2840-21-813-1974

Aircraft Gas Turbine Engine Turbine Nozzle

2840218131974 218131974 11A00082P118

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

2840-21-813-1974 NOZZLE,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840218131974 218131974

Managed by Canada
NSN Created on 10 Mar 1967
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-21-813-1974 NOZZLE,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840218131974 218131974 1/1
NSN 2840-21-813-1974 (Generic Image) 1/1

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11A00082P118 A single stationary item designed for the purpose of directing air at the proper angle
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2840-21-813-1974 Demil Restrictions 2840-21-813-1974

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

2840-21-813-1974 is a Aircraft Gas Turbine Engine Turbine Nozzle

2840-21-813-1974 End Users End Users 2840-21-813-1974

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