2840-12-341-2978

Aircraft Gas Turbine Engine Turbine Rotor

2840123412978 123412978 VG95211-ML-123412978 JJ49790

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

2840-12-341-2978 ROTOR,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840123412978 123412978

Managed by Germany
NSN Created on 21 Aug 1996
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-12-341-2978 ROTOR,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840123412978 123412978 1/1
NSN 2840-12-341-2978 (Generic Image) 1/1

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VG95211-ML-123412978 JJ49790 A single or multistage assembly designed to receive thermal energy from
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2840-12-341-2978 Demil Restrictions 2840-12-341-2978

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

2840-12-341-2978 is a Aircraft Gas Turbine Engine Turbine Rotor

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Italy (ZR)

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