Part Number
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.
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 | TF-33 AIRCRAFT ENGINE |
| FEAT | SPECIAL FEATURES | SURFACE TREATMENT AMS 2416, CHROMATE, MODIFIED PER PWA-S-2416; 15.199-15.201 IN. ID., 8TH STAGE |
| ABKV | OUTSIDE DIAMETER | 17.237 INCHES MINIMUM AND 17.247 INCHES MAXIMUM |
| RDAL | REFERENCE DATA AND LITERATURE | 2J-TF33-4, FIGURE 6, INDEX 47 |
| MATT | MATERIAL | STEEL |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| ABHP | OVERALL LENGTH | 2.793 INCHES MINIMUM AND 2.797 INCHES MAXIMUM |