2840-12-195-2267

Aircraft Gas Turbine Engine Turbine Nozzle

2840121952267 121952267 JJ918569

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

2840-12-195-2267 NOZZLE,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840121952267 121952267

Managed by Germany
NSN Created on 27 Jan 1983
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-12-195-2267 NOZZLE,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840121952267 121952267 1/1
NSN 2840-12-195-2267 (Generic Image) 1/1

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JJ918569 A single stationary item designed for the purpose of directing air at the proper angle and
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2840-12-195-2267 Demil Restrictions 2840-12-195-2267

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

2840-12-195-2267 is a Aircraft Gas Turbine Engine Turbine Nozzle

2840-12-195-2267 End Users End Users 2840-12-195-2267

Germany (ZG)
United Kingdom (ZK)
Italy (ZR)

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