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1560-01-568-6868
Aircraft Rudder
1560015686868 015686868 68A240001-1023
A hinged or pivoted vertical control surface, usually hinged to the tail post aft of the vertical stabilizer, for the purpose of applying yawing moments to an aircraft to assist in initiating right or left turns about the vertical axis of flight. It may include a trim tab mechanism. Excludes STABILIZER, VERTICAL. View more Aircraft Rudder
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January 2023
3

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Related Documents 1560-01-568-6868 1+ Documents (More...)
United States (US) 4. 1560-01-568-6868 Marketplace Restrictions Approved Sources Datasheet Management
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Restrictions 1560-01-568-6868
1560-01-568-6868 is a Aircraft Rudder 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 a US Munitions List or Commerce Control List Item which must be destroyed to prevent restoration or repair. Only authorized parties may possess this item. This item may be hazardous as it is in a Federal Supply Class for potentially hazardous items. A MSDS should be available from the supplier for the end user to evaluate any hazards. This item does not contain a precious metal.
Import and Export 1560-01-568-6868
- Schedule B
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- HTS Code
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End Users 1560-01-568-6868
- Singapore (YJ01)
- Effective Date:
- 1 Nov 2008
- Republic of Korea (ZH01)
- Effective Date:
- 1 Sep 2010
Approved Sources 1560-01-568-6868
- Part Number
- Manufacturer
- Status
- 68A240001-1023
- Manufacturer
- 76301 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-568-6868
- Characteristic
- Specifications
- FIIG
- Specifications
- A11500
- End Item Identification [AGAV]
- F-15Sg Platform
- Part Name Assigned By Controlling Agency [CXCY]
- Rudder Assy, Vertical Stabilizer
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Freight Information 1560-01-568-6868
1560-01-568-6868 has freight characteristics managed by Singapore.. 1560-01-568-6868 has a variance between NMFC and UFC when transported by rail and the description should be consulted.