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as120 CH 5&6

Total questions: 24

Worksheet time: 12mins

Name
Class
Date
1.

Wings angled upward from the fuselage

a)

Dihedral

b)

Anhedral

c)

neither

2.

what is lift

a)

Rearward force created by disruption of airflow

b)

Upward force produced by the dynamic effect of the air on the wing

c)

neither

3.

Downward force produced by airplane, crew, fuel, and baggage load

a)

lift

b)

drag

c)

weight

4.

What is critical angle of attack?

a)

That angle of attack at which a wing stalls but only at certain airspeeds or weights

b)

That angle of attack at which a wing stalls at any airspeed, attitude or weight

c)

That angle of attack at which a wing stalls but only a certain flight attitudes

5.

What is used to reduce wingtip vortices

a)

winglets

b)

flaps

c)

elevator

6.

What is winglets advantage?

a)

Reduces induced drag caused by vortices

b)

Creates an offsetting thrust

c)

All of the above

7.

What is ground effect?

a)

Increased efficiency of a wing when flying within a wing's length of the ground

b)

An increase in drag by as much as 50% when flying within a wing's length of the ground

c)

Condition of reduced lift when flying within a wing's length of the ground

8.

What happens when an airplane is turned?

a)

Loss of airspeed, unless additional power is added

b)

Loss of altitude, unless additional lift is created

c)

Increase in altitude, unless excess lift is reduced

9.

What is the danger of a steeply banked turn?

a)

Increased stall speed

b)

Increased pitch

c)

Decreased stall speed

10.

What is defined as computing intermediate values between a series of given values?

a)

Approximation

b)

Interpolation

c)

Estimation

11.

What is load factor?

a)

Ratio of the load supported by the wings as compared to the actual weight of the aircraft

b)

Center-seeking force directed inward created by the horizontal component of lift

c)

Amount of G's that an airplane should be capable of withstanding without failure

12.

If a pilot has improperly loaded or balanced an airplane, during which phase of flight will poor or unsafe performance normally occur?

a)

Takeoff

b)

Cruise

c)

Landing

13.

Which of the following in NOT a primary flight control?

a)

Elevator

b)

Flap

c)

Aileron

14.

Which of the following is NOT a secondary flight control?

a)

Rudder

b)

Flap

c)

Spoiler

15.

Near stall, how should flight controls feel?

a)

No different than at cruise speeds

b)

Soft and sluggish

c)

Firm and responsive

16.

What does the checklist item "Flight Controls - FREE and CORRECT" mean?

a)

During the outside preflight, inspect the flight control surfaces hinges for corrosion, etc.

b)

Just before takeoff, verify that the flight controls move freely and the flight control surfaces move in the correct direction

c)

During the outside preflight, inspect the flight control surfaces rods and pulleys

17.

Hydraulic flight controls system

a)

Fluids used to transmit stick forces to control surfaces

b)

Electronic signals used to tranmit stick forces to control surfaces

c)

Rods and pulleys used to transmit stick forces to control surfaces

18.

Fly-by-wire flight control systems are

a)

Rods and pulleys used to transmit stick forces to control surfaces

b)

Fluids used to transmit stick forces to control surfaces

c)

Electronic signals used to tranmit stick forces to control surfaces

19.

Why are flaps, slats and slots used on aircraft?

a)

Permit low speed characteristics for takeoff and landing

b)

Permit high speed characteristics for cruise speeds

c)

All of the above

20.

In the diagram, which airplane has flaps & slats extended?

a)

Airplane A

b)

Airplane B

c)

Airplane C

21.

Flaps

a)

Trailing edge device that increases left and drag

b)

Leading edge device that delays airflow separation at high AOA

c)

Deployed on top of the wings to reduce lift and increase drag

22.

Spoliers

a)

Relieves pilot of need to maintain pressure on flight controls

b)

Trailing edge device that increases left and drag

c)

Deployed on top of the wings to reduce lift and increase drag

23.

Trim Systems

a)

Relieves pilot of need to maintain pressure on flight controls

b)

Deployed on top of the wings to reduce lift and increase drag

c)

Leading edge device that delays airflow separation at high AOA

24.

What direction will this airplane turn?

a)

LEFT

b)

RIGHT

c)

STRAIGHT AN LEVEL