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
Managed by United Kingdom
NSN Created on 16 Jun 2005
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality

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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
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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
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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
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
Restrictions 2840-99-907-1631
Approved Sources 2840-99-907-1631
- Part Number
- Manufacturer
- Status
- A7A/2000/471
- Manufacturer
- KE154 - Ministry Of Defence, Hercules (Active)
- Source Control
- Source Control
- 698114-3
- 98897 - Lockheed Martin Corp (Active)
- Primary Buy
- Primary Buy