Part Number
Definition:
A HOUSING DESIGNED TO SURROUND, RETAIN, SUPPORT, AND PROTECT AN ANTIFRICTION BEARING MOUNTED ON A SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. IT MAY ALSO ACT AS A SUMP TO COLLECT THE LUBRICANT TO BE PUMPED BACK TO THE TANK.
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 |
|---|---|---|
| FEAT | SPECIAL FEATURES | MFG'D OF STEEL,AMS 6322; 0.572 - 0.586 IN. LG.,0.513 - 0.525 BODY LG.,2.284 - 2.285 IN. BODY OD,2.165 - 2.165 IN. BODY ID,0.060 - 0.060 IN. INTERNAL FLANGE THK,1.930 - 1.950 IN. INTERNAL FLANGE ID,0.453 - 0.455 IN. DISTANCE FROM INTERNAL FLANGE TO EXTERNAL FLANGE,3.535 - 3.555 IN. EXTERNAL FLANGE OD,0.059 - 0.061 IN. EXTERNAL FLANGE THK; ROCKWELL C26-32 HARDNESS,THREE 0.276 - 0.266 IN. DIA. HOLES EQUALLY SPACED ON EXTERNAL FLANGE ON 1.533 IN. CENTERLINE RADIUS |
| AGAV | END ITEM IDENTIFICATION | AIRCRAFT JDET ENGINE,TF30 |