FAA Private Pilot Helicopter (PRH)Helicopter Aerodynamics and SystemsMedium

A helicopter is loaded to maximum gross weight for a hover-out-of-ground-effect departure on a hot day at a high-elevation airport. Compared to the same helicopter loaded at a lighter weight under the same conditions, what effect does the increased gross weight have on hover performance?

  1. AIt has no effect on power required but decreases hover ceiling
  2. BIt increases the power required to hover and decreases hover ceiling
  3. CIt decreases the power required to hover and increases hover ceiling
  4. DIt increases the power required but increases hover ceiling
Show answer & explanation

Correct answer: B. It increases the power required to hover and decreases hover ceiling

A higher gross weight requires the rotor system to produce more lift, which requires greater blade pitch and induced drag, thus increasing power required to hover; this reduces the maximum altitude at which the helicopter can hover (hover ceiling) for given conditions.

Why the other options are wrong

  • A. Power required does increase with weight, it does not stay constant.
  • C. Increased weight requires more, not less, power to hover.
  • D. Increased weight decreases, not increases, hover ceiling.

Weight Effect on Hover Performance

Increased gross weight requires greater rotor thrust, increasing power required to hover and lowering the hover ceiling.

  • More weight requires more lift, more induced drag, more power
  • Hover ceiling decreases as gross weight increases
  • High density altitude compounds the power penalty of heavy loading

Memory trick: Heavier helicopter, higher power hunger, lower hover height

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