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FAA Part 107 Loading and Performance

Authored by Bill Habiger

Science, Physics

11th Grade - University

27 Questions

NGSS covered

Used 30+ times

FAA Part 107 Loading and Performance
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1.

MULTIPLE CHOICE QUESTION

30 sec โ€ข 5 pts

An airplane has been loaded in such a manner that the CG is located aft of the aft CG limit. One undesirable flight characteristic a pilot might experience with this airplane would be

a longer takeoff run

difficulty in recovering from a stalled condition

stalling at higher-than-normal airspeed

2.

MULTIPLE CHOICE QUESTION

30 sec โ€ข 5 pts

When operating an unmanned airplane, the remote pilot should consider that the load factor on the wings may be increased anytime

the CG is shifted rearward to the aft CG limit

the airplane is subjected to maneuvers other than straight and level flight

the gross weight is reduced

3.

MULTIPLE CHOICE QUESTION

30 sec โ€ข 5 pts

Which of these maneuvers would cause an increase in load factor?

a level turn

a power off stall

a steady climb

4.

MULTIPLE CHOICE QUESTION

30 sec โ€ข 5 pts

To ensure that the unmanned aircraft center of gravity (CG) limits are not

exceeded, follow the aircraft loading instructions specified in the

Pilot's Operating Handbook or UAS Flight Manual

Aeronautical Information Manual (AIM)

Aircraft Weight and Balance Handbook

5.

MULTIPLE CHOICE QUESTION

30 sec โ€ข 5 pts

What could be a consequence of operating a small unmanned aircraft above its maximum allowable weight?

Faster speed

Increased maneuverability

Shorter endurance

Tags

NGSS.MS-ETS1-1

NGSS.MS-PS3-1

6.

MULTIPLE CHOICE QUESTION

30 sec โ€ข 5 pts

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

is visible to the visual observer or other crewmembers

does not adversely affect the center of gravity

can be easily removed without the use of tools

7.

MULTIPLE CHOICE QUESTION

30 sec โ€ข 5 pts

The angle of attack at which an airplane wing stalls will

increase if the CG is moved forward

change with an increase in gross weight

remain the same regardless of gross weight

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