-
FOR 24HF, 51HF
remove 522AB
-
FOR 40HF, 67HF
remove 622AB.
4. Procedure
_________ R (Ref. Fig. 404/TASK 36-22-16-991-004, 405/TASK 36-22-16-991-005) Subtask 36-22-16-020-052
A. Removal of the Cables CAUTION : MAKE MATCH MARKS ON ALL THE ELECTRICAL WIRES BEFORE YOU
_______ DISCONNECT THEM. INCORRECT CONNECTION OF WIRES WILL CAUSE DAMAGE TO EQUIPMENT.
(1)
Remove the bolts (32) and the clamps (31) from the cable (13) or (18).
(2)
Remove the applicable cable (13) or (18) from the electrical raceway.
(3)
Cut the applicable electrical cable (13) or (18) at the in-line splice connector.
(a)
For the cable 24HF:
-at the connector 4015VS in route 1S.
(b)
For the cable 40HF:
-at the connector 4014VS in route 1S.
(c)
For the cable 51HF:
-at the connector 4023VS in route 2S.
(d)
For the cable 67HF:
-at the connector 4022VS in route 2S.
(4)
Remove and discard the lockwire from the connectors (19), (23) and
(24) and the nut (20).
(5)
For the cable 24HF(40HF):
(a)
Disconnect the connector (19) from the connector (23).
(b)
Remove the nut (20) from the connector (23).
(c)
Remove the connector (23) from the flanged attachment (21).
(6)
For the cable 51HF(67HF):
(a) Disconnect the connector (24) from the connector (22).
(7)
Remove the applicable cable (13) or (18).
(8)
Put blanking caps on the disconnected connectors.
1EFF : ALL 1 36-22-16Page 434 1 1 May 01/05R 1 1 1CES 1
TASK 36-22-16-400-003
Installation of the Cables 24HF(40HF),51HF(67HF)
WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______ NOTICES ARE IN POSITION.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers No specific warning notice No specific access platform 2.8 m (9 ft. 2 in.) No specific Torque Wrench : range 0.00 to 1.20 m.daN
(0.00 to 9.00 lbf.ft) 98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific NSA936809RG0001 Material No. 11-026 GB DEF-STAN 68-148/1 SOLVENT GENERAL PURPOSE (Ref. 20-31-00) Material No. 19-003 USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
Material No. 19-010 USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
1EFF : ALL 1 36-22-16Page 435 1 1 Aug 01/05R 1 1 1CES 1
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
27-80-00-866-004 Extending the Slats on the Ground 27-80-00-866-005 Retracting the Slats on the Ground 36-22-00-710-001 Operational Test of the Overheat Detection System
R ESPM 204312 36-22-16-991-004 Fig. 404 36-22-16-991-005 Fig. 405
3. Job Set-up
__________
Subtask 36-22-16-941-059
A. Safety Precautions
(1)
Make sure that the safety barriers are in position.
(2)
Make sure that the warning notice is in position in the cockpit to tell persons not to operate the slat controls.
Subtask 36-22-16-860-069
B. Aircraft Maintenance Configuration
(1)
Make sure that the slats are fully extended (Ref. TASK 27-80-00-866-004).
(2)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) is installed on the flap/slat control lever on panel 114VU.
(3)
Make sure that the access platform is in position below the applicable access panels.
(4)
Make sure that the applicable access panels are removed:
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