2840-12-195-3358

Aircraft Gas Turbine Engine Turbine Nozzle

2840121953358 121953358 JJ918580

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

2840-12-195-3358 NOZZLE,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840121953358 121953358

Managed by Germany
NSN Created on 8 Feb 1983
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-12-195-3358 NOZZLE,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840121953358 121953358 1/1
NSN 2840-12-195-3358 (Generic Image) 1/1

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JJ918580 A single stationary item designed for the purpose of directing air at the proper angle and
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2840-12-195-3358 Demil Restrictions 2840-12-195-3358

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

2840-12-195-3358 is a Aircraft Gas Turbine Engine Turbine Nozzle

2840-12-195-3358 End Users End Users 2840-12-195-3358

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United Kingdom (ZK)
Italy (ZR)

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