2840-21-850-1468

Aircraft Gas Turbine Engine Turbine Rotor

2840218501468 218501468 11A00090G06 11A00090G006

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, AIRCRAFT GAS TURBINE ENGINE and/or the ROTOR, FAN, AIRCRAFT GAS TURBINE ENGINE through a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It consists of disks, blades, hubs, and the like. It is the moving part of a TURBINE ASSEMBLY, AIRCRAFT GAS TURBINE ENGINE. It has facilities for attaching to a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Turbine Rotor

2840-21-850-1468 ROTOR,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840218501468 218501468

Managed by Canada
NSN Created on 2 Aug 1968
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-21-850-1468 ROTOR,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840218501468 218501468 1/1
NSN 2840-21-850-1468 (Generic Image) 1/1

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11A00090G06 11A00090G006 A single or multistage assembly designed to receive thermal energy from the
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2840-21-850-1468 Demil Restrictions 2840-21-850-1468

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

2840-21-850-1468 is a Aircraft Gas Turbine Engine Turbine Rotor

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