2840-20-006-9213

Turbo-Jet Engine

2840200069213 200069213 3042000 JT15D-5A

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

2840-20-006-9213 ENGINE,TURBO-JET 2840200069213 200069213

Managed by Canada
NSN Created on 29 May 2012
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-20-006-9213 ENGINE,TURBO-JET 2840200069213 200069213 1/1
NSN 2840-20-006-9213 (Generic Image) 1/1

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3042000 JT15D-5A A continuous-combustion type power unit, may be with or without container, designed
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X | HMIC : N | PMIC : A | EDC: | ADPEC : 0 2915 https//www.nsnlookup.com /fsg-28/fsc-2840/ca 2840-20-006-9213
Turbo-Jet Engine 2840200069213 200069213 CharacteristicSpecificationsFIIGA23900End Item Identification
[AGAV]Jt15d-5A https//www.nsnlookup.com /fsg-29/fsc-2915/us 2915-01-604-0210 Turbine Engine Main Fuel
Every Day 2915-01-504-3593 RQST NE Restrictions https//www.nsnlookup.com /fsg-28/fsc-2840/ca 2840-20-006-9213
Turbo-Jet Engine 2840200069213 200069213 CharacteristicSpecificationsFIIGA23900End Item Identification
[AGAV]Jt15d-5A https//www.nsnlookup.com /fsg-29/fsc-2915/us 2915-01-504-3593 Fuel Pressurizing And Drain
| HMIC : N | PMIC : A | EDC: A | ADPEC : 0 2840 https//www.nsnlookup.com /fsg-28/fsc-2840/ca 2840-20-006-9213
Turbo-Jet Engine 2840200069213 200069213 CharacteristicSpecificationsFIIGA23900End Item Identification
[AGAV]Jt15d-5A https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-504-3594 Turbine Engine Bleed Valve

2840-20-006-9213 Demil Restrictions 2840-20-006-9213

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2840-20-006-9213 is a Turbo-Jet Engine

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