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1680-01-512-0785
Push-Pull Control Assembly
1680015120785 015120785 S1239-53
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
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Restrictions 1680-01-512-0785
1680-01-512-0785 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. 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 1680-01-512-0785
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1680-01-512-0785
- Turkey (ZW01)
- Effective Date:
- 1 Aug 2003
Approved Sources 1680-01-512-0785
- Part Number
- Manufacturer
- Status
- S1239-53
- Manufacturer
- 7EK50 - Textron Aviation Inc (Active)
- Primary Buy
- Primary Buy
- S1239-53
- 71379 - Cessna Aircraft Company (Replaced)
- Original Design
- Original Design
Datasheet 1680-01-512-0785
- Characteristic
- Specifications
- FIIG
- Specifications
- A524C0
- End Item Identification [AGAV]
- 100/R182/200 Series Aircraft, Except 208
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Freight Information 1680-01-512-0785
1680-01-512-0785 has freight characteristics managed by Turkey.. 1680-01-512-0785 has a variance between NMFC and UFC when transported by rail and the description should be consulted.