2840-21-890-1914
Aircraft Gas Turbine Engine Turbine Nozzle
2840218901914 218901914
A single stationary item designed for the purpose of directing air at the proper angle and velocity to a ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It has provisions for attaching to a CASE (3), TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may have an inner support shroud. View more Aircraft Gas Turbine Engine Turbine Nozzle
Managed by Canada
Data Last Changed
January 2024
January 2024
NATO Update Count
1
1
NATO Data Quality
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