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2840-01-548-5411
Turbo-Shaft Aircraft Engine
2840015485411 015485411 2-001-020-25
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 2840-01-548-5411 3+ Documents (More...)
Turbo-Shaft Aircraft Engine 2840015485411 2-001-020-25 A continuous-combustion type engine, may be with
Day 2840-01-548-5411 RQST NE Restrictions 2840-01-548-5411 DEMIL: C | DEMILI : 1 | CRITICALITY : | HMIC
Turbo-Shaft Aircraft Engine 2840015485411 2840-14-555-7661 2840-00-000 https//www.nsnlookup.com
Aircraft Engine 2840012864187 286-4187 2840-43-001-2246 www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-548-5411
Restrictions 2840-01-548-5411
2840-01-548-5411 is a Turbo-Shaft Aircraft Engine 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 2840-01-548-5411
- Italy (ZR01)
- Effective Date:
- 1 Feb 2007
Approved Sources 2840-01-548-5411
- Part Number
- Manufacturer
- Status
- 2-001-020-25
- Manufacturer
- 99193 - Honeywell International Inc. (Active)
- Primary Buy
- Primary Buy
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Freight Information 2840-01-548-5411
2840-01-548-5411 has freight characteristics.. 2840-01-548-5411 has a variance between NMFC and UFC when transported by rail and the description should be consulted.