Part Number
Definition:
AN ITEM DESIGNED TO TRANSFER ROTARY MOTION FROM A ROTOR, TURBINE, NONAIRCRAFT GAS TURBINE ENGINE TO A ROTOR, COMPRESSOR, NONAIRCRAFT GAS TURBINE ENGINE AND/OR A ROTOR, FAN, NONAIRCRAFT GAS TURBINE ENGINE. IT MAY INCLUDE THE HUB, TURBINE, NONAIRCRAFT GAS TURBINE ENGINE. IT MAY INCLUDE PROVISIONS FOR MOUNTING BEARINGS AND/OR SEALS.
CAGE Information
Code | Company |
---|---|
45153 | HAMILTON SUNDSTRAND CORPORATION DIV |
Federal Supply Class
Title
GAS TURBINES AND JET ENGINES; NO
Inclusions:
INCLUDES AIRFLOW DEFLECTORS; COMBUSTION CHAMBERS, COMPRESSORS, TURBINES, ACCESSORY GEAR BOXES AND THEIR COMPONENTS.
Exclusions:
EXCLUDES COMPONENTS FOR GAS TURBINES AND JET ENGINES, AIRCRAFT PRIME MOVER (FSC 2840); ENGINE FUEL SYSTEMS (FSC 2910); ENGINE ELECTRICAL SYSTEMS (FSC 2920); ENGINE COOLING SYSTEMS (FSC 2930); ENGINE AIR/OIL CLEANERS/FILTERS/STRAINERS (FSC 2940); ENGINE ACCESSORIES (AIR DUCT HEATERS, ENGINE MOUNTED CONTROL ASSEMBLIES) (FSC 2990).
Characteristics (Decoded)
MRC | Requirements Statement | Clear Text Reply |
---|---|---|
AGAV | END ITEM IDENTIFICATION | 2350-01-061-2445 |
MATT | MATERIAL | STEEL CORROSION RESISTING OVERALL |
FEAT | SPECIAL FEATURES | ALL CHARACTERISTICS DATA PROPRIETARY; SURFACE FINISH 16.0 MICROINCH ON PLAIN END; 32.0 MICROINCH INTERNAL; 250.0 MICROINCH EXTERNAL; EXTERNAL FLANGE ON RIGHT END; 0.938 IN. DIA; 0.125 IN. THICK; 4 SHOULDERS 2 UNDERCUTS BETWEEN ENDS; SMALLEST DIA 0.625 IN.; LARGEST DIA 0.6692 MIN 0.6695 MAX IN.; ONE 0.664-32UNS 3A THREADED SHOULDER; FLAT KEYWAY LOCATED ON SHOULDER BEHIND FLANGE; 0.791 IN. LG; 0.1895 MIN 0.1915 MAX IN. W; 0.0822 MIN 0.0875 MAX IN. DEPTH; INTERNAL FLAT ROOT; SIDE FIT; INVOLUTE SPLINE DATA: 11 TEETH; 0.3438 IN. PITCH DIA; 0.5 IN. PITCH FRACTION; 0.2977 IN. BASE CIRCLE DIA; 30 DEG PRESSURE ANGLE; 0.375 IN. MIN FORM DIA; 0.045 IN. WIRE SIZE; 0.2955 IN. MAX LG BETWEEN 2 WIRES; 0.001 IN. MAX PROFILE VARIATION; 0.0003 IN. MAX LEAD VARIATION; ARMY COGNIZANT SERVICE |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS 5643 ASSN STD SINGLE MATERIAL RESPONSE OVERALL AND MIL-H-6875 MIL SPEC SINGLE MATERIAL RESPONSE OVERALL |
CQFM | HARDNESS RATING | 35.0 ROCKWELL C MINIMUM OVERALL AND 42.0 ROCKWELL C MAXIMUM OVERALL |
ABHP | OVERALL LENGTH | 4.969 INCHES NOMINAL |