2840-15-152-0757
Turbo-Jet Engine
2840151520757 151520757 A-1044013-101
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
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Managed by  Italy
NSN Created on 3 Aug 2000
Data Last Changed 
July 2023
July 2023
NATO Update Count 
1
1
NATO Data Quality 
       

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A-1044013-101 A continuous-combustion type power unit, may be with or without container, designed to 
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2840-15-152-0757 4+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/it 2840-15-152-0757
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Turbo-Jet Engine 2840151520757 151520757 ) https//www.nsnlookup.com /fsg-28/fsc-2840/it https//
Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components from Italy (IT) Jun 2001 2840-15-152-0757
Turbo-Jet Engine 2840151520757 151520757 ) https//www.nsnlookup.com /fsg-28/fsc-2840/it https//
Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components from Italy (IT) Jun 2001 2840-15-152-0757
CRITICALITY : | HMIC : | PMIC : | EDC: | ADPEC https//www.nsnlookup.com /fsg-28/fsc-2840/it 2840-15-152-0757 
Turbo-Jet Engine 2840151520757 151520757 Components from Italy (IT) Jun 2001 2840-15-152-0757 https
Turbo-Jet Engine 2840151520757 151520757 Components from Italy (IT) Jun 2001 2840-15-152-0757 https
5 9 Oct 1996 2840-15-154-4606 Turbo-Jet Engine 2104F244RNCC: 5 | RNVC: 9 | DAC: 1 6 Jun 2001 2840-15-152-0757 
 Restrictions  2840-15-152-0757
 Approved Sources  2840-15-152-0757
- Part Number
- Manufacturer
 - Status
 - A-1044013-101
  - Manufacturer
 -  A0019 - Leonardo Spa Aircraft Division (Active) 
- Primary Buy
  - Primary Buy
 
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