increases, and CAS decreases

decreases, and CAS decreases

decreases, and CAS increases

increases, and CAS increases

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

decreases as mass decreases.

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

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

Low flap setting, high PA, low OAT.

High flap setting, low PA, low OAT.

Low flap setting, high PA, high OAT.

Low flap setting, low PA, low OAT.

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

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, and a distance equivalent to 2 seconds at V₁

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

lower air density.

lower temperature.

fuel consumption.

movement of the centre of gravity.

a 1% higher TAS for maximum specific range.

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

1,3,4,5

1,3,4

2, 3, 4

1,2,3,4

(1) Short; (2) decrease; (3) increasing

(1) Short; (2) increase; (3) increasing.

(1) Long: (2) decrease; (3) decreasing

 (1) Long; (2) increase; (3) increasing.

Increase and the climb gradient will increase.

Increase and the climb gradient will decrease.

Decrease and the climb gradient will increase

Decrease and the climb gradient will decrease.

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

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

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.