Loading and Performance, Part 107 certification 2026

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Progress: 24% (23/94)

Learning progress ?

1. What effect does high density altitude have on the efficiency of a UA propeller?Not learned 2. To ensure that the unmanned aircraft center of gravity (CG) limits are not exceeded, follow the aircraft loading instructions specified in theNot learned 3. What could be a consequence of operating a small unmanned aircraft above its maximum allowable weight?Not learned 4. According to 14 CFR part 107, who is responsible for determining the performance of a small unmanned aircraft?Not learned 5. When operating an unmanned airplane, the remote pilot should consider that the load factor on the wings may be increased any timeNot learned 6. A stall occurs when the smooth airflow over the unmanned airplane's wing is disrupted, and the lift degenerates rapidly. This is caused when the wingNot learned 7. (Refer to Figure 2.) If an unmanned airplane weighs 33 pounds, what approximate weight would the airplane structure be required to support during a 30° banked turn while maintaining altitude?Not learned 8. How would high density altitude affect the performance of a small unmanned aircraft?Not learned 9. Operating outside of the weight and balance limits of an unmanned aircraftNot learned 10. (Refer to Figure 2.) If an unmanned aircraft weighs 20 pounds, what approximate weight would the aircraft structure be required to support during a 60° banked turn while maintaining altitude?Not learned 11. An unmanned aircraft has been loaded in such a manner that the CG is located aft of the aft CG limit. One undesirable flight characteristic a remote pilot might experience with this aircraft would beNot learned 12. (Refer to Figure 2.) If an unmanned aircraft weighs 45 pounds, what approximate weight would the aircraft structure be required to support during a 45° banked turn while maintaining altitude?Not learned 13. The four forces acting on an airplane in flight areNot learned 14. When are the four forces that act on an airplane in equilibrium?Not learned 15. (Refer to Figure 1.) The acute angle A is the angle ofNot learned 16. The term "angle of attack" is defined as the angle between theNot learned 17. What is the relationship of lift, drag, thrust, and weight when the airplane is in straight-and-level flight?Not learned 18. An airplane said to be inherently stable willNot learned 19. The amount of excess load that can be imposed on the wing of an airplane depends upon theNot learned 20. Which basic flight maneuver increases the load factor on an airplane as compared to straight-and-level flight?Not learned 21. What effect does high density altitude, as compared to low density altitude, have on propeller efficiency and why?Not learned 22. What is density altitude?Not learned 23. If the outside air temperature (OAT) at a given altitude is warmer than standard, the density altitude isNot learned 24. Which combination of atmospheric conditions will reduce aircraft takeoff and climb performance?Not learned 25. What effect does high density altitude have on aircraft performance?Not learned 26. What effect, if any, does high humidity have on aircraft performance?Not learned 27. The angle of attack at which an airplane wing stalls willNot learned 28. Under which condition will pressure altitude be equal to true altitude?Not learned 29. Under what condition is pressure altitude and density altitude the same value?Not learned 30. Which factor would tend to increase the density altitude at a given airport?Not learned 31. Which statement relates to Bernoulli's principle?Not learned 32. The angle between the chord line of an airfoil and the relative wind is known as the angle ofNot learned 33. Changes in the center of pressure of a wing affect the aircraft'sNot learned 34. At what bank angle for a turn does the additional force on the wings become significant?Not learned 35. Center of gravity can be found byNot learned 36. In weight and balance calculations, arm isNot learned