2840-21-887-5190
Turbine Engine Axial-Centrifugal Compressor Rotor
2840218875190 218875190
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
Managed by Canada
Data Last Changed
January 2024
January 2024
NATO Update Count
1
1
NATO Data Quality
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Request a Quotation from participating marketplace vendors Request Restrictions 2840-21-887-5190 DEMIL
: | DEMILI : | CRITICALITY : | HMIC : | PMIC : | EDC: | ADPEC : 2840-21-887-5190 is a Turbine Engine
Request a Quotation from participating marketplace vendors Request Restrictions 2840-21-887-5190 DEMIL
: | DEMILI : | CRITICALITY : | HMIC : | PMIC : | EDC: | ADPEC : 2840-21-887-5190 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 2840-21-887-5190
2840218875190 218875190 293-3858 2840-99-103-3965 2840-14-577-8223 2840-14-399-3241 2840-14-493
2840218875190 218875190 293-3858 2840-99-103-3965 2840-14-577-8223 2840-14-399-3241 2840-14-493
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