Part Number
Definition:
A COMPONENT OF A VANE ASSEMBLY, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. IT IS DESIGNED TO RECEIVE AIR FROM THE PRECEDING COMPRESSOR BLADES AND DELIVER IT TO THE SUCCEEDING ROW OF COMPRESSOR BLADES, DIFFUSER, OR COMBUSTION AREA AT CORRECT PRESSURE, VELOCITY AND DIRECTION.
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 |
|---|---|---|
| FEAT | SPECIAL FEATURES | ALUMINUM ALLOY,AMS 4141;11.422 IN. MIN 11.447 IN. MAX LG,9.655 IN. MIN 9.675 IN. MAX W,0.271 IN. MIN 0.278 IN. MAX DIA OF 10 HOLES,0.338 IN. MIN 0.345 IN. MAX DIA OF 2 HOLES |
| AGAV | END ITEM IDENTIFICATION | ACFT ENG TF39 |