No, there is no P-factor (asymmetric blade effect) as on a propeller-driven aircraft.

Carb icing can occur with temperatures as high 30°C and humidity as low as 50%, but it is more likely when below 20°C and high humidity, especially during low power settings.

Basic Empty Mass (BEM) is the mass of the aircraft with the basic equipment, unconsumable fluids and unusable fuel and oil.

Battery power to the starter motors.

For every 1kg of air passing through the combustion chamber, 11kg of air pass bypass the combustion chamber.

When rolling the aircraft the up-going wing will experience more drag than the down-going wing. This will result in a yawing moment that directly opposes the desired direction of turn. (i.e.: rolling left will cause a right yaw.)

The track changes constantly.

TAS will increase.

None. The go around procedure is distinct from the take off procedure. You will still have an acceleration altitude, but you will not have a screen height, V1, Vr, V2, flap retraction altitude, etc.

They provide at least 1000ft clearance over obstacles within 25NM of the homing facility.