1560-14-438-5220
Aircraft Rudder
1560144385220 144385220 R4A350M1
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 1990
Data Last Changed
July 2023
July 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 1560-14-438-5220
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Related Documents 1560-14-438-5220 1+ Documents (More...)
Feb 2001 1560-14-521-0818 Aircraft Rudder T700A5530001003RNCC: 5 | RNVC: 1 | DAC: 2 5 Jul 2000 1560-14-438-5220
Restrictions 1560-14-438-5220
End Users 1560-14-438-5220
- France (ZF)
Approved Sources 1560-14-438-5220
- Part Number
- Manufacturer
- Status
- R4A350M1
- Manufacturer
- F6117 - Dassault Aviation (Active)
- Primary Buy
- Primary Buy
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