2835-14-286-0210

Nonaircraft Gas Turbine Engine Turbine Rotor

2835142860210 142860210 TV501

A single or multistage assembly designed to receive thermal energy from the combustion section and convert it to mechanical energy to drive the ROTOR, COMPRESSOR, NONAIRCRAFT GAS TURBINE ENGINE and/or the ROTOR, FAN, NONAIRCRAFT GAS TURBINE ENGINE through a SHAFT, TURBINE, NONAIRCRAFT GAS TURBINE ENGINE. It consists of disks, blades, hubs, and the like. It is the moving part of a TURBINE ASSEMBLY, NONAIRCRAFT GAS TURBINE ENGINE. It has facilities for attaching to a SHAFT, TURBINE, NONAIRCRAFT GAS TURBINE ENGINE. View more Nonaircraft Gas Turbine Engine Turbine Rotor

2835-14-286-0210 ROTOR,TURBINE,NONAIRCRAFT GAS TURBINE ENGINE 2835142860210 142860210

Managed by France
NSN Created on 1 Jan 1972
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2835-14-286-0210 ROTOR,TURBINE,NONAIRCRAFT GAS TURBINE ENGINE 2835142860210 142860210 1/1
NSN 2835-14-286-0210 (Generic Image) 1/1

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2835-14-286-0210 Related Documents Related Documents 2835-14-286-0210 5+ Documents (More...)

2835-14-566-8146 2835-01-597-4230 2835-99-301-7976 https//www.nsnlookup.com /fsg-28/fsc-2835/fr 2835-14-286-0210
2835142860210 142860210,TV501 RNVC 2 DAC 2 NATO Stock Numbers Related to 2835-14-286-0210 2835-
222561297 Turbine Rotor NATO Stock Numbers Related to 2835-22-256-1297 2835-14-566-8146 2835-01-597-4230 142860210
,TV501 RNVC 2 DAC 2 NATO Stock Numbers Related to 2835-14-286-0210 2835-14-566-8146 2835-01-597-4230
Nonaircraft Gas Turbine Engine Turbine Rotor 680210009RNCC: 3 | RNVC: 2 | DAC: 6 26 Nov 1996 2835-14-286-0210
6625-01-069-6678 6625010696678 010696678 is an electronic subassembly designed to be plugged into one or more basic pieces of test equipment to extend the capabilities of the basic instrument. the basic instrument cannot function without one or more plug-in units (as required) in position.
2640-01-441-2388 2640014412388 014412388 is a metal, or metal and rubber, tubular stem containing a valve core and cap. the mounting end may have a base with a fitting designed for mounting on a pneumatic tire, inner tube, or tire rim, to permit and retain inflation or permit deflation. the mounting end may be internally threaded for adaptability to a valve spud or may be provided with cure-on or clamp in features. the other end is externally threaded to accommodate a valve cap, and internally threaded to accommodate the valve core.

2835-14-286-0210 Demil Restrictions 2835-14-286-0210

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2835-14-286-0210 is a Nonaircraft Gas Turbine Engine Turbine Rotor

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