55 900 kg

53 500 kg

 51 900 kg

55 000 kg

860 ft/min

630 ft/min

910ft/min

813 ft/min

14.9 NM

13.4 NM

10.0 NM

12.5 NM

Both engine types will suffer from similar degradation.

It will cause no change in performance in either type of engine.

Turbine engines will suffer from worse degradation in performance than piston engines.

Piston engines will suffer from worse degradation in performance than turbine engines.

to conduct an instrument approach at the alternate.

after engine failure, if the aeroplane is above the one-engine-inoperative cruise ceiling.

after cabin depressurisation.

to conduct a visual approach with one engine out.

special crosswind limitations may apply in case of contaminated runways. Aircraft-type-specific limitations are to be found in the Operations Manual Part B.

Crosswind limitations are only given for dry runway surface conditions. Aircraft-type-specific limitations are to be found in the Operations Manual Part A.

special crosswind limitations may apply in case of contaminated runways. Aireraft-type-specific limitations are to be found in the Operations Manual Part D.

Crosswind limitations are only given for dry runway surface conditions. Aircraft-type-specific limitations are to be found in the Operations Manual Part C.

Both the low-speed buffet and high-speed buffet decrease

The low-speed buffet decreases and the high-speed buffet increases.

Both the low-speed buffet and high-speed buffet increase.

The low-speed buffet increases and the high-speed buffet decreases.

It increases until the increase in TAS is offset by the increase in power required.

It decreases until the increase in Ground speed is offset by the increase in power required.

It decreases until the decrease in TAS is offset by the increase in Power required.

It increases until the increase in the Ground speed is offset by the increase in power required.

465 ft

215 ft

515 ft

265 ft

76 kt

88 kt

82 kt

78 kt