2840-14-510-1411

Turbo-Jet Engine

2840145101411 145101411 ECU102 SEC ECU102 2840AA8011367

A continuous-combustion type power unit, may be with or without container, designed to exert thrust. It's prime physical characteristics include air compressor(s), combustion chamber(s) and gas turbine. The operating principle is as follows: atmospheric air is inducted into the unit at its front, compressed, heated by combustion of a fuel, expanded through the gas turbine, and ejected at high velocity. It may incorporate features to vary direction of the thrust. View more Turbo-Jet Engine

2840-14-510-1411 ENGINE,TURBO-JET 2840145101411 145101411

Managed by France
NSN Created on 4 Nov 1998
Data Last Changed
July 2023
NATO Update Count
1
NATO Data Quality
2840-14-510-1411 ENGINE,TURBO-JET 2840145101411 145101411 1/1
NSN 2840-14-510-1411 (Generic Image) 1/1

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2840-14-510-1411 Related Documents Related Documents 2840-14-510-1411 4+ Documents (More...)

https//www.nsnlookup.com
/fsg-28/fsc-2840/ro
2840-39-000-0738 Turbo-Jet Engine 2840390000738 390000738
Documents 2840-39-000-0738 3+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-510-1411
Turbo-Jet Engine 2840145101411 145101411 6 Feb 1997 2840-14-510-1411 Turbo-Jet Engine ECU102 SECRNCC
https//www.nsnlookup.com /nato/nato-stock-numbers/inc Turbo-Jet Engine (INC 02007) 6 Feb 1997 2840-14-510-1411
https//www.nsnlookup.com
/fsg-28/fsc-2840/fr
2840-14-437-3871 Access Cover 2840144373871 144373871
Turbines and Jet Engines, Aircraft, Prime Moving; and Components from France (FR) 6 Feb 1997 2840-14-510-1411
Turbo-Jet Engine ECU102 SECRNCC: 3 | RNVC: 2 | DAC: 6 4 Nov 1998 2840-14-437-3871 Restrictions
https//www.nsnlookup.com
/nato/nato-stock-numbers/inc
Turbo-Jet Engine (INC 02007)
Feb 2002 2840-14-485-6918 Turbo-Jet Engine 304-840-002-0RNCC: 3 | RNVC: 2 | DAC: 4 6 Feb 1997 2840-14-510-1411
Turbo-Jet Engine ECU102 SECRNCC: 3 | RNVC: 2 | DAC: 6 4 Nov 1998 2840-39-000-0738 Turbo-Jet Engine
https//www.nsnlookup.com
/fsg-28/fsc-2840
Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components from France (FR)
Dec 2004 2840-14-485-6918 Turbo-Jet Engine 304-840-002-0RNCC: 3 | RNVC: 2 | DAC: 4 6 Feb 1997 2840-14-510-1411
Turbo-Jet Engine ECU102 SECRNCC: 3 | RNVC: 2 | DAC: 6 4 Nov 1998 2840-14-437-3871 Access Cover

2840-14-510-1411 Demil Restrictions 2840-14-510-1411

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

2840-14-510-1411 is a Turbo-Jet Engine

2840-14-510-1411 End Users End Users 2840-14-510-1411

France (ZF)

2840-14-510-1411 Manufacturers Approved Sources 2840-14-510-1411

Part Number
Manufacturer
Status
ECU102 SEC
F0228 - Safran Helicopter Engines (Active)
Primary Buy
RNCC 3 RNVC 2 DAC 6
ECU102
F0228 - Safran Helicopter Engines (Active)
Primary Buy
RNCC 3 RNVC 2 DAC 6
2840AA8011367
F3033 - Direction Centrale Du Materiel De (Active)
NATO Reference
RNCC 6 RNVC 9 DAC 9

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