2840-21-888-8938

Turbine Engine Axial-Centrifugal Compressor Rotor

2840218888938 218888938

A single or multistage assembly designed to deliver air at the proper pressure, direction and velocity. It consists of disks, blades, hubs, and the like. It is the moving part of COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It has facilities for attaching to a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Compressor Rotor

2840-21-888-8938 COMPRESSOR ROTOR,AXIAL-CENTRIFUGAL,TURBINE ENGINE 2840218888938 218888938

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Data Last Changed
January 2024
NATO Update Count
1
NATO Data Quality
2840-21-888-8938 COMPRESSOR ROTOR,AXIAL-CENTRIFUGAL,TURBINE ENGINE 2840218888938 218888938 1/1
NSN 2840-21-888-8938 (Generic Image) 1/1

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: | DEMILI : | CRITICALITY : | HMIC : | PMIC : | EDC: | ADPEC : 2840-21-888-8938 is a Turbine Engine
2840-14-493-7246 2840-14-408-3348 2840-12-360-3747 https//www.nsnlookup.com /fsg-28/fsc-2840/ca 2840-21-888-8938
2840218888938 218888938 293-3858 2840-99-103-3965 2840-14-577-8223 2840-14-399-3241 2840-14-493

2840-21-888-8938 Demil Restrictions 2840-21-888-8938

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

2840-21-888-8938 is a Turbine Engine Axial-Centrifugal Compressor Rotor

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