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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TV501 A single or multistage assembly designed to receive thermal energy from the combustion section
RQST NE Updated Every Day 2835-14-286-0210 RQST Updated Every Day 2835-14-286-0210 RQST NE Related Documents
,TV501 TV501 A single or multistage assembly designed to receive thermal energy from the combustion section
| RNVC: 2 | DAC: 2 1 Jan 1970 2835-14-346-4774 https//www.nsnlookup.com /fsg-28/fsc-2835/fr 2835-14-286-0210
2835142860210 142860210,TV501 Engines; Non-Aircraft Prime Mover, Aircraft Non-Prime Mover, and
2835-14-346-4774 Turbine Engine Air Intake EA1M240-87RNCC: 3 | RNVC: 2 | DAC: 2 12 Dec 1977 2835-14-286-0210

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

DEMIL: | DEMILI: | CRITICALITY: | HMIC: | PMIC: | EDC: | ADPEC:

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

2835-14-286-0210 End Users End Users 2835-14-286-0210

France (ZF)

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