Search results
Results from the WOW.Com Content Network
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 fuselage is a steel frame covered with ... Max takeoff weight: 3,000 kg (6,614 lb) and max landing ... with max standard fuel; Rate of climb: 3.8 m/s ...
The maximum weight authorised for normal landing of an aircraft. The MLW must not exceed the MTOW. The operation landing weight may be limited to a weight lower than the Maximum Landing Weight by the most restrictive of the following requirements: Aircraft performance requirements for a given altitude and temperature:
Maximum landing weight: 24,500 lb (11,100 kg) Fuel capacity: 1,350 US gal (1,120 imp gal; 5,100 L) maximum internal fuel and 2x 150 US gal (120 imp gal; 570 L) optional drop-tanks Powerplant: 2 × Westinghouse J34-WE-36 turbojet engines, 3,400 lbf (15 kN) thrust each
The airframe is primarily composed of high strength aluminum alloys with limited use of steel and titanium alloys. The horizontal stabilizer, fairings, main landing gear doors, rudder and elevators, radome, rear pressure bulkhead and winglets are composite materials. The semi-monocoque fuselage structure is made of stressed skin, frame and ...
maximum ramp weight: MSA minimum safe altitude / minimum sector altitude MSD Minimum Stabilization Distance MSDS Material Safety Data Sheet MSG Message: MSL mean sea level: MSLW Max. Structural Landing Weight MSP Modes S-Specific Protocol MSSS Mode S-Specific Services MSTOW Max. Structural Take-off Weight MSZFW Max. Structural Zero Fuel Weight MTBF
The Hawker 4000 was certified to FAA FAR Part 25 standards, ... Max Landing Weight: 33,500 lb / 15,195 kg; Payload with full fuel: 2625 lb / 1190 kg; Fuel capacity: ...