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2840-01-271-8961

Turbo-Prop Aircraft Engine

2840012718961 012718961 6875452 T56-A-15LFE 6842601 T56A15 2840PL0728029

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

2840-01-271-8961 ENGINE,AIRCRAFT,TURBO-PROP 2840012718961 012718961

Managed by United States
NSN Created on 2 Feb 1988
Data Last Changed
January 2023
NATO Update Count
33
NATO Data Quality
2840-01-271-8961 ENGINE,AIRCRAFT,TURBO-PROP 2840012718961 012718961 1/1
NSN 2840-01-271-8961 (Generic Image) 1/1

2840-01-271-8961 Stock and Availability Marketplace 2840-01-271-8961

2840-01-271-8961 Related Documents Related Documents 2840-01-271-8961 5+ Documents (More...)

6875452 T56-A-15LFE 6842601 T56A15 2840PL0728029 A combustion type power unit, may be with or without
RQST NE Updated Every Day 2840-01-271-8961 RQST Updated Every Day 2840-01-271-8961 RQST NE Related
Documents 2840-01-271-8961 5+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840
Turbo-Prop Aircraft Engine 2840012718961 CharacteristicSpecificationsFIIGA23900End Item Identification
[AGAV] 2840-01-271-8961 https//www.nsnlookup.com /fsg-30/fsc-3030/us 3030-01-419-8591 Belt Prop Brake
RQST NE Restrictions https CharacteristicSpecificationsFIIGA23900End Item Identification [AGAV] 2840-01-271-8961
Every Day 5120-01-419-8596 RQST NE Restrictions https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-271-8961
Turbo-Prop Aircraft Engine 2840012718961 ENGINE,AIRCRAFT,TURBO-PROP 8 EA NS Request Quotation https
5120014198596014198596 | HMIC : N | PMIC : A | EDC: A | ADPEC : 0 5120 https//www.nsnlookup.com Aircraft Engine 2840012718961
-66/fsc-6680/us 6680-01-419-8583 Mold Repair Tool 6680014198583014198583 /fsg-28/fsc-2840/us 2840-01-271-8961
Turbo-Prop Aircraft https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-271-8961 Turbo-Prop Aircraft
Engine 2840012718961 30/fsc-3030/us 3030-01-419-8591 Belt Prop Brake https//www.nsnlookup.com /fsg-66
JavaScript in your web browser . 2840-21-869-4980Turbo-Prop Aircraft Engine2840218694980 218694980 T56A15
//www.nsnlookup.com /fsg-28/fsc-2840/ca 2840-21-869-4980 Turbo-Prop Aircraft Engine 2840218694980 T56A15
Turbo-Prop Aircraft Engine 2840012718961 Upgrade 2840-01-271-8961Turbo-Prop Aircraft Engine2840012718961

2840-01-271-8961 Demil Restrictions 2840-01-271-8961

DEMIL: C | DEMILI: 1 | CRITICALITY: X | HMIC: N | PMIC: U | EDC: | ADPEC:

2840-01-271-8961 is a Turbo-Prop Aircraft Engine that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. This item is a US Munitions List or Commerce Control List Item where key elements must be removed and destroyed to prevent this item being restored or repaired. Only authorized parties may possess this item. This item is not suspected to be hazardous. The precious metals content of this item is unknown.

2840-01-271-8961 HTS and ScheduleB Import and Export 2840-01-271-8961

2840-01-271-8961 End Users End Users 2840-01-271-8961

Poland (WP01)
Effective Date:
1 Jun 2011
Brazil (YA01)
Effective Date:
1 Jul 2001
Spain (YB01)
Effective Date:
1 Apr 1991
Malaysia (YW01)
Effective Date:
1 Sep 1993
Australia (ZA01)
Effective Date:
1 Jun 2004
Canada (ZC01)
Effective Date:
1 Apr 1991
South Africa (ZD01)
Effective Date:
1 Dec 2015
New Zealand (ZE01)
Effective Date:
1 May 2000
France (ZF01)
Effective Date:
1 Oct 2015
Republic of Korea (ZH01)
Effective Date:
1 Jun 1996
Netherlands (ZN01)
Effective Date:
1 Oct 2007
Italy (ZR01)
Effective Date:
1 Dec 2007
Norway (ZT01)
Effective Date:
1 Nov 1998
Greece (ZU01)
Effective Date:
1 May 2008
NATO Maintenance and Supply Agency (ZX01)
Effective Date:
1 Oct 2013

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2840-01-271-8961 Freight Data Freight Information 2840-01-271-8961

2840-01-271-8961 has freight characteristics managed by Canada.. 2840-01-271-8961 has a variance between NMFC and UFC when transported by rail and the description should be consulted.