FAA Federal Aviation Regulations (FARS, 14 CFR)
FARs > Part 27 > Section 399 - Dual control system
section 27.397 |
section 27.411
Each dual primary flight control system must be designed to withstand the loads that result when pilot forces of 0.75 times those obtained under § 27.395 are applied --
(a) In opposition; and
(b) In the same direction.
   
Current page: FARs > Part 27 > Section 399 - Dual control system
section 27.397 |
section 27.411
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