(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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