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The maximum landing weight (MLW), also known as the maximum structural landing weight or maximum structural landing mass, [1] is the maximum aircraft gross weight due to design or operational limitations at which an aircraft is permitted to land. The MLW is set in order to ensure safe landings; if an aircraft weighs too heavy during touchdown ...
This is a list of aircraft sorted by maximum takeoff ... MTOW = Maximum take-off weight, MLW = Maximum landing weight, TOR = Take-off run (SL, ISA+15°, MTOW), LR ...
The aircraft gross weight (also known as the all-up weight and abbreviated AUW) is the total aircraft weight at any moment during the flight or ground operation. [ 1 ] [ 2 ] [ 3 ] An aircraft's gross weight will decrease during a flight due to fuel and oil consumption.
[32] [33] [34] Both the earlier and later takeoff weights establish the An-225 as the world's heaviest aircraft, exceeding the weight of the double-deck Airbus A380 airliner. Airbus claims to have improved upon the An-225's maximum landing weight by landing an A380 at 591.7 t (652.2 short tons) during testing. [35] [a]
The aircraft were handed over to the Air Force in 2010. Six PC-12s are in service with the Finnish Air Force. ... Maximum landing weight: 4,500 kg (9,921 lb)
Two-place, fixed landing gear landplane, Lycoming O-320-E2A or -E3D engine of 150 hp (112 kW), gross weight 1,950 lb (885 kg). First certified on 14 February 1964. Approved as a 2,150 lb (975 kg) gross weight four place aircraft on 17 June 1965. [19] Built in the following variants: PA-26-140 Cherokee, initial version. [35]
The weight of an aircraft is the primary factor that determines the landing distance required by an aircraft. An increase in weight increases the stall speed of the aircraft. Therefore, the landing approach speed increases as the aircraft's weight increases. The kinetic energy ( 1 / 2 mV 2) that has to be dissipated to stop an aircraft ...
The oxygen, cabin pressurization, landing gear control, aircraft health and trend monitoring systems are adapted from the G650. [43] The auxiliary power unit is a Honeywell HTG400G. [41] The cabin pressurization reaches 10.69 psi (0.737 bar). [44]