Part Number
Definition:
A SINGLE OR MULTISTAGE ITEM DESIGNED TO RECEIVE, COMPRESS, AND DELIVER AIR TO THE COMBUSTION AREA AT A REQUIRED PRESSURE AND VELOCITY. IT CONSISTS OF A CASE (3) AND VANE ASSEMBLY, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE AND A ROTOR, COMPRESSOR, AIRCRAFT GAS 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 |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | TF33-P3/5/9 AICRAFT GAS TURBINE ENGINE |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4, FIG 17, IND 32 |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| FEAT | SPECIAL FEATURES | CONSISTS OF 150 VANES; INNER AND OUTER SHROUDS; AIR SEALING RING; STAGE 14; ONLY TO BE USED ON P3/5/9 ENGINE SERIES |
| CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME NOZZLE ASSEMBLY,TURBINE,AIRCRAFT GAS TURBINE ENGINE |