FAA Federal Aviation Regulations (FARS, 14 CFR)
FARs > Part 27 > Section 177 - Static directional stability
section 27.175 |
section 27.231
Static directional stability must be positive with throttle and collective controls held constant at the trim conditions specified in § 27.175 (a) and (b). This must be shown by steadily increasing 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. 27-21, 49 FR 44433, Nov. 6, 1984]
   
Current page: FARs > Part 27 > Section 177 - Static directional stability
section 27.175 |
section 27.231
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