Part Number
Definition:
A CONTINUOUS COMBUSTION TYPE ENGINE. CONSISTS PRIMARILY OF A COMPRESSOR, NONAIRCRAFT GAS TURBINE ENGINE; CHAMBER, COMBUSTION, NONAIRCRAFT GAS TURBINE ENGINE AND A TURBINE ASSEMBLY, NONAIRCRAFT GAS TURBINE ENGINE. IT MAY HAVE A FAN SECTION. AIR IS COMPRESSED AND HEATED BY A COMBUSTIBLE FUEL AND EXPANDED THROUGH THE TURBINE. IT IS DESIGNED TO FURNISH A SOURCE OF ROTARY SHAFT AND/OR PNEUMATIC POWER. THE PNEUMATIC POWER IS OBTAINED BY A BLEEDOFF OF THE ENGINE COMPRESSOR. FOR A COMPLETE OPERATING POWER UNIT, MOUNTED ON A BASE, SEE POWER UNIT, GAS TURBINE ENGINE.
CAGE Information
| Code | Company |
|---|---|
| 76301 | BOEING COMPANY THE DBA BOEING |
Federal Supply Class
Title
GAS TURBINES AND JET ENGINES; NO
Inclusions:
INCLUDES AIRFLOW DEFLECTORS; COMBUSTION CHAMBERS, COMPRESSORS, TURBINES, ACCESSORY GEAR BOXES AND THEIR COMPONENTS.
Exclusions:
EXCLUDES COMPONENTS FOR GAS TURBINES AND JET ENGINES, AIRCRAFT PRIME MOVER (FSC 2840); ENGINE FUEL SYSTEMS (FSC 2910); ENGINE ELECTRICAL SYSTEMS (FSC 2920); ENGINE COOLING SYSTEMS (FSC 2930); ENGINE AIR/OIL CLEANERS/FILTERS/STRAINERS (FSC 2940); ENGINE ACCESSORIES (AIR DUCT HEATERS, ENGINE MOUNTED CONTROL ASSEMBLIES) (FSC 2990).
Characteristics (Decoded)
| MRC | Requirements Statement | Clear Text Reply |
|---|---|---|
| FUEL | FUEL TYPE | JET FUEL |
| AGAV | END ITEM IDENTIFICATION | F-15C/D ACFT |
| RDAL | REFERENCE DATA AND LITERATURE | 2JA3-50-4 |
| FEAT | SPECIAL FEATURES | ALTITUDE AT WHICH HORSEPOWER IS RATED:0.0 FT. |
| ABHP | OVERALL LENGTH | 25.340 INCHES NOMINAL |