2840-21-841-6185

Aircraft Gas Turbine Engine Turbine Nozzle

2840218416185 218416185

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

2840-21-841-6185 NOZZLE,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840218416185 218416185

Managed by Canada
Data Last Changed
January 2024
NATO Update Count
1
NATO Data Quality
2840-21-841-6185 NOZZLE,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840218416185 218416185 1/1
NSN 2840-21-841-6185 (Generic Image) 1/1

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2840-21-841-6185 Demil Restrictions 2840-21-841-6185

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

2840-21-841-6185 is a Aircraft Gas Turbine Engine Turbine Nozzle

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