FAA Federal Aviation Regulations (FARS, 14 CFR)
FARs > Part 25 > Section 171 - General
section 25.161 |
section 25.173

The airplane must be longitudinally, directionally, and laterally stable in accordance with the provisions of §§ 25.173 through 25.177. In addition, suitable stability and control feel (static stability) is required in any condition normally encountered in service, if flight tests show it is necessary for safe operation.
[Doc. No. 5066, 29 FR 18291, Dec. 24, 1964, as amended by Amdt. 25-7, 30 FR 13117, Oct. 15, 1965]
  
Current page: FARs > Part 25 > Section 171 - General
section 25.161 |
section 25.173

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