Quantcast Table 1-2.  Equipment Data

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ARMY TM 9-2815-257-24 AIR FORCE TO 38G1-128-2 MARINE CORPS TM 10155A/2815-24/3 1-7 d.    Engine cooling is provided by a flywheel fan (12) connected to the crankshaft (10).  The fan forces air over the cylinder fins and engine components.  The fan is completely guarded by a cover to prevent inadvertent contact during operation. 1-13.   EQUIPMENT DATA. Refer to Table 1-2, Equipment Data, for a summary of specific capabilities, limitations, and critical data for maintenance of the engine assembly. Table 1-2.  Equipment Data WEIGHTS AND DIMENSIONS Weight   86.0 pounds (39.0 kilograms) Length   15.08 inches (38.3 centimeters) Width    16.58 inches (42.1 centimeters) Height   17.72 inches (45.0 centimeters) GENERAL SPECIFICATIONS Horsepower 6.7 horsepower (at 3600 rpm) Operating RPM 3000 to 3600 RPM Engine cooling system Forced air cooling Oil requirements: MIL-L-46167, OEA -25 F to +40 F (-31 C to +5 C) MIL-L-2104, OE/HDO-15/40 +5 F to +120 F (-15 C to +49 C) MIL-L-2104, OE/HDO-10 -15 F to +40 F (-26 C to +5 C) MIL-L-2104, OE/HDO-30 +15 F to +90 F (-9 C to +32 C) MIL-L-2104, OE/HDO-40 +30 F to +120 F (-1 C to +49 C) Oil capacity: Engine 1.2 quarts (1.1 liters) Oil consumption rate (at rated load) 0.04 ounces (1.18 milliliters) per hour   Compression ratio 19.5 Bore x stroke 3.07 x 2.44 inches (78 x 62 millimeters) Cylinder One Displacement 18.1 in3 (296 cm3)


 


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