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The landing gear represents 2.5 to 5% of the maximum takeoff weight (MTOW) and 1.5 to 1.75% of the aircraft cost, but 20% of the airframe direct maintenance cost. A suitably-designed wheel can support 30 t (66,000 lb), tolerate a ground speed of 300 km/h and roll a distance of 500,000 km (310,000 mi) ; it has a 20,000 hours time between overhaul and a 60,000 hours or 20 year life time.
14 wheels, 7 axles The Antonov An-225 's main landing gear (consisting of two 14-wheel bogies) The tables below show how various types of wheeled units are arranged to form the undercarriages of some popular aircraft from manufacturers Antonov , Airbus , and Boeing .
The aircraft features a cable-braced hang glider-style high-wing, weight-shift controls, a two-seats-in-tandem open cockpit with a cockpit fairing, tricycle landing gear with wheel pants and a single engine in pusher configuration. [1] The aircraft is made from welded stainless steel tubing, with its double surface wing covered in Dacron sailcloth.
An F/A-18 taking off from an aircraft carrier An Embraer E175 taking off. Takeoff is the phase of flight in which an aerospace vehicle leaves the ground and becomes airborne. For aircraft traveling vertically, this is known as liftoff.
Normal landings are done by touching all three wheels down at the same time in a three-point landing. This method does allow the shortest landing distance but can be difficult to carry out in crosswinds, [6] as rudder control may be reduced severely before the tailwheel can become effective. [citation needed] The alternative is the wheel landing.
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