FAA Federal Aviation Regulations (FARS, 14 CFR)
FARs > Part 29 > Section 177 - Static directional stability
section 29.175 |
section 29.181

Static directional stability must be positive with throttle and collective controls held constant at the trim conditions specified in § 29.175 (a), (b), and (c). Sideslip angle must increase steadily with directional control deflection for sideslip angles up to ±10° from trim. Sufficient cues must accompany sideslip to alert the pilot when approaching sideslip limits.
[Amdt. 29-24, 49 FR 44436, Nov. 6, 1984]
  
Current page: FARs > Part 29 > Section 177 - Static directional stability
section 29.175 |
section 29.181

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