2840-21-845-8612

Aircraft Gas Turbine Engine Turbine Nozzle

2840218458612 218458612

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

2840-21-845-8612 NOZZLE,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840218458612 218458612

Managed by Canada
Data Last Changed
January 2024
NATO Update Count
1
NATO Data Quality
2840-21-845-8612 NOZZLE,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840218458612 218458612 1/1
NSN 2840-21-845-8612 (Generic Image) 1/1

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2840-21-845-8612 Related Documents Related Documents 2840-21-845-8612 5+ Documents (More...)

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2840-21-845-8612 Demil Restrictions 2840-21-845-8612

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

2840-21-845-8612 is a Aircraft Gas Turbine Engine Turbine Nozzle

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