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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. First flown in 1955, more 172s have been built than any other aircraft. It was developed from the 1948 Cessna 170, using tricycle undercarriage, rather than a tail-dragger configuration.
Top speed: 302 km/h
Range: 1,185 km
Cruise speed: 226 km/h
Wingspan: 11 m
Weight: 757 kg
Engine type: Continental O-300
General characteristics
- Crew: one
- Capacity: three passengers
- Length: 27 ft 2 in (8.28 m)
- Wingspan: 36 ft 1 in (11.00 m)
- Height: 8 ft 11 in (2.72 m)
- Wing area: 174 sq ft (16.2 m2)
- Aspect ratio: 7.32
- Airfoil: modified NACA 2412
- Empty weight: 1,691 lb (767 kg)
- Gross weight: 2,450 lb (1,111 kg)
- Fuel capacity: 56 US gallons (212 litres)
- Powerplant: 1 × Lycoming IO-360-L2A four cylinder, horizontally opposed aircraft engine, 160 hp (120 kW)
- Propellers: 2-bladed metal, fixed pitch
Performance
- Cruise speed: 122 kn (140 mph, 226 km/h)
- Stall speed: 47 kn (54 mph, 87 km/h) (power off, flaps down)[81]
- Never exceed speed: 163 kn (188 mph, 302 km/h) (IAS)[8]
- Range: 696 nmi (801 mi, 1,289 km) with 45 minute reserve, 55% power, at 12,000 ft
- Service ceiling: 13,500 ft (4,100 m)
- Rate of climb: 721 ft/min (3.66 m/s)
- Wing loading: 14.1 lb/sq ft (68.6 kg/m2)
Avionics