TM 55-2840-254-23
Type Oil . . . . . . . . . . . . . . . . . . . . . . . . . . . MIL-L-23699 or MIL-L-7808
Rotational Directions
Compressor Rotor . . . . . . . . . . . Counterclockwise
First Turbine Rotor Disc . . . . . . . Counterclockwise
Second Turbine Rotor Disc . . . . Counterclockwise
Output Shaft . . . . . . . . . . . . . . . . Clockwise
Power Turbine Shaft . . . . . . . . . Clockwise
Third Turbine Rotor Disc . . . . . Clockwise
Fourth Turbine Rotor Disc . . . . . Clockwise
CAPABILITIES AND FEATURES
Combustion Chamber . . . . . . . . . . . . . . . External Annular
Compressor Ratio . . . . . . . . . . . . . . . . . 8 to 1
Horsepower (Military) . . . . . . . . . . . . . . . 3750
Maximum Altitude . . . . . . . . . . . . . . . . . . 25,000 Feet
Change 10
