(2)
 Oil reservoir capacity 6,3 l (1,64 US G) approx.

 (3)
 Oil consumption - should not exceed 90 cc per operating hour.

 E. Electrical System:
 (1)
 Power supply (aircraft bus) or,

 (2)
 Battery 28.6 +/- 2 V DC.

 F. Bleed-Air Control System
 (1)
 Inlet Guide-Vane Actuator - Nonoperating - Closed.

 (2)
 Bleed Control Valve - Nonoperating - Exhaust position.

 ENGINE ((GTCP 36-300)) - SERVICING
__________________________________

R **ON A/C 001-003, 051-099, 401-499,
 TASK 49-20-00-600-001
 Preservation / Storage / De-preservation of the Engine (GTCP 36-300)
 WARNING : MAKE SURE THAT YOU HAVE THE CORRECT FIRE FIGHTING EQUIPMENT
_______
 AVAILABLE.

 WARNING : DO NOT TOUCH THE APU UNTIL IT IS SUFFICIENTLY COOL TO PREVENT BURNS
_______
 WHEN YOU DO THE MAINTENANCE TASK(S).

 1. Reason for the Job
__________________

 The preservation procedure of the APU is carried out to prevent internal and
 external corrosion and deterioration when the APU is not in service.
 The preservation procedure will give the maximum protection and must be
 carried out in clean and dry conditions.
 Storage times and procedures are given in Table 301.

 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific blanking caps
 No specific circuit breaker(s) safety clip(s)
 No specific desiccant (silica gel)
 No specific humidity indicator
 No specific protective covers
 No specific warning notice
 No specific warning tag (S8145-26A)
 No specific water-vapor proof bag
 No specific access platform 3.5 m (11 ft. 6 in.)
 No specific container 5 l (1.3208 USgal)
 3862619-1 1 COVER - ASSEMBLY, APU GEN

 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 03-008 USA MIL-L-6081 GRADE 1010 OR GRADE 1005
 OIL (FUEL CONTROL PRESERVATION) (Ref. 20-31-00) Material No. 11-002 USA MIL-PRF-680
 DRY CLEANING SOLVENT (VARSOL/WHITE SPIRIT)
 (Ref. 20-31-00)
 C. 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
 24-41-00-862-002  De-energize the Aircraft Electrical Circuits Supplied
 from the External Power
 28-22-00-710-001  Operational Test of the APU Fuel-Pump System on
 Ground to Purge the Fuel Line
 49-00-00-710-004  Operational Test of the APU (4005KM) (GTCP 36-300)
 49-11-11-000-001  Removal of the Auxiliary Power Unit (APU) - 4005KM
 (GTCP 36-300)
 49-31-41-000-001  Removal of the Primary Fuel Nozzle and Manifold
 (8020KM) (GTCP 36-300)
 49-31-41-400-001  Installation of the Primary Fuel Nozzle and Manifold
 (8020KM) (GTCP 36-300)
 49-32-11-000-001  Removal of the Fuel Control Unit (FCU) (8022KM) (GTCP
 36-300)
 49-32-11-210-001  Inspection of the Fuel-Filter Differential-Pressure
 Indicator (GTCP 36-300)
 49-32-11-400-001  Installation of the Fuel Control Unit (FCU) (8022KM)
 (GTCP 36-300)
 49-32-12-000-001  Removal of the Flow Divider and Drain Valve Assembly
 (8023KM) (GTCP 36-300)
 49-32-12-400-001  Installation of the Flow Divider and Drain Valve
 Assembly (8023KM) (GTCP 36-300)
 49-41-38-000-001  Removal of the Ignition Unit (8030KM) (GTCP 36-300)
 49-41-38-400-001  Installation of the Ignition Unit (8030KM) (GTCP
 36-300)
 49-90-00-600-001  Check Oil Level and Replenish (GTCP 36-300) 
　
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