Which of the following increases the stall angle? a. Slats b. Flaps c. Spoilers d. Ailerons

Which of the following increases the stall angle?  
a. Slats  
b. Flaps  
c. Spoilers  
d. Ailerons
by

1 Answer

Answer :

a. Slats
by

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The control surface which gives longitudinal control is: a. The rudder b. The ailerons c. The elevators d. The flaps

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Last Answer : c. The elevators

Lowering the flaps during a landing approach: a. Increases the angle of descent without increasing the airspeed b. Decreases the angle of descent without increasing power c. Eliminates floating d. Permits approaches at a higher indicated airspeed

Description : Lowering the flaps during a landing approach: a. Increases the angle of descent without increasing the airspeed b. Decreases the angle of descent without increasing power c. Eliminates floating d. Permits approaches at a higher indicated airspeed

Last Answer : a. Increases the angle of descent without increasing the airspeed

If the ailerons are deflected to 10°, compared to 5°, this will cause: a. An increased angle of bank b. An increased rate of roll c. No change to either bank angle or roll rate d. A reduction in the adverse yawing moment

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In recovery from a spin: a. Ailerons should be kept neutral b. Airspeed increases c. Ailerons used to stop the spin d. Rudder and ailerons used against the direction of spin direction

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To give the best obstacle clearance on take-off, take-off should be made with: a. Flaps partially extended and at best rate of climb speed (Vy) b. Flaps partially extended and at best angle of climb speed (Vx) c. Flaps retracted and at best rate of climb speed (Vy) d. Flaps retracted and at best angle of climb speed (Vx)

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Last Answer : d. Decreased sink rate

The method of alighting the aeroplane on water during a ditching is to: a. Carry out a normal approach with flaps and gear selected as normal but to calculate all speeds plus 10kts b. Reduce the approach angle to 1.5deg (150ft/mile), add 15kts to all speeds, keep the aeroplane clean (no flaps or gear) and fly it into the surface c. Fly a normal approach but keep the gear up and land at lowest possible speed with the nose raised for the tail to strike first d. Fly a normal approach to stalling speed and then drop the aeroplane vertically onto the water

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Which stall has the greatest angle of attack? a. Low speed stall b. High speed stall (shock stall) c. Deep stall d. Accelerated stall

Description : Which stall has the greatest angle of attack? a. Low speed stall b. High speed stall (shock stall) c. Deep stall d. Accelerated stall

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If the angle of attack is increased beyond the critical angle of attack, the wing will no longer produce sufficient lift to support the weight of the aircraft: a. Unless the airspeed is greater than the normal stall speed b. Regardless of airspeed or pitch attitude c. Unless the pitch attitude is on or below the natural horizon d. In which case, the control column should be pulled-back immediately

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Last Answer : b. Regardless of airspeed or pitch attitude

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Last Answer : b. The lift would increase when the flaps are lowered

If a landing is to be made without flaps, the landing speed must be: a. reduced b. increased c. the same as for landing with flaps d. the same as for landing with flaps but with a steeper approach

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When does the first segment of the take-off climb begin? a. When V2 is reached b. When 35 feet is reached c. When flaps are up d. When gear and flaps are up

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What is the recommended technique to counter the loss of airspeed and resultant lift from wind shear? a. Maintain, or increase, pitch attitude and accept the lower-than-normal airspeed indications b. Lower the pitch attitude and regain lost airspeed c. Avoid overstressing aircraft, pitch to stick shaker, and apply maximum power d. Accelerate the aircraft to prevent a stall by sacrificing altitude

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Last Answer : c. Avoid overstressing aircraft, pitch to stick shaker, and apply maximum power

If the stalling speed in a 15 degree bank turn is 60kt, what would the stall speed be in a 45 degree bank? a. 83kt b. 70kt c. 85kt d. 60kt

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Last Answer : b. 70kt

A stall warning device must be set to operate: a. At the stalling speed b. At a speed just below the stalling speed c. At a speed about 5% to 10% above the stalling speed d. At a speed about 20% above the stalling speed

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Last Answer : c. At a speed about 5% to 10% above the stalling speed

If airbrakes are extended during a glide, and speed maintained, the rate of descent will: a. Increase and glide angle will be steeper b. Increase but glide angle will remain the same c. Decrease d. Remain the same

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What factors affect descent angle in a glide? a. Configuration and altitude b. Configuration and angle of attack c. Mass and altitude d. Mass and configuration

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An aircraft is travelling at 120 kts, what angle of bank would be required for a rate 1(one) turn? a. 30° b. 12° c. 18° d. 35°

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