NSN 2840-00-869-1447

Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE LOCK RING

2840-00-869-1447 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: 777886CL5, 777886CL5, 777886CL5, 777886CL5, 777886CL5, 777886CL5, 777886CL5, 777886CL5, 777886CL5, 2840-00-869-1447, 00-869-1447, 2840008691447, 008691447

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
28JAN 01, 196000-869-144752365 ( LOCK RING, TURBINE NOZZLE, AIRCRAFT GAS TURBINE ENGINE )
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-869-1447
Part Number Cage Code Manufacturer
777886CL54V114A-1 MACHINING
777886CL550748BOGUE EXECUTIVE ENTERPRISES INCDBA/DEXTER TOOL CO
777886CL502382EDAC TECHNOLOGIES CORPORATIONDBA GROS-IT INDUSTRIES
777886CL533617ELECTRO-METHODS INC
777886CL515014MACHINE PRODUCTS CO INC
777886CL550381MTU AERO ENGINE COMPONENTS INC
777886CL515152TIMKEN AEROSPACE TRANSMISSIONS, LLC
777886CL552661UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY
777886CL577445UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS
Technical Data | NSN 2840-00-869-1447
Characteristic Specifications
MATERIAL STEEL
OUTSIDE DIAMETER34.878 INCHES MINIMUM AND 34.908 INCHES MAXIMUM
OVERALL THICKNESS0.135 INCHES MINIMUM AND 0.139 INCHES MAXIMUM
STAGE NUMBER3
REFERENCE DATA AND LITERATURE2J-TF33-34, FIGURE 28, INDEX 21
SPECIAL FEATURESMATL SPEC AMS 5731
CRITICALITY CODE JUSTIFICATIONAGAV
END ITEM IDENTIFICATIONACFT ENG TF33