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While executing a 60 degree level turn, your aircraft is at a load factor of 2.0. What does this mean?. The total load on the aircraft's structure is two times its weight.. The load factor is over the load limit. The gust factor is two times the total load limit.

Which statement is true relative to changing angle of attack?. A decrease in angle of attack will increase pressure below the wing, and decrease drag. An increase in angle of attack will increase drag. An increase in angle of attack will decrease pressure below the wing, and increase drag.

(Refer to Figure 4.) What increase in load factor would take place if the angle of bank were increased from 60° to 80°?. 3 Gs. 3.5 Gs. 4 Gs.

If the airspeed is decreased from 98 knots to 85 knots during a coordinated level 45 degree banked turn, the load factor will. remain the same, but the radius of turn will decrease. decrease, and the rate of turn will decrease. remain the same, but the radius of turn will increase.

The angle of attack at which a wing stalls remains constant regardless of. weight, dynamic pressure, bank angle, or pitch attitude. dynamic pressure, but varies with weight, bank angle, and pitch attitude. weight and pitch attitude, but varies with dynamic pressure and bank angle.

To avoid possible wake turbulence from a large jet aircraft that has just landed prior to your takeoff, at which point on the runway should you plan to become airborne?. Past the point where the jet touched down. At the point where the jet touched down, or just prior to this point. Approximately 500 feet prior to the point where the jet touched down.

What is the best indicator to the pilot of the load factor on the airplane?. How firmly the pilot is pressed into the seat during a maneuver. Amount of pressure required to operate the controls. Airspeed when pulling out of a descent.

When transitioning from straight-and-level flight to a constant airspeed climb, the angle of attack and lift. are increased and remain at a higher lift-to-weight ratio to maintain the climb. remain the same and maintain a steady state lift-to-weight ratio during the climb. are momentarily increased and lift returns to a steady state during the climb.

Your flight takes you in the path of a large aircraft. In order to avoid the vortices you should fly. at the same altitude as the large aircraft. below the altitude of the large aircraft. above the flight path of the large aircraft.

Lift on a wing is most properly defined as the. force acting perpendicular to the relative wind. differential pressure acting perpendicular to the chord of the wing. reduced pressure resulting from a laminar flow over the upper camber of an airfoil, which acts perpendicular to the mean camber.