Subtask 36-22-16-860-058
B. Aircraft Maintenance Configuration
(1)
Extend the slats fully (Ref. TASK 27-80-00-866-004).
(2)
Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) on the flap/slat control lever on panel 114VU.
Subtask 36-22-16-865-051
C. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 49VU AIR BLEED/ENG 1/CTL 3HA1 D12 49VU AIR BLEED/ENG 1/MONG 2HA1 D11
121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21 122VU AIR BLEED/ENG 2/CTL 3HA2 Z23 122VU AIR BLEED/ENG 2/MONG 2HA2 Z22
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Subtask 36-22-16-010-051
D. Get Access
(1)
Put the access platform in position below the applicable access panels.
(2)
Remove the applicable access panels:
-
FOR 21HF, 77HF remove 191EB, 191CT, 191BT, 521AB, 521BB, 521CB
-
FOR 37HF, 64HF remove 192EB, 192CT, 192BT, 621AB, 621BB, 621CB.
4. Procedure
_________ R (Ref. Fig. 405/TASK 36-22-16-991-005, 408/TASK 36-22-16-991-006) Subtask 36-22-16-020-051
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 (35) and the clamps (33) from the applicable cable
(40) and/or the cable (44). Retain the spacers (43).
(2)
Cut the cable-ties (42) from the cable (40) and/or the cable (40). Retain the spacers (41).
(3)
Remove the applicable cable (40) and/or the cable (44) from the electrical raceway.
(4)
Cut the electrical cable at the in-line splice connector.
(a)
For the cable 21HF:
-at the connector 4001VS in route 1S.
(b)
For the cable 37HF:
-at the connector 4000VS in route 1S.
(c)
For the cable 77HF:
-at the connector 4025VS in route 2S.
(d)
For the cable 64HF:
-at the connector 4024VS in route 2S.
(5)
Remove and discard the lockwire from the connectors (19), (23) and
(24) and the nut (20).
(6)
For the cables 21HF(37HF):
-disconnect the connector (24) from the connector (22).
(7)
For the cables 77HF(64HF):
-disconnect the connector (19) from the connector (23)
-
remove the nut (20) from the connector (23)
-
remove the connector (23) from the flanged attachment (21).
(8)
Remove the applicable cable 21HF(37HF) (40) or 77HF(64HF) (44).
(9)
Put blanking caps on the disconnected connectors.
R Cable Installation Figure 408/TASK 36-22-16-991-006
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TASK 36-22-16-400-002
Installation of the Cables 21HF(37HF),77HF(64HF)
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)
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