2840-37-512-2301

Aircraft Gas Turbine Engine Turbine Nozzle Assembly

2840375122301 375122301 85B6661-051

A 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. The assembled item forms a complete circle. View more Aircraft Gas Turbine Engine Turbine Nozzle Assembly

2840-37-512-2301 NOZZLE ASSEMBLY,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840375122301 375122301

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NSN Created on 6 Jul 2005
Data Last Changed
January 2023
NATO Update Count
1
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2840-37-512-2301 DEMIL: | DEMILI : | CRITICALITY : | HMIC : | PMIC : | EDC: | ADPEC : 2840-37-512-2301
8349 Aircraft Gas Turbine Engine Heat Shield A81061323-01RNCC: 5 | RNVC: 2 | DAC: 1 15 Sep 2011 2840-37-512-2301

2840-37-512-2301 Demil Restrictions 2840-37-512-2301

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

2840-37-512-2301 is a Aircraft Gas Turbine Engine Turbine Nozzle Assembly

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