(4)
 Remove the drip pan from beneath the oil cooler.

 (5)
 Set the LIGHT control switch 11LJ to the off position.

 (6)
 Close the APU access doors 315AL, 316AR (Ref. TASK 52-41-00-410-001).

 (7)
 Remove the access platform(s). Subtask 49-91-44-865-067

 B.
 Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1KD, 2KD

 Subtask 49-91-44-860-054
 C. Aircraft Maintenance Configuration
 (1)
 Pressurize the reservoirs of the hydraulic systems.
 (Ref. TASK 29-14-00-614-002).

 (2)
 De-energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-862-002).

 (3)
 Remove the warning notice(s).

 PUMPS - OIL ((GTCP 36-300)) - MAINTENANCE PRACTICES
___________________________________________________ R **ON A/C 001-003, 051-099, 401-499,
 TASK 49-91-45-200-002 Remove and discard Lube Filter Element (GTCP 36-300) WARNING : DO NOT TOUCH THE APU UNTIL IT IS SUFFICIENTLY COOL TO PREVENT BURNS
_______ WHEN YOU DO THE MAINTENANCE TASK(S).
 WARNING : CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK. LOOSE
_______ LOCKWIRE CAN CUT OR BLIND YOU.
 WARNING : DO NOT LET OIL STAY ON YOUR SKIN FOR A LONG TIME AS IT CAN CAUSE
_______ INJURY.
 1.
 Reason for the Job

__________________
 Refer to the MPD TASK: 499141-01

 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 notice
 No specific container 10 l (2.6416 USgal)
 No specific access platform 3.5 m (11 ft. 6 in.)

 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 03-002  GB DEF-STAN 91-101 LUBRICATING OIL TURBINE ENGINE SYNT BASE (Ref. 20-31-00)
 Material No. 19-010  USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)  C. Expendable Parts

 -------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
1  O-ring  49-91-45 01 -035
 1  O-ring  49-91-45 01A-035
 2  filter element  49-91-45 01 -030
 2  filter element  49-91-45 01A-030
 3  O-ring  49-91-45 01 -020
 3  O-ring  49-91-45 01A-020
 D. Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-23-51-000-001  Removal of the APU Generator 8XS
 24-23-51-400-001  Installation of the APU Generator 8XS
 24-41-00-861-002  Energize the Aircraft Electrical Circuits from the
 External Power
 24-42-00-862-001  De-energize the Ground Service Network Supplied from
 the External Power
 29-00-00-864-001  Put the Related Hydraulic System in the Depressurized
 Configuration before Maintenance Action
 29-14-00-614-002  Pressurization of the Hydraulic Reservoirs through
 the Ground Connector
 49-00-00-860-003  APU Start by External Power (GTCP 36-300)
 49-00-00-860-004  APU Shutdown by External Power (GTCP 36-300)
 49-11-00-000-002  Removal of the Generator Substitution Kit (GTCP
 36-300)
 49-11-00-400-002  Installation of the Generator Substitution Kit
 (Flight without Generator) (GTCP 36-300)
 49-11-11-000-001  Removal of the Auxiliary Power Unit (APU) - 4005KM
 (GTCP 36-300)
 49-11-11-400-001  Installation of the Auxiliary Power Unit (APU) -
4005KM (GTCP 36-300)
 49-90-00-600-001  Check Oil Level and Replenish (GTCP 36-300)
 49-91-41-200-001  Remove and discard Alternator Scavenge Filter Element
 (8069KM) (GTCP 36-300)
 52-41-00-010-001  Open the APU Doors for Access
 52-41-00-410-001  Close the APU Doors after Access
 49-91-45-991-002  Fig. 201 
　
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