He has to decrease his speed.

He has to maintain his speed.

He has to increase his speed.

There is too little data to answer the question.

An increase in TAS will lead to a decrease in fuel flow up to the maximum endurance speed and increase

thereafter

An increase in TAS will lead to an increase in the fuel flow up to the maximum endurance speed and decrease

thereafter

TAS and fuel flow are independent of one another, so the fuel flow is unaffected by any change in TAS.

An increase in TAS will lead to an increase in the fuel flow.

Minimum fuel flow

Longest flight duration

Minimum specific fuel consumption.

Minimum drag.

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.

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.

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.

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.

3

1

2

4

The BEST performance will occur when the outside air temperature is high and the pressure altitude is low.

The WORST performance will occur with a combination of low outside air temperature and low pressure

altitude

The WORST performance will occur with a combination of high outside air temperature and high pressure

altitude.

The BEST performance will occur when the outside air temperature is low and the pressure altitude is high.

 speed for lowest endurance

Speed for lowest range.

speed for best range.

 speed for best endurance.