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 |
|---|---|
| 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 |
|---|---|---|
| ABHP | OVERALL LENGTH | 2.230 INCHES MINIMUM AND 2.232 INCHES MAXIMUM |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| CZCJ | STAGE NUMBER | 13 |
| MATT | MATERIAL | STEEL CORROSION RESISTING VANE |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | COMPRESSOR STSTOR-13 STAGE,ASSY OF |
| FEAT | SPECIAL FEATURES | 19.320-19.330 IN. ID,SAME AS P/N 704273 EXCEPT OMIT ALL COATING AND RELATED DATA |
| ABMZ | DIAMETER | 27.720 INCHES MINIMUM AND 27.740 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | TF33 AIRCRAFT ENGINE |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| RDAL | REFERENCE DATA AND LITERATURE | T.O.2J-TF33-4, FIG. 17, IND 25 |
| CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |