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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 ...
Type MTOW [kg] MLW [tonnes] TOR [m] LR [m] ICAO category FAA category; Antonov An-225: 640,000: 591.7: 3,500: Super: Super Scaled Composites Model 351 Stratolaunch
The structural weight limits are based on aircraft maximum structural capability and define the envelope for the CG charts (both maximum weight and CG limits). An aircraft's structural weight capability is typically a function of when the aircraft was manufactured, and in some cases, old aircraft can have their structural weight capability ...
When the weight of the aircraft is at or below the allowable limit(s) for its configuration (parked, ground movement, take-off, landing, etc.) and its center of gravity is within the allowable range, and both will remain so for the duration of the flight, the aircraft is said to be within weight and balance. Different maximum weights may be ...
ACNs depend on the landing gear geometry (number of wheels and wheel spacing), the landing gear load (that is dependent upon the aircraft weight and center of gravity) and the tire pressure. Normally, the aftmost center of gravity for the Maximum Ramp Weight (MRW) lead to the critical ACN.
Data from Jane's All The World's Aircraft 1988-89 General characteristics Crew: 2 pilots and 1 flight attendant Capacity: 30 passengers Length: 20 m (65 ft 7 in) Wingspan: 19.78 m (64 ft 11 in) Height: 6.35 m (20 ft 10 in) Wing area: 39.4 m 2 (424 sq ft) Airfoil: root: NACA 23018 mod. ; tip: NACA 23012 Empty weight: 7,070 kg (15,587 lb) Max takeoff weight: 11,990 kg (26,433 lb) (ER) Maximum ...
The Monarch Butterfly has a very low 0.168 kg/m 2 wing loading The McDonnell Douglas MD-11 has a high 837 kg/m 2 maximum wing loading. In aerodynamics, wing loading is the total weight of an aircraft or flying animal divided by the area of its wing.
MEDIUM aircraft landing behind HEAVY aircraft — 2 minutes; LIGHT aircraft landing behind SUPER aircraft — 4 minutes; LIGHT aircraft landing behind HEAVY or MEDIUM aircraft — 3 minutes; For departing aircraft, time-based separation minima are more complicated and depend on the runways used, but range from 2 minutes to 4 minutes. [2]