Key factors that affect airplane takeoff speed (sometimes referred to as its rotation speed) include: direction of airflow, the airplane's shape (especially its wings), the airplane's size, and its weight.
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Maximum permissible takeoff weight or regulated takeoff weight, varies according to flap setting, altitude, air temperature, length of runway and other factors. It is different from one takeoff to the next, but can never be higher than the MTOW.
Flying in high density altitude conditionsFor pilots, high density altitude results in increased takeoff distance, reduced rate of climb, and increased landing roll distance. Failure to plan for these adjustments can result in an accident.
Pressure, temperature, and humidity have a great influence on aircraft performance because of their effect upon density. There is no rule-of-thumb or chart used to compute the effects of humidity on density altitude, but it must be taken into consideration.
The ground effect is particularly beneficial for takeoffs because of its ability to reduce stall speed. Airplanes can stall if they are unable to produce a sufficient amount of lift. Because the ground effect involves an increase in lift, its ability to reduce stall speed.
Zero fuel weight refers to the maximum certified aircraft weight prior to useable fuel being added. Useful load is the weight of the crew, passengers, baggage, usable fuel, and drainable oil. Generally, this can be found by subtracting the basic empty weight from the maximum allowable gross weight.
If you haven't reached 70% of your takeoff speed by the time you've reached 50% of the length of the runway, you should abort your takeoff. You should always use your takeoff performance charts to make sure you have enough runway for a safe takeoff.
A headwind reduces the takeoff ground roll, allowing for shorter runway lengths, and reduces wear on the tires. Similarly, for landing, a headwind lowers the groundspeed at touchdown, shortening the distance required to stop, and reduces tire wear.