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1680-01-421-4423
Push-Pull Control Assembly
1680014214423 014214423 3V710-1177-2
A control consisting of a wire, wire rope, or a center load rail with ball bearings, within a flexible conduit. One end must have a threaded sleeve for mounting to a wall, bulkhead, or handle, or clevis. It is used to operate or control, either manually or mechanically a mechanical device. It may include such attaching devices as nut(s), washer(s), clevis, bracket(s), and/or the like. For items designed to transmit rotary motion, see SHAFT ASSEMBLY, FLEXIBLE. View more Push-Pull Control Assembly
January 2023
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Marketplace 1680-01-421-4423
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Restrictions 1680-01-421-4423
1680-01-421-4423 is a Push-Pull Control Assembly that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. 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 1680-01-421-4423
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1680-01-421-4423
- Spain (YB01)
- Effective Date:
- 1 Nov 1995
Approved Sources 1680-01-421-4423
- Part Number
- Manufacturer
- Status
- 3V710-1177-2
- Manufacturer
- 7EK50 - Textron Aviation Inc (Active)
- Primary Buy
- Primary Buy
- 3V710-1177-2
- 70898 - Beechcraft Corporation (Replaced)
- Original Design
- Original Design
Datasheet 1680-01-421-4423
- Characteristic
- Specifications
- FIIG
- Specifications
- A524C0
- End Item Identification [AGAV]
- Beechcraft Bonanza
NATO Stock Numbers Related to 1680-01-421-4423
Freight Information 1680-01-421-4423
1680-01-421-4423 has freight characteristics.. 1680-01-421-4423 has a variance between NMFC and UFC when transported by rail and the description should be consulted.