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English: Landing gear of an aircraft, schematic view of the retracting mechanism. Filled circles are fixed relative to the airframe. Coloured arcs denote the locus of points. 1 Hydraulic Ram 2 Hinge Mechanism 3 Strut 4 Wheel Boss 5 Wheel . 6 Fuselage/Wing
Aircraft Wheels and Configuration Nose section Center section Example 717, 727, 737: 6 wheels [1x2]+[2x2] A Boeing 737 from Southwest Airlines: 747: 18 wheels [1x2]+[4x4] A Boeing 747-400's main landing gear. Note the toes-up bias angle of the bogies on the wing gear, to ensure correct stowage upon retraction: 707, 720, 757, 767, 787: 10 wheels ...
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.
A Cessna 150 converted to taildragger configuration by installation of an aftermarket modification kit. Conventional landing gear, or tailwheel-type landing gear, is an aircraft undercarriage consisting of two main wheels forward of the center of gravity and a small wheel or skid to support the tail.
The Wilga 32 was an improved small-series export variant of the type, powered by a Continental flat engine, which was also locally produced in Indonesia as the "Gelatik". ". After completing an initial batch of 13 Wilga 3s, there were some improvements made to the model, most notably the landing gear base being increased from 2.12 to 2.83 m (7.0 to 9.3 ft) to improve stability during takeoff r
The PA-17 Vagabond version features dual controls, enabling it to be used for pilot training. It has a bungee cord shock-absorbed landing gear (solid gear on the PA-15), and a 65 hp (48 kW) Continental A-65 engine. [1] There was a small increase in climb rate and useful load over the PA-15, despite an increase in empty weight. [5]
Data from Jane's All the World's Aircraft, 1988–1989 General characteristics Crew: 2 Capacity: 19 passengers Length: 47 ft 1.75 in (14.3701 m) Wingspan: 52 ft 0 in (15.85 m) Height: 17 ft 5.5 in (5.321 m) Wing area: 271 sq ft (25.2 m 2) Airfoil: root: NACA 63A418 ; tip: NACA 63A412 Empty weight: 9,613 lb (4,360 kg) Max takeoff weight: 15,332 lb (6,954 kg) Powerplant: 2 × Garrett TPE331-10UG ...
The aircraft was designed in 1958 by the Nanchang Aircraft Factory (now Hongdu Aviation). As the Shenyang Aircraft Factory already had experience building the Shenyang JJ-1 begun technical research for the CJ-6, more than 20 Shenyang designers were transferred to Nanchang, including chief designers Tu Jida and Lin Jiahua. [ 2 ]