2840-14-511-4421
Turbo-Shaft Aircraft Engine
2840145114421 145114421 250C20F 2840AA8016001
A continuous-combustion type engine, may be with or without container, designed to use superheated air to drive a turbine rotor which is connected to the rotorshaft of a helicopter by way of reduction gears. View more Turbo-Shaft Aircraft Engine
Managed by France
NSN Created on 16 Dec 1998
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
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Related Documents 2840-14-511-4421 1+ Documents (More...)
250C20F 2840AA8016001 A continuous-combustion type engine, may be with or without container, designed
RQST NE Updated Every Day 2840-14-511-4421 RQST Updated Every Day 2840-14-511-4421 RQST NE Related Documents
2840-14-511-4421 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-511-4421
RQST NE Updated Every Day 2840-14-511-4421 RQST Updated Every Day 2840-14-511-4421 RQST NE Related Documents
2840-14-511-4421 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-511-4421
Restrictions 2840-14-511-4421
End Users 2840-14-511-4421
- Brazil (YA)
- France (ZF)
Approved Sources 2840-14-511-4421
- Part Number
- Manufacturer
- Status
- 250C20F
- Manufacturer
- 83873 - Essex Group Inc (Obsolete)
- Canceled/Obsolete
- Canceled/Obsolete
- 2840AA8016001
- F3033 - Direction Centrale Du Materiel De (Active)
- NATO Reference
- NATO Reference
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