2840-14-435-9899

Aircraft Gas Turbine Engine Turbine Rotor

2840144359899 144359899 078-01-202

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

2840-14-435-9899 ROTOR,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840144359899 144359899

Managed by France
NSN Created on 29 Nov 1989
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-14-435-9899 ROTOR,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840144359899 144359899 1/1
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2840-14-435-9899 Related Documents Related Documents 2840-14-435-9899 2+ Documents (More...)

Outillage 007-02M1RNCC: 3 | RNVC: 2 | DAC: 1007-02-0M1RNCC: 5 | RNVC: 2 | DAC: 1 1 Jan 1972 2840-14-435-9899

2840-14-435-9899 Demil Restrictions 2840-14-435-9899

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

2840-14-435-9899 is a Aircraft Gas Turbine Engine Turbine Rotor

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