(4)
Close the FWD and aft cargo-compartment doors (Ref. TASK 52-30-00-860-002).
(5)
Close the bulk cargo door (Ref. TASK 52-30-00-860-008).
(6)
Close all the landing gear doors (Ref. TASK 32-22-00-410-001), (Ref. TASK 32-12-00-410-001).
(7)
Close all the access door panels that you opened during the storage procedure.
(8)
Seal with STORAGE PRESERVATION (Material No. 15-002) and adhesive tape all the openings that give access to:
-
the passenger compartment,
-
the cockpit,
-
the cargo compartement,
-
the APU,
-
the engines,
-
the landing gears.
(9)
Seal with adhesive tape:
-
the passenger/crew door handles,
-
the emergency exit door handles,
-
the FWD and aft cargo door handles,
-
the bulk cargo door handle
-
the avionics-compartment doors handles.
R EFF : 004-049, 055-099, 101-149, 151-199, 10-12-00Page 226 201-299, 301-399, 401-499, Aug 01/05 CES
(10)
Depressurize the aircraft hydraulic systems (Ref. TASK 29-23-00-864-001), (Ref. TASK 29-24-00-864-001), (Ref. TASK 29-10-00-864-003).
(11)
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
(12)
Remove all the fixtures, tools, test and support equipment used during this procedure.
(13)
Make an entry in the aircraft log book or attach a tag on the Captain side stick to tell the crew that the protection covers/devices are installed.
R EFF : 301-399, 10-12-00Page 227 May 01/05 CES
**ON A/C ALL
TASK 10-12-00-553-007
Storage Procedure (Storage Not More than 2 Years)
CAUTION : MAKE SURE THAT YOU OBEY THE MAINTENANCE PROGRAM FOR STORED/ PARKED
_______ AIRCRAFT. DO NOT CHANGE OR STOP THE MAINTENANCE PROGRAM WITHOUT APPROVAL FROM YOUR LOCAL AUTHORITIES.
CAUTION : DURING THIS PROCEDURE:
_______
-MAKE SURE THAT THE LANDING GEAR GROUND SAFETIES, LOCKING DEVICES AND WHEEL CHOCKS ARE IN POSITION.
-KEEP THE ACCESS PLATFORM AT A SUFFICIENT DISTANCE FROM THE AIRCRAFT (IN WIND, SHOCK ABSORBER REBOUND CAN CAUSE MOVEMENT OF THE AIRCRAFT).
1. Reason for the Job
__________________
This procedure gives the preservation steps for a storage period of not more than 2 years.
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific blanking caps No specific talcum No specific wheel chocks No specific 1 WARNING NOTICE
EFF : ALL 10-12-00Page 228 May 01/05R CES
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 02-003 F NSA 307110 TYPE 4
HYDRAULIC FLUID (PHOSPHATE ESTER BASE)
(Ref. 20-31-00)
Material No. 03-001 USA MIL-PRF-7870
MINERAL OIL (LOW TEMP) (Ref. 20-31-00)
Material No. 04-001 F AIR-4205
WHEEL BEARING MINERAL GREASE (Ref. 20-31-00)
Material No. 04-004 USA MIL-PRF-23827 TYPE I
SYNTH.ESTER BASED GREASE HIGH PRESSURE
(Ref. 20-31-00)
Material No. 04-011 USA MIL-G-4343
SILICONE GREASE PNEUMATIC SYST AND SEALS
(Ref. 20-31-00)
Material No. 05-005 USA MIL-C-16173 GRADE II
CORROSION PREVENTIVE (Ref. 20-31-00)
Material No. 05-027 USA MIL-L-81309
RUST INHIBITOR(FOR CORROSION USE 15-004)
(Ref. 20-31-00)
Material No. 05-043 VARNISH P.T.F.E SPRAY (Ref. 20-31-00) Material No. 15-002 USA MIL-B-131 TYPE I BARRIER MATERIAL WATER VAPOR PROOF (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
05-57-00-200-001 Aircraft Stability 10-11-00-555-013 Protection Equipment for Parking or Storage Procedure 10-20-00-556-001 Mooring of the Aircraft 12-16-38-613-001 Servicing of the Toilet System 12-21-11-615-001 External Cleaning 12-21-12-100-002 Cleaning of the Cockpit Equipment/Furnishings
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