1560-14-392-3312
Aircraft Rudder
1560143923312 143923312 262-10-32251-50 85-692-5623
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 France
NSN Created on 21 Mar 1984
Data Last Changed
July 2023
July 2023
NATO Update Count
1
1
NATO Data Quality
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262-10-32251-50 85-692-5623 A hinged or pivoted vertical control surface, usually hinged to the tail
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Restrictions 1560-14-392-3312
End Users 1560-14-392-3312
- France (ZF)
Approved Sources 1560-14-392-3312
- Part Number
- Manufacturer
- Status
- 262-10-32251-50
- Manufacturer
- F6198 - Airbus Operations (Active)
- Primary Buy
- Primary Buy
- 85-692-5623
- F5385 - Section De Codification 85 (Cancelled)
- NATO Reference
- NATO Reference
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