FAA Federal Aviation Regulations (FARS, 14 CFR)
FARs > Part 23 > Section 687 - Spring devices
section 23.685 |
section 23.689

The reliability of any spring device used in the control system must be established by tests simulating service conditions unless failure of the spring will not cause flutter or unsafe flight characteristics.
  
Current page: FARs > Part 23 > Section 687 - Spring devices
section 23.685 |
section 23.689

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