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1680-01-416-2618
Push-Pull Control Assembly
1680014162618 014162618 508-10313-1
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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Restrictions 1680-01-416-2618
1680-01-416-2618 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 1680-01-416-2618
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- HTS Code
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End Users 1680-01-416-2618
- Spain (YB01)
- Effective Date:
- 1 Jul 1995
- Republic of Korea (ZH01)
- Effective Date:
- 1 Jun 1999
Approved Sources 1680-01-416-2618
- Part Number
- Manufacturer
- Status
- 508-10313-1
- Manufacturer
- 82918 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Datasheet 1680-01-416-2618
- Characteristic
- Specifications
- FIIG
- Specifications
- A524C0
- End Item Identification [AGAV]
- F-4 Aircraft
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Freight Information 1680-01-416-2618
1680-01-416-2618 has freight characteristics.. 1680-01-416-2618 has a variance between NMFC and UFC when transported by rail and the description should be consulted.