove all the STORAGE PRESERVATION (Material No. 15-002) and 
R  adhesive tapes. 
R  (2) We recommend to clean the aircraft externally (Ref. TASK 12-21-11-
R  615-001). 
R  Subtask 10-12-00-650-055 
R  C. Aircraft Configuration 
R  (1) Energize the aircraft electrical circuits from the external power 
R  (Ref. TASK 24-41-00-861-002). 
R  (2) On the overhead panel 25 VU, on the CABIN PRESS section: 
R  - release the DITCHING pushbutton switch to open the avionics 
R  ventilation skin valves and the outflow valves. 
R  NOTE : Make sure that the avionics ventilation continues to operate____ 
R  correctly. 
R  (3) Pressurize the aircraft hydraulic systems (Ref. TASK 29-23-00-863-
R  001), (Ref. TASK 29-24-00-863-001), (Ref. TASK 29-10-00-863-003). 
R  Subtask 10-12-00-710-070 
R  D. Do these Tests: 
R  (1) Do a test of the crossfeed valves (Ref. TASK 28-23-00-720-001). 
R  (2) Do a test the engine LP-fuel shut-off valve (Ref. TASK 28-24-00-710-
R  002). 
R  (3) Do a test of the APU shut-off valve (Ref. TASK 28-29-00-710-001).

R  (4) Do a test of the aileron and its hydraulic system (Ref. TASK 27-14-
R  00-710-001). 
R  (5) Do a test of the elevator and its hydraulic system (Ref. TASK 27-34-
R  00-710-001). 
R  (6) Do a test of the rudder hydraulic actuation (Ref. TASK 27-24-00-710-
R  001). 
R  (7) Do a test of the flap system (Ref. TASK 27-54-00-710-001). 
R  (8) Do a test of the spoiler hydraulic system (Ref. TASK 27-64-00-710-
R  001). 
R  (9) Do a test of the slat system (Ref. TASK 27-84-00-710-001). 
R  (10) Do a test of the landing gear doors (Ref. TASK 32-31-00-710-002). 
R  Subtask 10-12-00-210-074 
R  E. Inspection of the Landing Gear 
R  (1) Do a general visual inspection: 
R  - of the NLG (Ref. TASK 05-27-10-200-001) 
R  - of the MLG (Ref. TASK 05-27-30-200-001) 
R  (2) Remove the mooring tool from the NLG. 
R  (3) Lift and turn the wheels by hand to make sure that there is no defect 
R  on the bearings: 
R  - for NLG (Ref. TASK 07-12-00-582-001) 
R  - for MLG (Ref. TASK 07-12-00-582-002) 
R  (4) Put the aircraft on its wheels. 
R  (5) Put the aircraft in mooring condition (Ref. TASK 10-20-00-556-001). 
R  (6) Do a Check of each wheel-half for corrosion. If you find corrosion, 
R  clean with CLEANING AGENTS (Material No. 11-002). 
　
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