5670-01-155-3187 FRAME,OBSERVATION WINDOW Index 4730-01-155-3189 STRAINER BODY,SEDIMENT

National Stock Number:
2835-01-155-3188

Federal Supply Class:
2835

National Item Identification Number:
011553188

Description:
SHAFT,TURBINE,NONAIRCRAFT GAS TU

Detail:
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.


Manufacturer Information:
72305945153HAMILTON SUNDSTRAND CORPORATION
72305955820RTX CORPORATION
72305958163MEGGITT (NORTH HOLLYWOOD), INC.
72305999167HAMILTON SUNDSTRAND CORPORATION


Techincal Specification:
HARDNESS RATING35.0 ROCKWELL C MINIMUM AND 42.0 ROCKWELL C MAXIMUM OVERALL
OVERALL LENGTH4.969 INCHES NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATIONAMS 5643 ASSN STD SINGLE MATERIAL RESPONSE AND MIL-H-6875 MIL SPEC SINGLE MATERIAL RESPONSE OVERALL
MATERIALSTEEL CORROSION RESISTING OVERALL
SPECIAL FEATURESALL 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


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