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1560-00-122-8183
Aircraft Rudder
1560001228183 001228183 5118595
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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May 2023
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 Restrictions  1560-00-122-8183
1560-00-122-8183 is a Aircraft Rudder that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item is a US Munitions List Item and must be mutilated to scrap. 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  1560-00-122-8183
- Schedule B
 - Subscribe to View Schedule B
 - HTS Code
 - Subscribe to View HTS Code
 
 End Users  1560-00-122-8183
- New Zealand (ZE01)   
- Effective Date:
  - 1 Apr 1991
 
- Greece (ZU01)   
- Effective Date:
  - 1 Apr 1991
 
 Approved Sources  1560-00-122-8183
- Part Number
- Manufacturer
 - Status
 - 5118595
  - Manufacturer
 -  88277 - The Boeing Company (Active) 
- Primary Buy
  - Primary Buy
 - 5118595
 -  18355 - The Boeing Company (Active) 
- Canceled/Obsolete
  - Canceled/Obsolete
 
 Datasheet  1560-00-122-8183
- Characteristic
- Specifications
 - FIIG
  - Specifications
 - A11500
 - Aircraft Mission Design Series [CZEK]
 - C-47
 
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 Freight Information  1560-00-122-8183
1560-00-122-8183 has freight characteristics.. 1560-00-122-8183 has a variance between NMFC and UFC when transported by rail and the description should be consulted.