2840-99-907-1631

Aircraft Gas Turbine Engine Outer Augmentor Nozzle Section

2840999071631 999071631 A7A/2000/471 698114-3

A rigid item designed to help direct the flow of hot gases from an AFTERBURNER,TURBINE ENGINE. It is an integral part of a NOZZLE,AUGMENTER EXHAUST,AIRCRAFT GAS TURBINE ENGINE. The item is external to the AUGMENTOR NOZZLE SECTION,CONVERGENT,AIRCRAFT GAS TURBINE ENGINE and the AUGMENTOR NOZZLE SECTION,INNER,AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Outer Augmentor Nozzle Section

2840-99-907-1631 AUGMENTOR NOZZLE SECTION,OUTER,AIRCRAFT GAS TURBINE ENGINE 2840999071631 999071631

Managed by United Kingdom
NSN Created on 16 Jun 2005
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-99-907-1631 AUGMENTOR NOZZLE SECTION,OUTER,AIRCRAFT GAS TURBINE ENGINE 2840999071631 999071631 1/1
NSN 2840-99-907-1631 (Generic Image) 1/1

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A7A/2000/471 698114-3 A rigid item designed to help direct the flow of hot gases from an AFTERBURNER
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2840999071631 999071631,A7A/2000/471 014888416 698114-3 357-1941 2840-01-616-7681 2840-01-480-1742
357-1941 2840-01-616-7681 2840-01-480-1742 2840-01-443-5863 2840-01-616-1430 2840-01-553-0698 2840-99-907-1631
2840-01-616-7681 2840-01-480-1742 2840-01-443-5863 https//www.nsnlookup.com /fsg-28/fsc-2840/uk 2840-99-907-1631
2840999071631 999071631,A7A/2000/471 2840-01-680-8111 2840016808111 016808111,4321786-02 357-1941
357-1941 2840-01-616-7681 2840-01-480-1742 2840-01-443-5863 2840-01-616-1430 2840-01-553-0698 2840-99-907-1631

2840-99-907-1631 Demil Restrictions 2840-99-907-1631

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

2840-99-907-1631 is a Aircraft Gas Turbine Engine Outer Augmentor Nozzle Section

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