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2840-01-631-5692
Turbo-Shaft Aircraft Engine
2840016315692 016315692 3066T90G02
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
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Related Documents 2840-01-631-5692 1+ Documents (More...)
Turbo-Shaft Aircraft Engine 2840016315692 United States (US) 4. 2840-01-631-5692 Marketplace Restrictions
Day 2840-01-631-5692 RQST NE Related Documents 2840-01-631-5692 DEMIL: C | DEMILI : 1 | CRITICALITY :
Restrictions 2840-01-631-5692
2840-01-631-5692 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. This item does not contain a precious metal.
End Users 2840-01-631-5692
- Republic of Korea (ZH01)
- Effective Date:
- 1 Sep 2014
Approved Sources 2840-01-631-5692
- Part Number
- Manufacturer
- Status
- 3066T90G02
- Manufacturer
- 99207 - General Electric Company (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-631-5692
- Characteristic
- Specifications
- FIIG
- Specifications
- T197-B
- Part Name Assigned By Controlling Agency [CXCY]
- Engine Assy-Ct7-8A
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Freight Information 2840-01-631-5692
2840-01-631-5692 has freight characteristics managed by the Republic of Korea.. 2840-01-631-5692 has a variance between NMFC and UFC when transported by rail and the description should be consulted.