National Stock Number (NSN) Output Data
Definition:
A SINGLE OR MULTISTAGE ASSEMBLY DESIGNED TO DELIVER AIR AT THE PROPER PRESSURE, DIRECTION AND VELOCITY. IT CONSISTS OF DISKS, BLADES, HUBS, AND THE LIKE. IT IS THE MOVING PART OF COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. IT HAS FACILITIES FOR ATTACHING TO A SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
Reference/Part Number
| Part Number | CAGE | Status | RNCC | RNVC | DAC | RNAAC | MSDS | SADC |
|---|---|---|---|---|---|---|---|---|
| 6009T42P05 | 99207 | A | 3 | 2 | 2 | MB |
CAGE Information
| Code | Company |
|---|---|
| 99207 | GENERAL ELECTRIC COMPANY DBA GE DIV |
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 |
|---|---|---|
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ROTOR SPOOL,REAR-COMPRESSOR |
| APGF | DESIGN TYPE | AXIAL-CENTRIFUGAL |
| ABMZ | DIAMETER | 13.064 INCHES MINIMUM AND 13.072 INCHES MAXIMUM |
| ABHP | OVERALL LENGTH | 5.895 INCHES MINIMUM AND 5.899 INCHES MAXIMUM |
| FEAT | SPECIAL FEATURES | ORIGINAL NAME SPOOL,AXIAL COMPRESSOR,TURBINE ENGINE |
| AGAV | END ITEM IDENTIFICATION | ACFT ENG J85 |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |