Aircraft Maximum Gross Takeoff Weight MGTOW

Aircraft Maximum Gross Takeoff Weight MGTOWAircraft Maximum Gross Takeoff Weight MGTOWIn the FAAs Handbook of Aeronautical Knowledge, Maximum Takeoff Weight is defined as the maximum allowable weight for takeoff. More specifically, the maximum takeoff weight is a limitation placed on the aircraft by the aircraft manufacturer during the design and testing process. Its a fixed weight. Industry Jargon In aviation, MTOW is short for Maximum Takeoff Weight. Sometimes people refer to this weight as MGTOWor Maximum Gross Takeoff Weight. These two terms are interchangeable. More rarely, this weight can be referred to as Maximum Brake Release Weight. MTOW or MGTOW should notlage be confused with the Maximum Gross Weight of the aircraft itself, which is the maximum weight an aircraft can structurally handle, whether taking off or sitting on the ramp. The Maximum Gross Weight for an aircraft should never be exceeded at any time. MTOW can sometimes be exceeded, but not usually by a signifi cant amount. For example, an aircraft can exceed MTOW when sitting on the ramp but must get rid of this weight before its brakes are released on the departure runway. Since the aircraft will burn fuel during the startup and taxi, its possible that it will weigh slightly more upon startup than during takeoff. Importance Due to structural limitations, an aircraft is restricted to a certain weight while taking off. If this weight is exceeded, the aircraft may become structurally damaged, or worse, fail to complete a successful takeoff altogether. Aircraft designers and manufacturers know the importance of MTOW. To their customers, a higher MTOW means an airplane can take off with more fuel and will have a longer range. Use Caution Its important to note that just because an aircraft is certified for a particular Maximum Takeoff Weight doesnt mean that the aircraft can always take off at this maximum weight. Many individual factors are to be considered for an aircraft to be dete rmined safe to take off at a particular weight. A pilot needs to compute takeoff and climb performance, which is largely dependent on other variables like the following Elevation The higher the field elevation, the thinner the air is. An airplane will have a decrease in performance at high altitudes, which means a full payload may not be possible.Temperature High temperatures also decrease aircraft performance, and can require a lighter load.Density altitude The higher the density altitude, which is pressure altitude corrected for nonstandard temperature, the worse the aircraft performance.Runway length and surface An aircraft loaded to its maximum takeoff weight may require a long runway, and the same aircraft may not be able to take off on a shorter runway under certain conditions. Runway gradient An up-sloping runway will require a longer takeoff distance than a down-sloping or flat runway, and should be taken into consideration with a heavy aircraft.Wind strength A headwind aids takeoff performance a tailwind degrades it.Obstacles during departure Extremely heavy aircraft wont have a very good climb rate therefore, its especially important to calculate the climb gradient and rate for aircraft at the particular takeoff weight. A required climb gradient to overcome obstacles may not be possible in a very heavy aircraft.