When operating an unmanned airplane the remote pilot should consider that the load factor on the wings may be increased any time?

The chart shows a gray line with "VR1667, VR1617, VR1638, and VR1668." Could this area present a hazard to the operations of a small UA?

True/False - A UAS may carry a payload of hazardous materials as defined by 49 CFR 171?

False, UAS may not transport hazardous materials without a waiver

As density altitude increases, what happens to the performance of the UAS?

What causes density altitude to increase?

High altitude, high temperature, high humidity

What is the critical angle of attack?

The angle at which lift is no longer generated and the UAS goes into an aerodynamic stall.

According to 14 CFR part 107, who is responsible for determining the performance of a small unmanned aircraft?1. Owner or operator2. Remote Pilot in Command3. Manufacturer

When operating an unmanned aircraft, the Remote Pilot in Command should consider that the load factor on the wings or rotors may be increased anytime when:1. The center of gravity (CG) is shifted rearward to the aft CG limit2. The aircraft is subjected to maneuvers other than straight and level flight.

3. The gross weight is reduced

The aircraft is subjected to maneuvers other than straight and level flight.

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 wing:1. Exceeds maximum allowable operating weight2. Exceeds the maximum speed

3. Exceeds its critical angle of attack

Exceeds its critical angle of attack

Before each flight, the Remote PIC must ensure that:1. The site supervisor has approved the flight2. Objects carried on the sUAS are secure

3. ATC has granted clearance

Objects carried on the sUAS are secure

What could be a consequence of operating a small unmanned aircraft above its maximum allowable weight?1. Increased maneuverability2. Shorter endurance

3. Faster speed

To ensure that the unmanned aircraft center of gravity (CG) limits are not exceeded, follow the aircraft loading instructions specified in the:1. Aircraft Weight and Balance Handbook2. Pilot’s Operating Handbook or UAS Flight Manual

3. Aeronautical Information Manual (AIM)

Pilot’s Operating Handbook or UAS Flight Manual