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The Cessna 172 Skyhawk is an American four-seat, single-engine, high wing, fixed-wing aircraft made by the Cessna Aircraft Company. [2] First flown in 1955, [2] more 172s have been built than any other aircraft. [3] It was developed from the 1948 Cessna 170 but with tricycle landing gear rather than conventional landing gear.
The fuel economy in aircraft is the ... rising fuel prices coupled with the ... 9.19 km/kg or 13.6 L/100 km in a four-seat diesel-powered Cessna 182 for ...
Data from Global Security [better source needed] General characteristics Crew: one Capacity: three passengers Length: 26 ft 11 in (8.20 m) Wingspan: 35 ft 10 in (10.92 m) Height: 8 ft 10 in (2.69 m) Wing area: 159 sq ft (14.8 m 2) Empty weight: 1,363 lb (618 kg) Gross weight: 2,500 lb (1,134 kg) Powerplant: 1 × Continental IO-360-D 6-cylinder air-cooled horizontally-opposed piston engine, 210 ...
The O-320 family of engines includes the carbureted O-320, the fuel-injected IO-320, the inverted mount, fuel-injected AIO-320 and the aerobatic, fuel-injected AEIO-320 series. The LIO-320 is a "left-handed" version with the crankshaft rotating in the opposite direction for use on twin-engined aircraft to eliminate the critical engine .
The fuel consumption per mile or per kilometre is a more appropriate comparison for aircraft that travel at very different speeds. [citation needed] There also exists power-specific fuel consumption, which equals the thrust-specific fuel consumption divided by speed. It can have units of pounds per hour per horsepower.
An aircraft's gross weight will decrease during a flight due to fuel and oil consumption. An aircraft's gross weight may also vary during a flight due to payload dropping or in-flight refuelling . At the moment of releasing its brakes, the gross weight of an aircraft is equal to its takeoff weight.
With a fuel fraction of nearly 85%, the GlobalFlyer could carry 5 times its weight in fuel.. In aerospace engineering, an aircraft's fuel fraction, fuel weight fraction, [1] or a spacecraft's propellant fraction, is the weight of the fuel or propellant divided by the gross take-off weight of the craft (including propellant): [2]
The main petroleum component used in blending avgas is alkylate, which is a mixture of various isooctanes. Some refineries also use reformate.All grades of avgas that meet CAN 2–3 [further explanation needed], 25-M82 [further explanation needed] have a density of 6.01 pounds per US gallon (720 g/L) at 15 °C (59 °F).