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2840-01-567-3682
Aircraft Gas Turbine Engine Compressor Disk
2840015673682 015673682 3075839-1
An item having provisions on the outer periphery for attaching a designated number of BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It also has provisions for attachment to a HUB, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE and/or a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Compressor Disk
June 2023
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Restrictions 2840-01-567-3682
2840-01-567-3682 is a Aircraft Gas Turbine Engine Compressor Disk 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 Non-Critical Munitions List Item or a Non-Sensitive Commerce Control List Item and cannnot be in the possession of any party outside of the USA who is a 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 2840-01-567-3682
- Schedule B
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- HTS Code
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End Users 2840-01-567-3682
- Spain (YB01)
- Effective Date:
- 1 Sep 2010
- Belgium (ZB01)
- Effective Date:
- 1 Sep 2008
- Republic of Korea (ZH01)
- Effective Date:
- 1 Jun 2009
- Portugal (ZP01)
- Effective Date:
- 1 Nov 2015
Approved Sources 2840-01-567-3682
- Part Number
- Manufacturer
- Status
- 3075839-1
- Manufacturer
- 99193 - Honeywell International Inc. (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-567-3682
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- End Item Identification [AGAV]
- Aircraft, Falcon 20, Engine Tfe731
- Part Name Assigned By Controlling Agency [CXCY]
- Disk Lpg Rotor 2Stg
NATO Stock Numbers Related to 2840-01-567-3682
Freight Information 2840-01-567-3682
2840-01-567-3682 has freight characteristics.. 2840-01-567-3682 has a variance between NMFC and UFC when transported by rail and the description should be consulted.