2840-14-534-6899
Turbine Engine Bleed Valve
2840145346899 145346899 T214A10T0006 34119001
An item which is a component of a turbine engine with multistage compressors and which reduces and neutralizes the pressure surges resulting from differing operating conditions thus preventing surging. View more Turbine Engine Bleed Valve
Managed by France
NSN Created on 2 Apr 2003
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 2840-14-534-6899
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Related Documents 2840-14-534-6899 1+ Documents (More...)
T214A10T0006 34119001 An item which is a component of a turbine engine with multistage compressors and
RQST NE Updated Every Day 2840-14-534-6899 RQST Updated Every Day 2840-14-534-6899 RQST NE Related Documents
2840-14-534-6899 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-534-6899
RQST NE Updated Every Day 2840-14-534-6899 RQST Updated Every Day 2840-14-534-6899 RQST NE Related Documents
2840-14-534-6899 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-534-6899
Restrictions 2840-14-534-6899
End Users 2840-14-534-6899
- Spain (YB)
- Australia (ZA)
- France (ZF)
- Germany (ZG)
Approved Sources 2840-14-534-6899
- Part Number
- Manufacturer
- Status
- T214A10T0006
- Manufacturer
- F0210 - Airbus Helicopters (Ets De (Active)
- Source Control
- Source Control
- 34119001
- FA3W9 - Safran Aerosystems Ex Safran (Active)
- Primary Buy
- Primary Buy
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