National Stock Number (NSN) Output Data
Definition:
A RIGID ITEM DESIGNED TO MAINTAIN A PREDETERMINED SPACE BETWEEN TWO ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. IT MAY BE A COMPLETE 360 DEGREES OR A SECTION THEREOF.
Reference/Part Number
| Part Number | CAGE | Status | RNCC | RNVC | DAC | RNAAC | MSDS | SADC |
|---|---|---|---|---|---|---|---|---|
| 714349 | 77445 | A | 5 | 9 | 4 | MF | ||
| 479352 | 77445 | A | 5 | 9 | 4 | MF | ||
| 762384 | 02403 | A | 5 | 2 | 4 | MF | ||
| 762384 | 15014 | F | 5 | 9 | 4 | MF | ||
| 762384 | 50748 | A | 5 | 2 | 4 | MF | ||
| 762384 | 50381 | A | 5 | 2 | 4 | MF | ||
| 762384 | 33617 | A | 5 | 2 | 4 | MF | ||
| 762384 | 15152 | A | 5 | 2 | 4 | MF | ||
| 714188 | 77445 | A | 5 | 9 | 2 | MF | ||
| 762384 | 4A011 | A | 5 | 2 | 4 | MF | ||
| 762384 | 77445 | A | 3 | 2 | 2 | MF | ||
| 762384 | 75877 | Y | 5 | 2 | 4 | MF |
CAGE Information
| Code | Company |
|---|---|
| 02403 | TURBINE ENGINE COMPONENTS TECHNOLOGI |
| 77445 | UNITED TECHNOLOGIES CORPORATION DBA |
| 15014 | MACHINE PRODUCTS CO INC |
| 50748 | BOGUE EXECUTIVE ENTERPRISES INC DBA/ |
| 50381 | MTU AERO ENGINE COMPONENTS INC |
| 33617 | ELECTRO-METHODS INC |
| 15152 | TIMKEN AEROSPACE TRANSMISSIONS LLC |
| 4A011 | STOWE MACHINE CO. INC. |
| 75877 | DOBSON CARTAGE AND STORAGE CO |
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 | TF-33 AIRCRAFT ENGINE |
| ABHP | OVERALL LENGTH | 3.127 INCHES MINIMUM AND 3.131 INCHES MAXIMUM |
| RDAL | REFERENCE DATA AND LITERATURE | 2J-TF33-4 |
| ABKV | OUTSIDE DIAMETER | 17.237 INCHES MINIMUM AND 17.247 INCHES MAXIMUM |
| FEAT | SPECIAL FEATURES | SURFACE TREAT,AMS 2416,CHROMATE,MODIFIED PER PWA-S-2416; 15.199-15.201 IN. ID., 6TH STAGE |
| MATT | MATERIAL | STEEL |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |