Part Number
Definition:
(ALL EXCEPT USA) FOR USA INC 61835 CANCELED REPLACED BY HUB, ROTOR, GAS TURBINE ENGINE: INC 40961, FIIG A107, APPL KEY G. A COMPONENT OF A TURBINE ROTOR. IT IS DESIGNED TO ATTACH TO THE FRONT AND/OR REAR OF THE TURBINE ROTOR PROVIDING SUPPORT, ALIGNMENT, AND A MEANS OF ATTACHMENT FOR A SHAFT. IT MAY HAVE PROVISIONS FOR INSTALLING BEARINGS, AND/OR OIL, AND AIR SEALS. SEE ALSO DISK AND HUB, TURBINE, TURBINE ENGINE.
CAGE Information
| Code | Company |
|---|---|
| 77445 | UNITED TECHNOLOGIES CORPORATION DBA |
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 |
|---|---|---|
| TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | NICKEL ALLOY,4.882 IN. MIN,4.895 IN. MAX LG O/A |
| TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | NICKEL ALLOY,4.882 IN. MIN,4.895 IN. MAX LG O/A |