Premium Information is available for this item - Upgrade for $1 a day
1680-01-564-4114
Remote Control Lever
1680015644114 015644114 936843-101
A rigid item usually in the form of an arm of various shapes and cross sections, containing two or more holes so spaced that one serves as a pivot with or without hubs and must have a definite means for securing to a shaft (such as threaded hole for set-screw, keyway(s), splines, serrations or some clamping device). The other hole(s) connect(s) to CONNECTING LINK, RIGID; WIRE ROPE ASSEMBLY, SINGLE LEG; or CLEVIS, ROD END; to provide transmission of movement to other parts of the mechanism. See also BELL CRANK. For manually operated items see LEVER, MANUAL CONTROL. View more Remote Control Lever
January 2023
8
Marketplace 1680-01-564-4114
Request a Quotation from participating marketplace vendors
Related Documents 1680-01-564-4114 1+ Documents (More...)
Restrictions 1680-01-564-4114
1680-01-564-4114 is a Remote Control Lever 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 1680-01-564-4114
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1680-01-564-4114
- Australia (ZA01)
- Effective Date:
- 1 Jun 2008
- Canada (ZC01)
- Effective Date:
- 1 Dec 2011
- Germany (ZG01)
- Effective Date:
- 1 Nov 2011
Approved Sources 1680-01-564-4114
- Part Number
- Manufacturer
- Status
- 936843-101
- Manufacturer
- 98897 - Lockheed Martin Corp (Active)
- Primary Buy
- Primary Buy
Datasheet 1680-01-564-4114
- Characteristic
- Specifications
- FIIG
- Specifications
- A524P0
- End Item Identification [AGAV]
- P-3A Aircraft, Next Higher Assembly, Door Assembly 1560-00-899-1033
- Center To Center Distance Between Link And Shaft Holes [BFGW]
- 4.680 Inches Nominal
- Material [MATT]
- Steel
- Link End Hole Diameter [BFHA]
- 0.251 Inches Minimum And 0.258 Inches Maximum
- Link End Thickness [BFGY]
- 0.250 Inches Nominal
- Shaft End Thickness [BFGX]
- 0.950 Inches Nominal
- Part Name Assigned By Controlling Agency [CXCY]
- Hinge Lever Exhaust Door, Fwd
- Style Designator [STYL]
- One Hole Tongue Link End, Securing Hole Shaft End
NATO Stock Numbers Related to 1680-01-564-4114
Freight Information 1680-01-564-4114
1680-01-564-4114 has freight characteristics managed by Australia.. 1680-01-564-4114 has a variance between NMFC and UFC when transported by rail and the description should be consulted.