Summary

  • Reduced-thrust takeoff increases engine durability by reducing operational stress and minimizing temperatures in the turbines, ultimately extending the serviceable life of the engine.
  • Maximum structural takeoff weight must never be exceeded, as it is determined by aircraft structure resistance criteria, landing gear resistance, and impact criteria during landing.
  • Reduced-thrust takeoff is not recommended on contaminated runways or in the presence of wind shear, as it can result in loss of speed and potentially dangerous situations.