
ARMY TM 9-2815-254-24
AIR FORCE TO 38G1-94-2
SECTION II. EQUIPMENT DESCRIPTION AND DATA
1 - 7 . G E N E R A L .
The diesel engine (FIGURE 1-1) is four cylinder, four cycle, fuel injected, naturally-aspirated, and liquid-cooled.
The firing order is 1-3-4-2. The number one cylinder is toward the fan end of the engine. The serial number is found
on left side of the cylinder body at number one cylinder location. Rotation of engine is counterclockwise as viewed
from flywheel.
NOTE
All locations referenced herein are given facing the flywheel end (rear)
of the engine.
1-8.
DETAILED DESCRIPTION.
1-8.1.
Cooling System. The cooling system consists of a radiator, water pump, cooling fan, thermostat, and connecting
hoses. The fan is mounted on shaft of water pump and both are belt driven from the crankshaft pulley. The thermo-
stat controls engine temperature and is installed in the top of engine. The function of the cooling system is to main-
tain a specific operating temperature of 180° to 203°F (82° to 95°C) for the engine.
1-8.2.
Lubrication System. The lubrication system consists of the oil pan, a gerotor type oil pump, spin-on type oil filter,
and internal passages within the engine. There are two external oil lines, one for rocker arm lubrication and one
for fuel injector pump lubrication.
1-8.3.
Fuel System. The function of the fuel system is to inject a metered quantity of clean atomized fuel into the engine
cylinders at a precise time near the end of the compression stroke of each piston. The fuel system consists of
the fuel tank, fuel filter/water separator, fuel injection pump, and the fuel injectors. The fuel tank and fuel filter/wa-
ter separator are not mounted on engine. The injection pump is mounted on the front cover and is driven by the
timing gears.
1-8.4.
Electrical System. The electrical system is 24 VDC operation and consists of an alternator, starter, externally
mounted batter and other items as required. The alternator is mounted on front of engine and is belt driven.
When the engine is operating, the alternator supplies 24 VDC to recharge the battery and maintain it at a full state
of charge. The starter is mounted on the flywheel housing and when energized engages the ring gear of the fly-
wheel to rotate the engine.
1-3
Summary of Contents for C-240PW-28
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Page 46: ...ARMY TM 9 2815 254 24 AIR FORCE TO 38G1 94 2 FIGURE 3 2 Water Pump 3 20...
Page 49: ...ARMY TM 9 2815 254 24 AIR FORCE TO 38G1 94 2 FIGURE 3 3 Fuel Filter Assembly 3 23...
Page 52: ...ARMY TM 9 2815 254 24 AIR FORCE TO 38G1 94 2 FIGURE 3 4 Fuel lnjectors and Piping 3 26...
Page 60: ...ARMY TM 9 2815 254 24 AIR FORCE TO 38G1 94 2 FIGURE 3 7 Fuel Feed Pump and Timer Assembly 3 34...
Page 61: ...ARMY TM 9 2815 254 24 AIR FORCE TO 38G1 94 2 FIGURE 3 8 Fuel Injection Pump Assembly 3 35...
Page 82: ...ARMY TM 9 2815 254 24 AlR FORCE TO 36G1 94 2 TABLE 3 1 Fuel Pump Test Specifications 3 56...
Page 98: ...ARMY TM 9 2815 254 24 AIR FORCE TO 38G1 94 2 FIGURE 3 39 Oil Piping 3 72...
Page 106: ...ARMY TM 9 2815 254 24 AIR FORCE TO 38G1 94 2 FIGURE 3 44 PCV Assembly 3 80 Change 2...
Page 109: ...ARMY TM 9 2815 254 24 AIR FORCE TO 38G1 94 2 FIGURE 3 45 Intake and Exhaust Manifolds 3 83...
Page 122: ...ARMY TM 9 2815 264 24 AIR FORCE TO 38G1 94 2 FIGURE 3 49 Alternator Assembly 3 96 Change 2...
Page 126: ...ARMY TM 9 2815 254 24 AIR FORCE TO 38G1 94 2 FIGURE 3 50 Front Gear Cover 3 100...
Page 129: ...ARMY TM 9 2815 254 24 AIR FORCE TO 38G1 94 2 FIGURE 3 52 Rocker Covet and Arms 3 103...
Page 137: ...ARMY TM 9 2815 254 24 AIR FORCE TO 38G1 94 2 FIGURE 3 60 Cylinder Head Assembly 3 111...
Page 185: ...ARMY TM 9 2815 254 24 AIR FORCE TO 38G1 94 2 FIGURE 3 107 Flywheel and Housing 3 159...
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Page 216: ...ARMY TM 9 2815 254 24 AIR FORCE TO 38G1 94 2 Section 111 MAINTENANCE LEVELTD PARAGRAPHS...
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Page 234: ...PIN 071752 002...