Subtask 32-12-13-942-053
N. Removal of Equipment
(1)
Remove the GROUND LOCK SLEEVE from the applicable MLG.
(2)
Remove the warning notice(s).
(3) Remove the access platform(s). Subtask 32-12-13-865-056
P. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1GA, 2GA, 52GA.
Subtask 32-12-13-720-050
Q. Test
(1) Do a functional test of the MLG (Ref. TASK 32-31-00-720-002).
5. Close-up
________ Subtask 32-12-13-860-052
A. Aircraft Maintenance Configuration
(1)
Install the GROUND LOCK SLEEVE (460005833) on the applicable MLG (Ref. TASK 32-00-00-481-001).
(2)
Lower the aircraft off jacks (Ref. TASK 07-11-00-586-002).
(3)
Put the aircraft back to the ground configuration (Ref. TASK 32-00-00-860-002).
(4)
De-energize the aircraft electrical circuits
(Ref. TASK 24-41-00-862-002).
Subtask 32-12-13-410-050
B. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Close the MLG doors (Ref. TASK 32-12-00-410-001).
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(3) Close the NLG doors (Ref. TASK 32-22-00-410-001).
(4) Close the access panel 197CB. Subtask 32-12-13-942-054
C. Removal of Equipment
(1)
Remove the temporary wax pencil marks from the skin at the inboard edge of the secondary hinged fairing.
(2)
Make sure that the work area is clean and clear of tool(s) and other items.
(3)
Remove the safety barriers.
(4)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
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TASK 32-12-13-400-002
Installation of the Secondary Hinged Fairing (That was Removed for Access Only)
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 3 m (9 ft. 10 in.)
R No specific Torque Wrench : range 0.00 to 1.20 m.daN
R (0.00 to 9.00 lbf.ft)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 09-001 USA MIL-S-8802 TYPE I CLASS A
FUEL TANK SEALANTPOLYSULFIDE (Ref. 20-31-00)
Material No. 09-018 USA AMS 3267/3
CORROSION INHIBITING LOW ADHESION SEALANT
(Ref. 20-31-00)
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)
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C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
4 cotter pin 52-81-11 01A-010 4 cotter pin 52-81-11 01L-010 4 cotter pin 52-81-11 01M-010 8 cotter pins 52-81-11 01A-010 8 cotter pins 52-81-11 01L-010 8 cotter pins 52-81-11 01M-010
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
20-28-00-912-004 Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage and in the Wings (this does not include the tanks)-
32-00-00-481-001 Installation of the Safety Devices on the Landing Gears 32-12-13-400-001 Installation of a Replacement Secondary Hinged Fairing
**ON A/C 001-049, 051-061, 101-105, 201-203,
32-12-13-991-001 Fig. 401
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