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1680-01-648-1796
Aircraft Universal Joint Companion Flange
1680016481796 016481796 25CT489-1
An item designed for aircraft application having a flange on one end with provisions for a shaft on the other end. Designed to mate with the flange of a YOKE, UNIVERSAL JOINT for the purpose of transmitting rotory motion. View more Aircraft Universal Joint Companion Flange
January 2023
4
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United States (US) 4. 1680-01-648-1796 Marketplace Restrictions Approved Sources Datasheet Management
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Restrictions 1680-01-648-1796
1680-01-648-1796 is a Aircraft Universal Joint Companion Flange 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 considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 1680-01-648-1796
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1680-01-648-1796
- Republic of Korea (ZH01)
- Effective Date:
- 1 Sep 2015
Approved Sources 1680-01-648-1796
- Part Number
- Manufacturer
- Status
- 25CT489-1
- Manufacturer
- 7EK50 - Textron Aviation Inc (Active)
- Primary Buy
- Primary Buy
- 25CT489-1
- 70898 - Beechcraft Corporation (Replaced)
- Original Design
- Original Design
Datasheet 1680-01-648-1796
- Characteristic
- Specifications
- FIIG
- Specifications
- A521S0
- End Item Identification [AGAV]
- Hawker 800Xp 850Xp
- Part Name Assigned By Controlling Agency [CXCY]
- Flange
NATO Stock Numbers Related to 1680-01-648-1796
Freight Information 1680-01-648-1796
1680-01-648-1796 has freight characteristics managed by the Republic of Korea.. 1680-01-648-1796 has a variance between NMFC and UFC when transported by rail and the description should be consulted.