(3)
 If the angle joint (4) is not in safety:

 -loosen the locknuts (14) and (15),
 -remove the angle joint (4) from the support (5) and turn it until it is in safety,
 -turn the swivel end assembly (13) until you can connect the angle joint (4) to the support (5),
 -TORQUE the locknut (14) to 0.3 m.daN (26.54 lbf.in).
 -
make sure that the angle joint (4) is in safety,

 -
make sure that the inner cable of the cable assembly (2) is between the inspection holes of the swivel end assembly (13)

 -TORQUE the locknut (15) to 0.6 m.daN (53.09 lbf.in).

 (4)
 Connect the angle joint (4) to the support (5) and install the washer

 (8) and the nut (7).
 (5) Safety the nut (7): FOR 32-12-15 01-001 R - with a new cotter pin (6)
 FOR 32-12-15 02-001 R - with a new cotter pin (6).
 (6) Safety the nut (14)
 WARNING : WEAR GOGGLES WHEN YOU REMOVE OR INSTALL THE LOCKWIRE. CUT,
_______ REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU.
 (a) Safety the locknut (14) with corrosion-resistant steel lockwire
 0.8 mm (0.032 in.) dia.
 1EFF : ALL 1 32-12-15Page 409 1 1 Nov 01/98 1 1 1CES 1

 (7) Remove the rigging pin from the bypass valve 2517GM (2518GM). Subtask 32-12-15-865-054
 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1GA, 2GA, 52GA, 1701GK, 1702GK.
 Subtask 32-12-15-941-053
 D. Preparation for Test
 (1)
 Energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-861-002)

 (2)
 Move the applicable MLG door control-handle to the open position.

 (3)
 Connect the PTU isolation coupling (Ref. TASK 29-23-00-860-002).

 (4)
 If the flight configuration precautions were obeyed, put the aircraft back to the serviceable condition (Ref. TASK 32-00-00-860-002).

 (5)
 Remove the warning notice(s).

 (6) Remove the access platform(s). Subtask 32-12-15-720-050
 E. Functional Test
 (1)
 Close the applicable MLG door (Ref. TASK 32-12-00-410-001). Make sure that the MLG door control-handle can move freely and is clear of the aircraft structure.

 (2)
 Open the applicable MLG door (Ref. TASK 32-12-00-010-001). Make sure that the MLG door control-handle can move freely and is clear of the aircraft structure.

 1EFF : ALL 1 32-12-15Page 410 1 1 Feb 01/98 1 1 1CES 1

 5. Close-up
________ Subtask 32-12-15-410-051
 A. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Close the applicable MLG door (Ref. TASK 32-12-00-410-001).

 (3)
 Close the access panel 195BB (196BB).

 1EFF : ALL 1 32-12-15Page 411 1 1 Feb 01/98 1 1 1CES 1 CONTROL CABLE - MLG DOOR GROUND OPENING (2804GM,2805GM) - REMOVAL/INSTALLATION

______________________________________________________________________________ TASK 32-12-16-000-001 Removal of the Control Cable 2804GM (2805GM) WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE
_______ YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.
 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.
 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s) No specific warning notices No specific access platform 2 m (6 ft. 7 in.) 460005835 1 GROUND LOCK SLEEVE 98DNSA20208040 1 RIGGING PIN
 1EFF : ALL 1 32-12-16Page 401 1 1 Feb 01/98 1 1 1CES 1 B. Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the
 External Power 29-10-00-863-001 Pressurize the Green Hydraulic System 29-10-00-864-001 Depressurize the Green Hydraulic System 29-23-00-860-001 Disconnection of the Isolation Coupling of the Power
　
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