Part Number
Definition:
A SINGLE OR MULTISTAGE ASSEMBLY DESIGNED TO RECEIVE THERMAL ENERGY FROM THE COMBUSTION SECTION AND CONVERT IT TO MECHANICAL ENERGY TO DRIVE THE ROTOR, COMPRESSOR, NONAIRCRAFT GAS TURBINE ENGINE AND/OR THE ROTOR, FAN, NONAIRCRAFT GAS TURBINE ENGINE THROUGH A SHAFT, TURBINE, NONAIRCRAFT GAS TURBINE ENGINE. IT CONSISTS OF DISKS, BLADES, HUBS, AND THE LIKE. IT IS THE MOVING PART OF A TURBINE ASSEMBLY, NONAIRCRAFT GAS TURBINE ENGINE. IT HAS FACILITIES FOR ATTACHING TO A SHAFT, TURBINE, NONAIRCRAFT GAS TURBINE ENGINE.
CAGE Information
| Code | Company |
|---|---|
| 12773 | HOWMET CORPORATION DBA LA PORTE CAST |
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 |
|---|---|---|
| FEAT | SPECIAL FEATURES | ROTOR DIAMETER IS 13.692MIN TO 13.696 MAX HIGH |
| AGAV | END ITEM IDENTIFICATION | 2350-01-087-1095,TANK M1A1 |