2840-15-207-3224

Turbo-Prop Aircraft Engine

2840152073224 152073224 856A2650G13 (241)AA262856A2650G13

A combustion type power unit, may be with or without container, designed to use superheated air to spin a turbine rotor attached to the propeller shaft through reduction gears. View more Turbo-Prop Aircraft Engine

2840-15-207-3224 ENGINE,AIRCRAFT,TURBO-PROP 2840152073224 152073224

Managed by Italy
NSN Created on 8 Oct 2012
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-15-207-3224 ENGINE,AIRCRAFT,TURBO-PROP 2840152073224 152073224 1/1
NSN 2840-15-207-3224 (Generic Image) 1/1

2840-15-207-3224 Stock and Availability Marketplace 2840-15-207-3224

Need Help?
Request a Quotation from participating marketplace vendors
eBay Updated Every Day
2840-15-207-3224 RQST NE eBay
eBay Updated Every Day
2840-15-207-3224 RQST eBay
Amazon Updated Every Day
2840-15-207-3224 RQST NE Amazon

2840-15-207-3224 Related Documents Related Documents 2840-15-207-3224 2+ Documents (More...)

856A2650G13 (241)AA262856A2650G13 A combustion type power unit, may be with or without container, designed
2840-15-207-3224 2+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/it 2840-15-207-3224
Turbo-Prop Aircraft Engine 2840152073224 856A2650G13 (241)AA262856A2650G13 A combustion type power unit
enable JavaScript in your web browser . 5120-15-004-7275Multiengine Trim Ba5120150047275 150047275 856A2650G13
www.nsnlookup.com /fsg-51/fsc-5120/it 5120-15-004-7275 https//www.nsnlookup.com /fsg-28/fsc-2840/it 2840-15-207-3224
Turbo-Prop Aircraft Engine 2840152073224 JavaScript in your web browser . 2840-15-207-3224Turbo-Prop

2840-15-207-3224 Demil Restrictions 2840-15-207-3224

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

2840-15-207-3224 is a Turbo-Prop Aircraft Engine

2840-15-207-3224 End Users End Users 2840-15-207-3224

Italy (ZR)

2840-15-207-3224 Similar Items Similar Supply Items to 2840-15-207-3224