2840-99-491-1280

Aircraft Gas Turbine Engine Turbine Rotor

2840994911280 994911280 GP11550A GP11550A ISSUE 10 36VV-26934

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

2840-99-491-1280 ROTOR,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840994911280 994911280

Managed by United Kingdom
NSN Created on 6 Jul 2001
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-99-491-1280 ROTOR,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840994911280 994911280 1/1
NSN 2840-99-491-1280 (Generic Image) 1/1

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GP11550A GP11550A ISSUE 10 36VV-26934 A single or multistage assembly designed to receive thermal energy
2840-99-491-1280 2+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/uk 2840-99-491-1280
RQST NE Updated Every Day 2840-99-491-1280 RQST Updated Every Day 2840-99-491-1280 RQST NE Restrictions
2390Cable Assembly6615002072390 002072390 26934 https//www.nsnlookup.com /fsg-28/fsc-2840/uk 2840-99-491-1280
Aircraft Gas Turbine Engine Turbine Rotor 1280Aircraft Gas Turbine Engine Turbine Rotor2840994911280 994911280
GP11550A GP11550A ISSUE 10 36VV-26934 fsc-2840/uk 2840-99-491-1280 Aircraft Gas Turbine Engine Turbine

2840-99-491-1280 Demil Restrictions 2840-99-491-1280

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

2840-99-491-1280 is a Aircraft Gas Turbine Engine Turbine Rotor

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