2840-21-896-1512

Aircraft Gas Turbine Engine Turbine Nozzle

2840218961512 218961512 12A00318G04

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

2840-21-896-1512 NOZZLE,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840218961512 218961512

Managed by Canada
NSN Created on 15 Jan 1985
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-21-896-1512 NOZZLE,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840218961512 218961512 1/1
NSN 2840-21-896-1512 (Generic Image) 1/1

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12A00318G04 A single stationary item designed for the purpose of directing air at the proper angle and
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2840-21-896-1512 Demil Restrictions 2840-21-896-1512

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

2840-21-896-1512 is a Aircraft Gas Turbine Engine Turbine Nozzle

2840-21-896-1512 End Users End Users 2840-21-896-1512

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