the thrust required is independent of the airspeed.

a thrust reduction results in an acceleration of the aeroplane.

a lower airspeed requires less thrust because drag is decreased.

a lower airspeed requires more thrust.

Minimum fuel flow

Longest flight duration

Minimum specific fuel consumption.

Minimum drag.

SR will decrease

SR will increase.

SR will remain constant but SFC will decrease.

SR will remain constant but SFC will increase.

You would expect to have to decrease the engine thrust to stay on the correct flight path because with the

headwind the ground path will tend to decrease.

You would expect to have to decrease the engine thrust to stay on the correct flight path because with the

headwind the ground path will tend to increase.

You would expect to have to increase the engine thrust to stay on the correct flight path because with the

headwind the ground path will tend to decrease.

You would expect to have to increase the engine thrust to stay on the correct flight path because with the

headwind the ground path will tend to increase.

The mass of an aeroplane does not have any effect on the speed for descent.

The higher the gross mass the greater is the speed for descent.

The higher the average temperature (OAT) the lower is the speed for descent.

The higher the gross mass the lower is the speed for descent.

3

1

2

4

 speed for lowest endurance

Speed for lowest range.

speed for best range.

 speed for best endurance.

the altitude in the standard atmosphere at which the prevailing density occurs.

the height obtained by setting the subscale of an altimeter to ONE.

the altitude obtained by setting the subscale of an altimeter to QNH.

the height in the standard atmosphere at which the prevailing density occurs.

SRincreases slowly with altitude up to full throttle height.

SR and SFC (Specific Fuel Consumption) decrease slowly with altitude up to full throttle height.

SR and SFC (Specific Fuel Consumption) increase slowly with altitude up to full throttle height.

SR decreases slowly with altitude up to throttle height.

decelerate during an abortive take-off.

park between two flights.

vacate at the end of the runway.

remain on the runway after a balked landing.