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1680-01-523-3605
Quadrant Control Assembly
1680015233605 015233605 17P1F6033-1
A cockpit mounted, manually operated item, designed to regulate aircraft functions, which may include throttle, afterburner, flaps, trim tabs, and the like. May consist of lever(s), grip(s), switch(es), and fulcrum(s). Excludes wire rope and push-pull assemblies, and all quadrants or levers that are engine mounted. View more Quadrant Control Assembly

January 2023
2

 Marketplace  1680-01-523-3605
 Marketplace  1680-01-523-3605
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 Related Documents  1680-01-523-3605  1+ Documents (More...)
 Related Documents  1680-01-523-3605  1+ Documents (More...) 
United States (US) 4. 1680-01-523-3605 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 1680-01-523-3605 RQST Updated Every Day 1680-01-523-3605 RQST NE Restrictions
 Restrictions  1680-01-523-3605
 Restrictions  1680-01-523-3605
1680-01-523-3605 is a Quadrant Control Assembly that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item has been confirmed as a Critical Munitions List Item or a Sensitive Commerce Control List Item and cannot be in the possession of any party anywhere in the World who is not an authorized NATO Government. Any other possessor of this item should mutilate it now as possession violates international and local laws. This item is a confirmed Commerce Control List Item (CCLI). This item is not suspected to be hazardous. This item does not contain a precious metal.
 Import and Export  1680-01-523-3605
 Import and Export  1680-01-523-3605
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
 End Users  1680-01-523-3605
 End Users  1680-01-523-3605
- US Air Force (FBB5)   - Effective Date:
- 1 Aug 2004
 Approved Sources  1680-01-523-3605
 Approved Sources  1680-01-523-3605
- Part Number- Manufacturer
- Status
- 17P1F6033-1
- Manufacturer
-  88277 - The Boeing Company (Active) - Primary Buy
- Primary Buy
 Datasheet  1680-01-523-3605
 Datasheet  1680-01-523-3605
- Characteristic- Specifications
- FIIG
- Specifications
- A529V0
- Material [MATT]
- Aluminum Alloy
- Aircraft Location [CZDJ]
- Stick And Rudder Pedal Control
- Aircraft Mission Design Series [CZEK]
- C-17A Aircraft
- Part Name Assigned By Controlling Agency [CXCY]
- Support Assy, Stature Adjust, Rudder Pedals
- Reference Data And Literature [RDAL]
- T.O. 1C-17A-4-47 F.18 I.88
 Management Data  1680-01-523-3605
 Management Data  1680-01-523-3605
- Effective Date
- Organization- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- May 2010
- Department of the Air Force (DF)- EA
- Subscribe
- 1
- EA
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 Freight Information  1680-01-523-3605
 Freight Information  1680-01-523-3605
1680-01-523-3605 has freight characteristics.. 1680-01-523-3605 has a variance between NMFC and UFC when transported by rail and the description should be consulted. 
 
 