NSN 2840-00-883-5965

Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR BLADE LOCK

2840-00-883-5965 An item used to maintain the position of a BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE in the proper place on a DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE. This item eliminates axial movement of the blade.

Alternate Parts: 715049, 715049, 715049, 715049, 715049, 715049, 715049, 715049, 715049, 2840-00-883-5965, 00-883-5965, 2840008835965, 008835965

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
28MAY 05, 197200-883-596550458 ( LOCK, TURBINE ROTOR BLADE, AIRCRAFT GAS TURBINE ENGINE )
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-883-5965
Part Number Cage Code Manufacturer
71504954850AMBEL PRECISION MANUFACTURINGCORPORATION
71504981753CONNECTICUT SPRING & STAMPINGCORPORATION THE
71504933617ELECTRO-METHODS INC
71504905813KREISLER INDUSTRIAL CORPORATIONDBA KREISLER INDUSTRIAL
71504931340THE BIRKEN MANUFACTURING COMPANY
71504915152TIMKEN AEROSPACE TRANSMISSIONS, LLC
71504951992UNION MACHINE COMPANY OF LYNN, INC.
71504952661UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY
71504977445UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS
Technical Data | NSN 2840-00-883-5965
Characteristic Specifications
MATERIAL STEEL CORROSION RESISTING
MATERIAL DOCUMENT AND CLASSIFICATIONAMS5517 ASSN STD SINGLE MATERIAL RESPONSE
HARDNESS RATING63.0 ROCKWELL A MINIMUM AND 68.0 ROCKWELL A MAXIMUM
STAGE NUMBER8
OVERALL WIDTH0.264 INCHES MINIMUM AND 0.294 INCHES MAXIMUM
OVERALL LENGTH1.315 INCHES MINIMUM AND 1.365 INCHES MAXIMUM
REFERENCE DATA AND LITERATURE2J-TF33-4
SPECIAL FEATURESGOES ON THE COMPRESSOR ROTOR-FRONT
END ITEM IDENTIFICATIONTF-33 AIRCRAFT ENGINE