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1680-01-506-2240
Aircraft Universal Joint Yoke
1680015062240 015062240 1650-600
A component of a universal joint designed for aircraft application. Consists of a fork-like device to accommodate the spider and bearings of universal joint by various attaching methods. The opposite end must have either a flange, hub, or splined stub shaft which is designed to be attached to a driving or driven member. For items with a shaft, the length of the plain portion must not exceed the length of the splines. See also YOKE, UNIVERSAL JOINT, NONVEHICULAR and YOKE, UNIVERSAL JOINT, VEHICULAR. View more Aircraft Universal Joint Yoke
January 2023
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Related Documents 1680-01-506-2240 5+ Documents (More...)
United States (US) 4. 1680-01-506-2240 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 1680-01-506-2240 RQST Updated Every Day 1680-01-506-2240 RQST NE Related Documents
1680-01-524-0438 1680/us 1680-01-494-7546 Aircraft Universal Joint Yoke 1680014947546 204-5833 1680-01-506-2240
1680-01-524-0438 https//www.nsnlookup.com /fsg-16/fsc-1680/us 1680-01-506-2240 Aircraft Universal
www.nsnlookup.com /fsg-16/fsc-1680/us 1680-01-670-8206 Aircraft Universal Joint Yoke 1680016708206 1680015062240
Aircraft Universal Joint Yoke 1680015062240 www.nsnlookup.com /fsg-16/fsc-1680/us 1680-01-492-6070
www.nsnlookup.com /fsg-16/fsc-1680/us 1680-01-494-7546 Aircraft Universal Joint Yoke 1680014947546 204-5833 1680-01-506-2240
1680-01-633-8111 1680-22-611-9870 1680-01-516-7133 https//www.nsnlookup.com /fsg-16/fsc-1680/us 1680-01-506-2240
Aircraft Universal Joint Yoke 1680015062240 Yoke 1680014926070 511-4026 1680-14-513-2458 1680-01
511-4026 1680-14-513-2458 1680-01-670-8206 1680-01-685-1193 1680-01-653-0205 1680-33-204-5833 1680-01-506-2240
Restrictions 1680-01-506-2240
1680-01-506-2240 is a Aircraft Universal Joint Yoke 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 1680-01-506-2240
- Schedule B
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- HTS Code
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End Users 1680-01-506-2240
- United Kingdom (ZK01)
- Effective Date:
- 1 Mar 2003
Approved Sources 1680-01-506-2240
- Part Number
- Manufacturer
- Status
- 1650-600
- Manufacturer
- 82402 - Triumph Gear Systems Inc (Active)
- Primary Buy
- Primary Buy
Datasheet 1680-01-506-2240
- Characteristic
- Specifications
- FIIG
- Specifications
- A522J0
- End Item Identification [AGAV]
- C-130 Main Landing Gear Actuator
- Part Name Assigned By Controlling Agency [CXCY]
- Fitting Yoke
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Freight Information 1680-01-506-2240
1680-01-506-2240 has freight characteristics.. 1680-01-506-2240 has a variance between NMFC and UFC when transported by rail and the description should be consulted.