1560-14-415-3554
Aircraft Rudder
1560144153554 144153554 DA2C351A2
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 5 May 1987
Data Last Changed
July 2023
July 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 1560-14-415-3554
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DA2C351A2 A hinged or pivoted vertical control surface, usually hinged to the tail post aft of the vertical
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Restrictions 1560-14-415-3554
End Users 1560-14-415-3554
- France (ZF)
- Greece (ZU)
Approved Sources 1560-14-415-3554
- Part Number
- Manufacturer
- Status
- DA2C351A2
- Manufacturer
- F6117 - Dassault Aviation (Active)
- Primary Buy
- Primary Buy
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