the maximum range speed increases and the maximum gradient climb speed is not affected.

the maximum range speed decreases and the maximum gradient climb speed decreases.

the maximum range speed decreases and the maximum gradient climb speed is not affected.

the maximum range speed decreases and the maximum gradient climb speed increases.

(1) Increase; (2) Decrease by more than 50%.

(1) Increase; (2) Increase by more than 50%.

 (1) Decrease by 50%; (2) Decrease by more than 50%

(1) Increase; (2) Decrease by 50%.

Inoperative flight management system.

Increased outside air temperature.

Increased take-off mass.

Inoperative anti-skid.

decreases, and CAS decreases

decreases, and CAS increases

increases, and CAS decreases

increases, and CAS increases

movement of the centre of gravity.

lower temperature.

lower air density.

fuel consumption.

 increases as mass decreases and is the altitude at which the specific range reaches its maximum.

decreases as mass decreases.

is the altitude up to which cabin pressure of 8 000 ft can be maintained.

is the altitude at which the specific range reaches its minimum.

a specific range which is approximately 99% of maximum specific range and a lower cruise speed.

an IAS which is 1% higher than the IAS for maximum specific range.

a specific range which is approximately 99% of maximum specific range and a higher cruise speed.

a 1% higher TAS for maximum specific range.

the distance to come to a full stop, and a distance equivalent to 2 seconds at V₁ all multiplied by 1.15.

 the distance to come to a full stop, and a distance equivalent to 2 seconds at V₁

150% of the distance to come to a full stop, and a distance equivalent to 2 seconds at V_EF.

the distance to come to a full stop multiplied by 1.15, and a distance equivalent to 2 seconds at V_EF.

Low flap setting, low PA, low OAT.

Low flap setting, high PA, high OAT.

Low flap setting, high PA, low OAT.

High flap setting, low PA, low OAT.

The required landing field length is the distance from 35 ft to the full stop point.

When determining the maximum allowable landing mass at destination, 60% of the available distance is taken into account, if the runway is expected to be dry.

An anti-skid system malfunction has no effect on the required landing field length.

In any case runway slope is one of the factors taken into account when determining the required landing field.