National Stock Number (NSN) Output Data
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.
Reference/Part Number
| Part Number | CAGE | Status | RNCC | RNVC | DAC | RNAAC | MSDS | SADC |
|---|---|---|---|---|---|---|---|---|
| 765574 | 77445 | A | 3 | 2 | 2 | MF |
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 |
|---|---|---|
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-34, FIG 14, IND 23 |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME COMPRESSOR,AXIAL,TURBINE ENGINE |
| AGAV | END ITEM IDENTIFICATION | TF33-P102/A/B/P103 AIRCRAFT GAS TURBINE ENGINE |
| ABMZ | DIAMETER | 27.720 INCHES MINIMUM AND 27.740 INCHES MAXIMUM |
| FEAT | SPECIAL FEATURES | STAGE 14; TO BE USED ONLY ON P102/A/B/P103 ENGINE SERIES; SUPERSEDES P/N 389471, 446074, 534384, 612794, 555894, 703174, 744894 |
| CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
| CRTL | CRITICALITY CODE JUSTIFICATION | ABMZ AND CZBJ AND FEAT |