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The Cessna 172 Skyhawk is an American four-seat, single-engine, ... (222 km/h) on 20 hp (15 kW) less. It had a useful load that was about 100 lb (45 kg) more than the ...
Used in the Cessna 172 I to M models. O-320-E2F 150 hp (112 kW) at 2700 rpm, Minimum fuel grade 80/87 avgas, compression ratio 7.00:1. Same as E1F but with fixed pitch prop provisions. [4] O-320-E2G 150 hp (112 kW) at 2700 rpm, Minimum fuel grade 80/87 avgas, compression ratio 7.00:1. Same as E2D but with O-320-A sump and intake pipes. [4] O ...
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
The aircraft is basically a Cessna 180 with a strengthened fuselage. The main difference between the two aircraft is the larger vertical fin on the 185 and the 300 hp (224 kW) Continental IO-520-D engine as opposed to the 230 hp (172 kW) Continental O-470-S fitted to the Cessna 180. The exception was that a Continental Motors IO-470-F engine of ...
The 175 was designed to fill a niche between the Cessna 172 and the slightly heavier, larger and faster Cessna 182.The engine of the 175, a reduction drive or geared version of the O-300 (Continental GO-300) used in the 172, is rated at 175 hp (130 kW), or 30 hp (22 kW) more than the engine offered in the contemporary 172.
For this reason, the useful load fraction calculates a similar number, but it is based on the combined weight of the payload and fuel together in relation to the total weight. Propeller-driven airliners had useful load fractions on the order of 25–35%. Modern jet airliners have considerably higher useful load fractions, on the order of 45–55%.
Cessna never offered a civil model directly analogous to these aircraft, but Cessna licensee Reims Aviation in France sold similar IO-360-powered models as the R172 Rocket and Hawk XP. [10] T-41A United States Air Force version of the Cessna 172F, 172G, and 172H for undergraduate pilot training, powered by 145 hp Continental O-300.
Data from Tecnam General characteristics Crew: 1 or 2 Capacity: 9 passenger seats / 1,414 kg (3,117 lb) useful load including fuel Length: 11.8 m (38 ft 9 in) Wingspan: 14 m (45 ft 11 in) ; 16.6 m (54 ft) on STOL variant Height: 4.4 m (14 ft 5 in) Wing area: 25.4 m 2 (273 sq ft) Aspect ratio: 7.7 Empty weight: 2,386 kg (5,260 lb) ; 2,416 kg (5,326 lb) on STOL variant Max takeoff weight: 3,680 ...
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