-all the spoiler servo-control bearings (Ref. TASK 12-22-27-640-005).
 -
the slat tracks surface with OILS (Material No. 03-001)

 -
the flap rotary actuators (Ref. TASK 12-22-27-640-008).

 Subtask 10-12-00-620-075
 G. Protection of the Engines
 (1)
 For a period up to 30 days, do the preservation of the engines (Ref. TASK 72-00-00-600-006).

 (2)
 For a period up to 90 days, do the preservation of the engines (Ref. TASK 72-00-00-600-025).

 (3)
 For a period of 90 days to one year, do the preservation of the engines (Ref. TASK 72-00-00-600-007).

 (4)
 Do the IDG on wing preservation.

 EFF : ALL  10-12-00Page 217   May 01/05R   CES

 **ON A/C 001-049, 101-105, 151-199, 201-210,

 Subtask 10-12-00-620-076-A
 H. Protection of the APU
 (1)
 Do the preservation of the APU (Ref. TASK 49-20-00-600-003).

 (2)
 If necessary, apply SPECIAL MATERIALS (Material No. 05-027) on cases, solenoids, brackets, screws and bolt heads in the APU compartment.

 **ON A/C 051-099,
 Subtask 10-12-00-620-076-B
 H. Protection of the APU
 (1)
 Do an inspection of the APU for preservation (Ref. TASK 49-20-00-200-001).

 (2)
 Do the preservation of the APU (Ref. TASK 49-20-00-600-001).

 (3)
 If necessary, apply SPECIAL MATERIALS (Material No. 05-027) on cases, solenoids, brackets, screws and bolt heads in the APU compartment.

R **ON A/C 106-149, 211-299, 301-399, 401-499,
 Subtask 10-12-00-620-076
 H. Protection of the APU
 (1)
 Do an inspection of the APU for preservation (Ref. TASK 49-20-00-210-001).

 (2)
 Do the preservation of the APU (Ref. TASK 49-20-00-600-002).

 (3)
 If necessary, apply SPECIAL MATERIALS (Material No. 05-027) on cases, solenoids, brackets, screws and bolt heads in the APU compartment.

 **ON A/C ALL
 Subtask 10-12-00-620-077
 J. External Protections of the Aircraft
 (1)
 With STORAGE PRESERVATION (Material No. 15-002) and adhesive tape:

 (a)
 Put a cover on the top of the rudder to prevent bird excrement.

 (b)
 Seal:

 -
the surge-tank overpressure

 -
the L and R ailerons to prevent bird nests

 -
the air conditioning inlets and outlets

 -
the avionics ventilation inlets and outlets

 -
the battery venturi.

 (2)
 Seal the fuel NACA air intakes and the overpressure protector outlet (trim and wing tanks) with fine nylon netting and adhesive tape.

 (3)
 Apply SPECIAL MATERIALS (Material No. 05-005) on the trailing edge of the wings.

 (4)
 Apply SPECIAL MATERIALS (Material No. 05-027):
 - on the leading edges of the nacelles and THS
 - on the refuel/defuel panel
 - on all the unpainted light-alloy areas.

 Subtask 10-12-00-210-069
 K. Visual Inspection of the Drains
 (1) Make sure that all the external structural drain holes are not clogged:
 (a)
 In the lower fuselage (Ref. TASK 53-59-00-210-001).

 (b)
 On the pylons (Ref. TASK 54-50-00-200-001).

 (c)
 On the engines.

 (d)
 In all other locations.

R EFF : ALL  10-12-00Page 219   May 01/05   CES

 Subtask 10-12-00-620-078

 L. Protection of the Cabin and the Cockpit
 (1)
 Protect with a plastic film the carpets of the cabin aisle, the cockpit and the galley areas.

 (2)
 Protect with STORAGE PRESERVATION (Material No. 15-002) all the passenger and cockpit seats

 (3)
 Open the cockpit and window shades.

 (4)
 Make sure that the sliding windows are closed.

 (5)
 Protect externally the cockpit windows with STORAGE PRESERVATION (Material No. 15-002) and adhesive tape. Do not apply adhesive tape on the windows.

R **ON A/C 001-003, 051-054,
 Subtask 10-12-00-620-079-A
 M. Protection of the Doors
 (1)
 Lubricate the external control handles of the passenger/crew doors (Ref. TASK 12-22-52-640-006).

 (2)
 Lubricate the safety pin guide-fitting and the door arming/disarming mechanism (Ref. TASK 12-22-52-640-014).

 (3)
 Lubricate the hinge-arm support-fitting bearings (Ref. TASK 12-22-52-640-016).
　
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