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To establish a climb after takeoff in an aircraft equipped with a constant-speed propeller, the output of the engine is reduced to climb power by decreasing manifold pressure and ______.
To establish a climb after takeoff in an aircraft equipped with a constant-speed propeller, the output of the engine is reduced to climb power by decreasing manifold pressure and ______.
  • increasing RPM by decreasing propeller blade angle
  • decreasing RPM by decreasing propeller blade angle
  • decreasing RPM by increasing propeller blade angle

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