2840-12-195-2266

Aircraft Gas Turbine Engine Turbine Nozzle

2840121952266 121952266 JJ918042

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

2840-12-195-2266 NOZZLE,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840121952266 121952266

Managed by Germany
NSN Created on 27 Jan 1983
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-12-195-2266 NOZZLE,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840121952266 121952266 1/1
NSN 2840-12-195-2266 (Generic Image) 1/1

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2840-12-195-2266 Related Documents Related Documents 2840-12-195-2266 5+ Documents (More...)

JJ918042 A single stationary item designed for the purpose of directing air at the proper angle and
RQST NE Updated Every Day 2840-12-195-2266 RQST Updated Every Day 2840-12-195-2266 RQST NE Related Documents
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2840-12-195-2266 Demil Restrictions 2840-12-195-2266

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

2840-12-195-2266 is a Aircraft Gas Turbine Engine Turbine Nozzle

2840-12-195-2266 End Users End Users 2840-12-195-2266

Germany (ZG)
Italy (ZR)

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