NSN 2840-01-124-0725

Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE LOCK RING

2840-01-124-0725 A round metallic item designed to retain a NOZZLE, NOZZLE ASSEMBLY, or NOZZLE SEGMENT, TURBINE, AIRCRAFT GAS TURBINE ENGINE in a CASE AND NOZZLE ASSEMBLY, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may be a complete 360 degrees circle or a section thereof.

Alternate Parts: 777886CL7, 777886CL7, 777886CL7, 777886CL7, 777886CL7, 777886CL7, 777886CL7, 777886CL7, 2840-01-124-0725, 01-124-0725, 2840011240725, 011240725

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
28DEC 27, 198101-124-072552365 ( LOCK RING, TURBINE NOZZLE, AIRCRAFT GAS TURBINE ENGINE )
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-124-0725
Part Number Cage Code Manufacturer
777886CL74V114A-1 MACHINING
777886CL750748BOGUE EXECUTIVE ENTERPRISES INCDBA/DEXTER TOOL CO
777886CL702382EDAC TECHNOLOGIES CORPORATIONDBA GROS-IT INDUSTRIES
777886CL733617ELECTRO-METHODS INC
777886CL750381MTU AERO ENGINE COMPONENTS INC
777886CL715152TIMKEN AEROSPACE TRANSMISSIONS, LLC
777886CL752661UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY
777886CL777445UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS
Technical Data | NSN 2840-01-124-0725
Characteristic Specifications
MATERIAL STEEL
OUTSIDE DIAMETER34.878 INCHES MINIMUM AND 34.908 INCHES MAXIMUM
OVERALL THICKNESS0.143 INCHES MINIMUM AND 0.147 INCHES MAXIMUM
STAGE NUMBER3
REFERENCE DATA AND LITERATURE2J-TF33-34, FIGURE 28, INDEX 21
SPECIAL FEATURESMATL AMS 5731
CRITICALITY CODE JUSTIFICATIONAGAV
END ITEM IDENTIFICATIONACFT ENG TF33