CESSNA 172 G1000


The Cessna 172 G1000 is a four-seat, high-wing, single-engine aircraft. The Cessna 172 G1000, manufactured by the Cessna Aircraft Company, is one of the world’s most popular flight training aircraft due to its reliability and the fact that it can be easily adapted by pilots.

Early 172s were almost identical in appearance to the Cessna 170s, with the same fuselage shape and the same tall landing gear legs, although later versions had revised landing gear, a lowered rear deck and an aft window. Cessna advertised this added rear visibility as ‘Omnivision’. The definitive structure, developed by the mid 1970s, consisted of the tail still used today. The airframe has remained almost unchanged since then, with updates mainly affecting avionics and engine fittings, including (especially in 2005) the Garmin G1000 glass cockpit option. Production ended in the mid-1980s, but was resumed in 1996 with the Cessna 172R and Cessna 172SP models with 120 kW (160 hp) and 135 kW (180 hp), respectively.

Early versions were manufactured with a Continental O-300 110 kW (145 hp) engine, while later versions were equipped with Lycoming O-360 135 kW (180 hp) engines, although the O-320 110 or 120 kW versions are more common. In addition, there are a few units equipped with Franklin 164 kW (220 hp) engines.

More specifications: Features and performance
1 pilot
3 passengers
9.3m (27,2ft)
11m (36,1ft)
2.7m (8,9 ft)
Wings Area
16.2m (174,4ft)
Modified NACA 2412
Empty weight
743kg (1.637lb)
Maximum takeoff weight
1.110kg (2.446,4)
Power plant
1 engine of four opposed cylinders cooled by air
118 kW (158HP; 160 CV)

Speed never exceeded (Vne): 302 km / h (188 MPH, 163 kt)
Maximum operating speed (Vno): 228 km / h (142 MPH, 123 kt)
Scope: 1 270 km (686 nmi, 789 mi)
Service ceiling: 4 115 m (13 500 ft)
Ascent regime: 3.7 m / s (720 ft / min)