1186. Before each flight, the remote PIC must ensure that

1300. What purpose does a rudder perform on an sUAS airplane

1187. You are operating an sUAS that does not have GPS or an installed ground speed limiter. How can you determine the speed you are operating?

1188. How can a remote pilot determine the altitude of the terrain and structures where the flight will be conducted?

1189. You are operating an sUAS that does not have GPS or an installed altimeter. How can you determine the altitude you are operating?

1190. When loading cameras or other equipment on an sUAS, mount the items in a manner that

1191. To ensure that the UA's center of gravity limits are not exceeded, follow the aircraft loading instructions specified in the

1192. What could be a consequence of operating a UA above its maximum allowable weight?

1193. When operating an aircraft the remote PIC is responsible for using

1194. Which of the following is true regarding weight and balance of small unmanned aircraft

1293. A UAS loaded with the most rearward center of CG is

1195. When Operating an UA, the remote PIC should consider that the load factor on the wings or rotors may be increased anytime

1198. (Refer to Figure 2) if an unmanned airplane weighs 33 pounds what approximate weight would the airplane structure be required to support during 30 banked turn while maintaining altitude

1199. The amount of excess load that can be imposed on the wing of an airplane depends upon the

1200. Which basic flight maneuver increases the load factor on an sUAS as compared to straight and level flight

1201. the term "angle of attack" is defined as the angle

1202. The angle of attack at which an airfoil stalls will

1203. A stall occurs when the smooth airflow over the unmanned aircraft's wing/propeller is disrupted, and the lift reduces rapidly. This is caused when the wing/propeller

1204. An increase in load factor will cause an unmanned aircraft

1314. In a 45 banking turn a UA will

1205. According to 14 CFR part 107, who is responsible for determining the performance of a sUA

1206. What effect dose an uphill terrain slope have on launch performance?

1207. The most critical condition of launch performance are the result of some combination of high gross weight, altitude, temperature and

1208. Maximum endurance is obtained at the point of minimum power to maintain the aircraft

1209. When range and economy of operation are the principle goals the remote pilot must ensure that the sUAS will be operated at the recommended

1210. what is the best source for sUAS performance data and information

1324. Upon request by the FAA the remote PIC must provide

1274. Sunrise is 0645. when can you launch your sUAS operation