2840-00-102-3967

Turbo-Shaft Aircraft Engine

2840001023967 001023967 1-000-080-12 T53L11C

A continuous-combustion type engine, may be with or without container, designed to use superheated air to drive a turbine rotor which is connected to the rotorshaft of a helicopter by way of reduction gears. View more Turbo-Shaft Aircraft Engine

2840-00-102-3967 ENGINE,AIRCRAFT,TURBO-SHAFT 2840001023967 001023967

Managed by United States
NSN Created on 29 May 1968
Data Last Changed
November 2023
NATO Update Count
8
NATO Data Quality
2840-00-102-3967 ENGINE,AIRCRAFT,TURBO-SHAFT 2840001023967 001023967 1/1
NSN 2840-00-102-3967 (Generic Image) 1/1

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1-000-080-12 T53L11C A continuous-combustion type engine, may be with or without container, designed
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1-000-080-12 1-000-080-13 A continuous-combustion type engine, may be with or without container, designed
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2840-00-102-3967 Demil Restrictions 2840-00-102-3967

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

2840-00-102-3967 is a Turbo-Shaft 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.

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