2840-21-887-5211
Aircraft Gas Turbine Engine Compressor Vane
2840218875211 218875211
A component of a VANE ASSEMBLY, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It is designed to receive air from the preceding compressor blades and deliver it to the succeeding row of compressor blades, diffuser, or combustion area at correct pressure, velocity and direction. View more Aircraft Gas Turbine Engine Compressor Vane
Managed by Canada
Data Last Changed
January 2024
January 2024
NATO Update Count
1
1
NATO Data Quality
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Related Documents 2840-21-887-5211 5+ Documents (More...)
Restrictions 2840-21-887-5211 DEMIL: | DEMILI : | CRITICALITY : | HMIC : | PMIC : | EDC: | ADPEC
Aircraft Gas Turbine Engine Compressor Vane Documents 2840-21-887-5211 4+ Documents ( More... )
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Aircraft Gas Turbine Engine Compressor Vane Documents 2840-21-887-5211 4+ Documents ( More... )
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Aircraft Gas Turbine Engine Compressor Vane Documents 2840-21-887-5211 4+ Documents ( More... )
and Components (FSC 2840) Compressor Vane 2840-21-806-2079 Moving; and Components (FSC 2840) 2840-21-887-5211
Aircraft Gas Turbine Engine Compressor Vane Documents 2840-21-887-5211 4+ Documents ( More... )
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Modification Kit 2840-21-844-2434 and Components from https//www.nsnlookup.com /fsg-28/fsc-2840/ca 2840-21-887-5211
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Turbine Engine Turbine Rotor Blade 2840-21-887-5057 Aircraft Gas Turbine Engine Compressor Blade 2840-21-887-5211
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