Part Number
Definition:
A CONTINUOUS COMBUSTION TYPE ENGINE. CONSISTS PRIMARILY OF A COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE, CHAMBER, COMBUSTION, AIRCRAFT GAS TURBINE ENGINE AND A TURBINE ASSEMBLY, AIRCRAFT GAS TURBINE ENGINE. IT MAY HAVE AN AFTERBURNER, TURBINE ENGINE AND/OR 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, PNEUMATIC POWER OR THRUST 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 |
|---|---|
| 07482 | GENERAL ELECTRIC COMPANY DBA GE DIV |
Federal Supply Class
Title
GAS TURBINES AND JET ENGINES, AI
Inclusions:
INCLUDES COMPRESSOR AND TURBINE ROTORS; BLADES; COMBUSTION CHAMBER; ACCESSORY GEAR BOX; AFTERBURNER; EXHAUST CONE; RESERVOIRS, HYDRAULIC; TANK, OIL.
Exclusions:
EXCLUDES OIL, AIR, ANTI-ICING, AND HYDRAULIC REGULATORS, VALVES, AND PUMPS SPECIALLY DESIGNED FOR GAS TURBINES AND JET ENGINES (FSC 2995); CONTROL ASSEMBLIES, PUSH-PULL (FSC 2995); ENGINE MOUNTED CONTROL ASSEMBLIES (FSC 2995); FUEL SYSTEM COMPONENTS (FSC 2915); ENGINE ELECTRICAL SYSTEM COMPONENTS (FSC 2925); ENGINE COOLING SYSTEM COMPONENTS (FSC 2935); ENGINE AIR/OIL CLEANER/FILTER/STRAINERS (FSC 2945).
Characteristics (Decoded)
| MRC | Requirements Statement | Clear Text Reply |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | F101-102 ENGINE |
| FUEL | FUEL TYPE | JET FUEL |
| AAXX | MOUNTING TYPE | ANY ACCEPTABLE |
| RDAL | REFERENCE DATA AND LITERATURE | 2J-F101-4 |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| AXKD | POWER OUTPUT FOR WHICH DESIGNED | PNEUMATIC/SHAFT |