2. Job Set-up Information
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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 access platform 3 m (9 ft. 10 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 27-80-00-866-004 Extending the Slats on the Ground 27-80-00-866-005 Retracting the Slats on the Ground 24-92-00-991-006 Fig. 602 24-92-00-991-008 Fig. 604 24-92-00-991-009 Fig. 605
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3. Job Set-up
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Subtask 24-92-00-860-057
A. Aircraft Maintenance Configuration
(1) Extend the slats (Ref. TASK 27-80-00-866-004).
Subtask 24-92-00-862-053
B. De-energize the aircraft electrical circuits
(Ref. TASK 24-41-00-862-002).
Subtask 24-92-00-869-057
C. Connect the aircraft to the ground (Ref. TASK 12-34-24-869-002).
Subtask 24-92-00-010-053
D. Get Access
(1) Put the adjustable access platform in position at the wing outboard leading-edge.
(2)
For the left wing. R (a) Remove and retain the access panels: 522AB.
(3)
For the right wing. R (a) Remove and retain the access panels: 622AB.
4. Procedure
_________
Subtask 24-92-00-210-053
A. Inspection of the End Fittings of Electrical Conduits (Ref. Fig. 602/TASK 24-92-00-991-006, 604/TASK 24-92-00-991-008, 605/TASK 24-92-00-991-009)
WARNING : BE CAREFUL NOT TO CUT YOUR FINGERS. FLAKES OF NICKEL ARE SHARP.
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(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.
Electrical Harness Conduits - Corrosion Protection Figure 604/TASK 24-92-00-991-008
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INTENTIONALLY BLANK
R 1 1
24-92-00Page 613
1 1 Feb 01/99 1 1 1CES 1
Location of Conduit Fittings Figure 605/TASK 24-92-00-991-009- 12 (SHEET 1)
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Location of Conduit Fittings Figure 605/TASK 24-92-00-991-009- 22 (SHEET 2)
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(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.
5. Close-up
________
Subtask 24-92-00-410-054
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other items.
(2) For the left wing. R (a) Install the access panels: 522AB.
(3) For the right wing.
R (a) Install the access panels: 622AB. Subtask 24-92-00-860-058
B. Put the aircraft back to its initial configuration.
(1)
Disconnect the aircraft from the ground (Ref. TASK 12-34-24-869-002).
(2)
Retract the slats (Ref. TASK 27-80-00-866-005).
(3)
Remove the access platform(s).
TASK 24-92-00-210-005
Inspection of the End Fittings of Electrical Conduits in the Wing Tip
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