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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 [1x2]+[2x4] A Boeing 757-200 from British Airways: 777: 14 wheels [1x2]+[2x6] A Boeing 777-200 from United Airlines.
The C-76 proved severely underpowered from the start, with a cruising speed of 160 mph (260 km/h), a service ceiling of 22,600 feet (6,900 m), a range of only 750 mi (1,210 km), and a cargo capacity of under 8,000 lb (3,600 kg). Colonel J.W. Sessums, a USAAF officer at the Air Materiel Command at Wright Field, later related:
Construction of an RV-10 wing in a garage An RV-10 at the Van's Aircraft display at Sun n Fun 2006 in Lakeland Florida RV10 at EAA Airventure 2014 RV-10 landing. The Van's Aircraft RV-10 is a four-seat, single-engine, low-wing homebuilt airplane sold in kit form by Van's Aircraft.
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.
The Miles & Atwood Special is a single seat, low-wing, open cockpit, racing aircraft with conventional landing gear. It was built by Leon Atwood and Lee Miles. [1] [2] [3] The aircraft uses solid wood spars. Fabric was attached using a relatively new process using screws with fabric tape covering, rather than conventional rib-stitching.
Single engine piston aircraft with tricycle landing gear [1]; Model Engine Power hp Seats Wing Sq. Ft. MTOW lb Empty lb Cruise knots Range nmi AS 202 Bravo NG: L. AEIO-360: 180: 3: 149: 2,202: 1,389
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Data from Van's Aircraft General characteristics Crew: one Capacity: one passenger Length: 21 ft 0 in (6.40 m) Wingspan: 24 ft 0 in (7.32 m) Height: 5 ft 7 in (1.70 m) Wing area: 116 sq ft (10.8 m 2) Empty weight: 1,120 lb (508 kg) Gross weight: 1,800 lb (816 kg) Fuel capacity: 42 U.S. gallons (160 L; 35 imp gal) Powerplant: 1 × Lycoming IO-360 four cylinder, horizontally opposed piston ...
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