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2840-01-545-0114
Turbo-Shaft Aircraft Engine
2840015450114 015450114 6899400
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
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Related Documents 2840-01-545-0114 1+ Documents (More...)
Aircraft Engine 2840015450114 United States (US) 4. 2840-01-545-0114 Marketplace Restrictions Approved
Sources Datasheet Management Every Day 2840-01-545-0114 RQST Updated Every Day 2840-01-545-0114 RQST
Restrictions 2840-01-545-0114
2840-01-545-0114 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 2840-01-545-0114
- Brazil (YA01)
- Effective Date:
- 1 Oct 2006
Approved Sources 2840-01-545-0114
- Part Number
- Manufacturer
- Status
- 6899400
- Manufacturer
- 63005 - Rolls-Royce Corporation (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-545-0114
- Characteristic
- Specifications
- FIIG
- Specifications
- T197-B
- Part Name Assigned By Controlling Agency [CXCY]
- Engine Assembly, 250-C20j
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Freight Information 2840-01-545-0114
2840-01-545-0114 has freight characteristics.. 2840-01-545-0114 has a variance between NMFC and UFC when transported by rail and the description should be consulted.