The most aft CG location may be limited by:

1. Insufficient stick force stability

2. Insufficient flare capability

3. Excessive in-flight manoeuvrability

4. Insufficient in-flight manoeuvrability

The combination that regroups all of the correct statements is?

Which statement about an aeroplane entering ground effect is correct?

I) The downwash angle decreases

II) The induced angle of attack decreases

The calibrated airspeed during approach and landing, with all engines operating, at which, when the critical engine is suddenly made inoperative, it is possible to maintain control of the aeroplane with that engine still inoperative, and maintain straight flight with an angle of bank of not more than 5*, is called?

Aileron flutter can be caused by?

For a given elevator deflection, aeroplane longitudinal maneuverability decreases when?

Which of these statements about the limiting value of 5 degrees bank angle during VMCA determination are correct or incorrect?

I) When the bank angle is decreased from 5 degrees to 0 degrees, the value of VMCA will remain approximately constant

II) When the bank angle is increased beyond 5 degrees, there is a increasing risk of fin stall

The main function of a trailing edge flap is to?

The stall speed line in the manoeuvring load image runs through a point where the?

If the wing area is increased, lift will?

When spoilers are used as speed brakes?

What is the heading change of an aeroplane after 1 second in a steady co-ordinated horizontal rate one turn?

The units of wing loading ?

(I) W/S 

(II) dynamic pressure q are

VS1g is?

Sweepback of a wing positively influences

1. Static longitudinal stability

2. Static lateral stability

3. Dynamic longitudinal stability

The combination that regroups all of the correct statements is?

Upward deflection of a trim tab in the longitudinal control results in?

Assuming zero thrust, the point on the image corresponding to the value for minimum sink rate is?

Which of these statements about the gust load factor on an aeroplane are correct or incorrect?

I) When the wing area increases, the gust load factor decreases

II) When the EAS increases, the gust load factor decreases

The manoeuvre stability of a large jet transport aeroplane is 280 N/g. What stick force is required, if the aeroplane is pulled to the limit manoeuvring load factor from a trimmed horizontal straight and steady flight? (cruise configuration)

The difference between IAS and TAS will?

Which statement is correct?

I - A stick pusher activates at a higher angle of attack than a stick shaker

II - A stick shaker prevents the pilot from increasing the angle of attack further.

The horn balance is used for aerodynamic balancing.

 It consists?

T-Tail is __________ stable than a conventional because they receive _________ downwash?

Wave drag above MCRIT consists of?

When comparing a trim tab with an anti-balance tab, which of the following statements is correct? The trim tab:

Which of the following flight phenomena can occur at Mach numbers below the critical Mach number?

During landing of a low-winged jet aeroplane, the greatest elevator up deflection is normally required when the flaps are?

Which of these statements are correct or incorrect regarding a sideslip, with the relative airflow coming from the left, on an aeroplane that exhibits both directional and lateral stability?

I - The initial tendency of the nose of the aeroplane is to move to the right

II - The initial tendency of the right wing is to move down

An aeroplane exhibits static longitudinal stability, if, when the angle of attack changes?

Asymmetric propeller blade effect is mainly induced by?

Considering bank angle and engine thrust, what limits are taken into account when defining Vmc?