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The fuel economy in aircraft is the measure of the transport energy ... 9.19 km/kg or 13.6 L/100 km in a four-seat diesel-powered Cessna 182 for 1,000-1,750 kg ...
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.
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.
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 ...
Cessna Model A: 1927 70 Single piston engine monoplane utility airplane Cessna Model BW: 13 Single piston engine monoplane utility airplane Cessna CG-2: Glider Cessna CH-1: 1953 ~50 Single piston engine utility helicopter Cessna CH-4: Single piston engine utility helicopter Cessna CR-1: 1 Single piston engine monoplane racer Cessna CR-2: 1930 1
This list of light aircraft certified for general aviation that is currently in production ... Cessna 172 Skyhawk L. IO-360/CD-155: 155-180: 4: 174: 2,550: 1,670-1,780:
Continental O-300 engine installation in a Cessna 172. The C-145 was developed from the 125 hp (93 kW) C-125 engine. Both powerplants share the same crankcase, although the C-145 produces an additional 20 hp (15 kW) through a longer piston stroke, higher compression ratio of 7.0:1 and different carburetor jetting.
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 .