Premium Information is available for this item - Upgrade for $1 a day
2840-01-653-4274
Turbo-Shaft Aircraft Engine
2840016534274 016534274 CT7-8F5
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
January 2023
4
Marketplace 2840-01-653-4274
Request a Quotation from participating marketplace vendors
Related Documents 2840-01-653-4274 1+ Documents (More...)
Turbo-Shaft Aircraft Engine 2840016534274 United States (US) 4. 2840-01-653-4274 Marketplace Restrictions
Day 2840-01-653-4274 RQST NE Restrictions 2840-01-653-4274 DEMIL: C | DEMILI : 1 | CRITICALITY : X |
Restrictions 2840-01-653-4274
2840-01-653-4274 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 2840-01-653-4274
- Spain (YB01)
- Effective Date:
- 1 Mar 2016
Approved Sources 2840-01-653-4274
- Part Number
- Manufacturer
- Status
- CT7-8F5
- Manufacturer
- 99207 - General Electric Company (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-653-4274
- Characteristic
- Specifications
- FIIG
- Specifications
- T197-B
- End Item Identification [AGAV]
- 72-00-00 Engine Assy
- Special Features [FEAT]
- Description: Engine Assy-Ct7-8F5; Part Of: 72-00-00 Engine Assy
NATO Stock Numbers Related to 2840-01-653-4274
Freight Information 2840-01-653-4274
2840-01-653-4274 has freight characteristics.. 2840-01-653-4274 has a variance between NMFC and UFC when transported by rail and the description should be consulted.