2840-12-371-7084

Aircraft Gas Turbine Engine Turbine Nozzle

2840123717084 123717084 AH30406P01

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

2840-12-371-7084 NOZZLE,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840123717084 123717084

Managed by Germany
NSN Created on 8 May 2007
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-12-371-7084 NOZZLE,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840123717084 123717084 1/1
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AH30406P01 A single stationary item designed for the purpose of directing air at the proper angle and
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2840-12-371-7084 Demil Restrictions 2840-12-371-7084

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2840-12-371-7084 is a Aircraft Gas Turbine Engine Turbine Nozzle

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Germany (ZG)

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