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Flight Safety Critical Aricraft Parts (FSCAP) Program (cont)
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TM-55-2840-254-23-1 Engine Gas Turbine Model T55-L-712 Manual
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CAPABILITIES AND FEATURES

TM 55-2840-254-23
Thermocouple, lmmers
2-310-086-01
Thermocouple, lmmers
2-310-087-01
Thermocouple, lmmers
2-310-088-01
Section II. EQUIPMENT DESCRIPTION AND DATA
Engine characteristics, capabilities, and features are as follows:
CHARACTERISTICS
Manufacturer . . . . . . . . . . . . . . . . . . . . . . ALLIED SIGNAL
Phoenix, AZ
Model . . . . . . . . . . . . . . . . . . . . . . . . . . . . . T55-L-712
Type . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Free power turbine, two stage
Dimensions
Overall Length . . . . . . . . . . . . . . 48.53 inches
Nominal Diameter . . . . . . . . . . . . 28.72 inches
Weight (Dry) . . . . . . . . . . . . . . . . . . . . . . . 750 Pounds (Approximate)
Type Fuel . . . . . . . . . . . . . . . . . . . . . . . . . MIL-T-5624 (Grade JP-4,
Alternate JP-5 or JP-8)
Change 10
1-4.4

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