Aerodynamics - Dauntless
Instrumentation and Avionics - Dauntless
Four Forces of Flight
Aerodynamic Principles
Aircraft Structures
100

Ground effect is most likely to result in what problem?

A. Settling to the surface abruptly during landing

B. Inability to get airborne even though airspeed is sufficient for normal takeoff needs

C. Becoming airborne before reaching recommended takeoff speed

C. Becoming airborne before reaching recommended takeoff speed

100

When operating the transponder on the VFR code (1200), what is the minimum mode the transponder must be set in?

A. Mode A

B. Mode F

C. Mode C

A. Mode A

100

This is the force of flight which counteracts weight.

What is lift?

100

This is created by the movement of air from high pressure towards low pressure around the end of the wing structure.

What is a wingtip vorticy?

100

This is the control surface used to roll the aircraft.

What are the ailerons?

200

Changes in the center of pressure of a wing affect the aircraft's

A. Lifting capacity

B. Aerodynamic balance and controllability

C. Lifting ratio

B. Aerodynamic balance and controllability

200

Requests for deviation for inoperable ADS-B equipment may be made to

A. The Federal Aviation Administration 24 hours before the scheduled operation

B. The ATC facility having jurisdiction over the airspace at any time

C. The ATC facility having jurisdiction over the airspace at least 1-hour prior

B. The ATC facility having jurisdiction over the airspace at any time

200

This force is the result of the propeller generating horizontal lift.

What is thrust?

200

This is the left turning tendency that is associated with Newton's third law.

What is torque reaction?


200

This is the fuselage design of the Cessna 172.

What is a semi-monocoque fuselage design?

300

What is the best indicator to the pilot of the load factor on the airplane?

A. How firmly the pilot is pressed into the seat during a maneuver

B. Airspeed when pulling out of a descent

C. Amount of pressure required to operate the controls

A. How firmly the pilot is pressed into the seat during a maneuver

300

Which color identifies the never-exceed speed?

A. Upper limit of the white arc

B. Upper limit of the green arc

C. The red radial line

C. The red radial line

300

This is the type of drag which is increased at lower speeds, when the aircraft creates a large amount of lift.

What is induced drag?

300

This is the speed of minimum drag on a Cessna 172

What is 68 knots?

300

This is the landing gear style on the Cessna 172

What is a tricycle aircraft gear?

400

An aircraft airfoil is designed to produce lift resulting from a difference in the

A. negative air pressure below and a vacuum above the wing's surface

B. vacuum below the airfoil's surface and greater air pressure above the airfoil's surface

C. higher air pressure below the airfoil's surface and lower air pressure above the airfoil's surface

C. higher air pressure below the airfoil's surface and lower air pressure above the airfoil's surface

400

The speed at which a single flight control can be moved, one time, to its full deflection without risk of damage to the aircraft is

A. Maneuvering speed

B. Never exceed speed

C. Structural cruise speed

A. Maneuvering speed

400

These are the three types of parasite drag.

What is form drag, interference drag, and skin friction drag?

400

This is the force that opposes a horizontal component of lift in a turn.

What is centrifugal force?

400

This material, used to construct airplanes, can be subject to heat damage.

What is a composite aircraft structure?

500

Which basic flight maneuver increases the load factor on an airplane as compared to straight-and-level flight?

A. Climbs

B. Turns

C. Stalls

B. Turns

500

In a non-FADEC aircraft, an electrical system failure (battery and alternator) occurs during flight. In this situation, you would

A. probably experience failure of the engine ignition system, fuel gauges, aircraft lighting system, and avionics equipment.

B. probably experience engine failure due to the loss of the engine-drivel fuel pump and also experience failure of the radio equipment, lights, and all instruments that require alternating current

C. experience avionics equipment failure 

C. experience avionics equipment failure

500

This is the point where weight is applied on the airplane.

What is the center of gravity?

500

This is how an aircraft responds to a disturbance over time, and these are the three ways in which the aircraft may react to that disturbance over time?

What is positive, neutral, and negative dynamic stability?

500

This is the engine design in the Cessna 172

100 BONUS POINTS:

How much horsepower is the Cessna 172?

What is a horizontally opposed engine?