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 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific airless spray No specific brush No specific dental No specific lint-free cloth No specific seal tools No specific adjustable platform 7 m (22 ft. 12 in.)
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-004  USA MIL-T-81533 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM) (Ref. 20-31-00)
 Material No. 15-008  AIB TN 10138 TYPE II GRADE 2 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
 C. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-34-24-869-002 Aircraft Grounding for the Maintenance Operations 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
 from the External Power 24-92-00-991-006 Fig. 602 24-92-00-991-016 Fig. 612 24-92-00-991-017 Fig. 613
 3. Job Set-up
__________
 Subtask 24-92-00-862-057
 A. De-energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-862-002).

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 B. Connect the aircraft to ground (Ref. TASK 12-34-24-869-002). Subtask 24-92-00-010-057
 C. Get Access
 (1)
 Put the adjustable platform in position at the vertical stabilizer trailing-edge.

 (2)
 For the left vertical stabilizer trailing-edge.

 (a) Remove and retain the access panels: 325CL, 325DL.

 (3)
 For the right vertical stabilizer trailing-edge.

 (a) Remove and retain the access panels 325BL, 325BR.
 4. Procedure
_________ Subtask 24-92-00-210-057
 A. Inspection of the End Fittings of Electrical Conduits (Ref. Fig. 602/TASK 24-92-00-991-006, 612/TASK 24-92-00-991-016, 613/TASK 24-92-00-991-017)
 WARNING : BE CAREFUL NOT TO CUT YOUR FINGERS. FLAKES OF NICKEL ARE SHARP.
_______
 (1) At each fitting use the procedure that follows to protect against corrosion:
 (a)
 Use CLEANING AGENTS (Material No. 11-004) and a lint-free cloth to remove any contamination from the fitting.

 (b)
 Remove any flakes or blisters, make sure that the you do not damage the base metal while you do this task.

 NOTE : A dental or a seal tools are recommended for the removal
____
 of flakes and blisters.

 (c) Use a brush or an airless spray to apply a continuous coat of STORAGE PRESERVATION (Material No. 15-008) with a thickness of
 0.030 mm (0.001 in.), to cover all the fitting.
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 Electrical Harness Conduits - Corrosion Protection Figure 612/TASK 24-92-00-991-016 
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 Location of Conduit Fittings Figure 613/TASK 24-92-00-991-017 
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 5. Close-up
________ Subtask 24-92-00-410-058
 A. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 For the left vertical stabilizer trailing-edge.

 (a) Install the access panels: 325CL, 325DL.

 (3)
 For the right vertical stabilizer trailing-edge.

 (a) Install the access panels: 325BL, 325BR.

 (4)
 Disconnect the aircraft from ground (Ref. TASK 12-34-24-869-002).

 (5)
 Remove the access platform(s).

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 Inspection of the End Fittings of Electrical Conduits in the Fuselage Tail Area
 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
 WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______ START A TASK ON OR NEAR:
 -
THE FLIGHT CONTROLS

 -
THE FLIGHT CONTROL SURFACES

 -
THE LANDING GEAR AND THE RELATED DOORS

 -COMPONENTS THAT MOVE.
 WARNING : MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND THE CAUTIONS INCLUDED IN
_______ THE REFERENCED PROCEDURES.
　
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