WorksheetsUAS 401Loading Performance responsibility weather factors ef
Total questions: 11
Worksheet time: 11mins
Name
Class
Date
1.
Before each flight, the remote PIC must ensure that
a)
— ATC has granted clearance.
b)
— the site supervisor has approved the flight.
c)
— objects carried on the sUAS are secure.
2.
According to 14 CFR Part 107, who is responsible for determining the performance of a small unmanned aircraft?
a)
— Remote pilot-in-command.
b)
— Manufacturer.
c)
— Owner or operator.
3.
The most critical conditions of launch performance are the result of some combination of high gross weight, altitude, temperature, and
a)
— unfavorable wind.
b)
— obstacles surrounding the launch site.
c)
— powerplant systems.
4.
When loading cameras or other equipment on an sUAS, mount the items in a manner that
a)
— is visible to the visual observer or other crewmembers.
b)
— does not adversely affect the center of gravity.
c)
— can be easily removed without the use of tools.
5.
A UAS loaded with the most rearward center of gravity is
a)
— less stable at all speeds.
b)
— more stable at slow speeds.
c)
— more stable at fast speeds.
6.
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
a)
— the aircraft is subjected to maneuvers other than straight and level flight.
b)
— the CG is shifted rearward to the aft CG limit.
c)
— the gross weight is reduced.
7.
(Refer to Figure 2.) If an sUAS weighs 10 pounds, what approximate weight would the sUAS structure be required to support during a 60° banked turn while maintaining altitude?
a)
— 10.15 pounds.
b)
— 30 pounds.
c)
— 20 pounds.
8.
(Refer to Figure 2.) If an sUAS weighs 50 pounds, what approximate weight would the sUAS structure be required to support during a 30° banked turn while maintaining altitude?
a)
— 60 pounds.
b)
— 45 pounds.
c)
— 30 pounds.
9.
(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?
a)
— 34 pounds.
b)
— 47 pounds.
c)
— 38 pounds.
10.
The amount of excess load that can be imposed on the wing of an airplane depends upon the
a)
— position of the CG.
b)
— speed of the airplane.
c)
— abruptness at which the load is applied.
11.
Which basic flight maneuver increases the load factor on an sUAS as compared to straight-and-level f light?
a)
— Climbs.
b)
— Turns.
c)
— Stalls.
100 %
