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2840-01-481-4354
Turbo-Prop Aircraft Engine
2840014814354 014814354 6875451
A combustion type power unit, may be with or without container, designed to use superheated air to spin a turbine rotor attached to the propeller shaft through reduction gears. View more Turbo-Prop Aircraft Engine
January 2023
7

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Restrictions 2840-01-481-4354
2840-01-481-4354 is a Turbo-Prop Aircraft Engine that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item has been confirmed as a Critical Munitions List Item or a Sensitive Commerce Control List Item and cannot be in the possession of any party anywhere in the World who is not an authorized NATO Government. Any other possessor of this item should mutilate it now as possession violates international and local laws. This item is a confirmed Commerce Control List Item (CCLI). This item is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 2840-01-481-4354
- Schedule B
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- HTS Code
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End Users 2840-01-481-4354
- Poland (WP01)
- Effective Date:
- 1 Aug 2011
- Spain (YB01)
- Effective Date:
- 1 Jan 2001
- Malaysia (YW01)
- Effective Date:
- 1 Jul 2007
- Netherlands (ZN01)
- Effective Date:
- 1 Feb 2013
Approved Sources 2840-01-481-4354
- Part Number
- Manufacturer
- Status
- 6875451
- Manufacturer
- 63005 - Rolls-Royce Corporation (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-481-4354
- Characteristic
- Specifications
- FIIG
- Specifications
- T197-B
- End Item Identification [AGAV]
- Aircraft Engine, C130 Aircraft
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Freight Information 2840-01-481-4354
2840-01-481-4354 has freight characteristics.. 2840-01-481-4354 has a variance between NMFC and UFC when transported by rail and the description should be consulted.