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Rudder sizing on a single-engine aircraft is typically governed by

  • A.Flutter margin
  • B.Crosswind landing and spin recovery
  • C.Engine-out control
  • D.Cruise directional stability

Answer: B

Correct answer: Crosswind landing and spin recovery

A single-engine aircraft has no asymmetric thrust case, so the sizing conditions that govern a twin's fin do not apply.

What remains are the two demands the question names: yawing the aircraft straight from its crab angle at the lowest speed of the approach, and generating the yawing moment needed to stop rotation in a spin, which requires rudder area that is not blanketed by the tailplane. Engine-out control governs a multi-engine aircraft, and cruise directional stability is met comfortably by a fin sized for either of these.

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