1560-21-806-3545
Aircraft Rudder
1560218063545 218063545 41A22000
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
Managed by Canada
NSN Created on 6 Oct 1967
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
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41A22000 A hinged or pivoted vertical control surface, usually hinged to the tail post aft of the vertical
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Restrictions 1560-21-806-3545
End Users 1560-21-806-3545
- Canada (ZC)
Approved Sources 1560-21-806-3545
- Part Number
- Manufacturer
- Status
- 41A22000
- Manufacturer
- 88308 - Bombardier Inccanadair (Active)
- Primary Buy
- Primary Buy
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