2840-14-530-0508
Turbine Engine Air Intake
2840145300508 145300508 S716A10A1002 N716A10A1002
An item designed to provide an optimum flow of air to the fore part of a turbine engine. Excludes AIR FLOW, NON AIRCRAFT GAS TURBINE ENGINE and BAFFLE AIR FLOW AIRCRAFT GAS TURBINE ENGINE. View more Turbine Engine Air Intake
Managed by France
NSN Created on 30 Apr 2002
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality

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Related Documents 2840-14-530-0508 1+ Documents (More...)
S716A10A1002 N716A10A1002 An item designed to provide an optimum flow of air to the fore part of a turbine
RQST NE Updated Every Day 2840-14-530-0508 RQST Updated Every Day 2840-14-530-0508 RQST NE Related Documents
2840-14-530-0508 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-530-0508
RQST NE Updated Every Day 2840-14-530-0508 RQST Updated Every Day 2840-14-530-0508 RQST NE Related Documents
2840-14-530-0508 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-530-0508
Restrictions 2840-14-530-0508
End Users 2840-14-530-0508
- France (ZF)
- Netherlands (ZN)
Approved Sources 2840-14-530-0508
- Part Number
- Manufacturer
- Status
- S716A10A1002
- Manufacturer
- F0210 - Airbus Helicopters (Ets De (Active)
- Primary Buy
- Primary Buy
- N716A10A1002
- F0210 - Airbus Helicopters (Ets De (Active)
- Canceled/Obsolete
- Canceled/Obsolete
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