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The Cessna 172 Skyhawk is an ... but resumed in 1996 with the 160 hp (120 kW) Cessna 172R Skyhawk. ... or enhanced landing and takeoff performance and safety with ...
160 hp (119 kW) at 2700 rpm, Minimum fuel grade 100/130 or 91/96 avgas, compression ratio 8.50:1. Same as B1A but with straight riser in oil sump and -32 carburetor. [4] O-320-B2A 160 hp (119 kW) at 2700 rpm, Minimum fuel grade 100/130 or 91/96 avgas, compression ratio 8.50:1. Same as B1A but with fixed-pitch propeller provisions. [4] O-320-B2B
Engines in the O-360 series produce between 145 and 225 hp (110 and 170 kW), with the basic O-360 producing 180 hp (130 kW). [1] The engine family has been installed in thousands of aircraft, including the Cessna 172, Piper Cherokee/Archer, Grumman Tiger, and many home-built types.
Single engine piston taildragger aircraft [1]; Model Engine Power hp Seats Wing Sq. Ft. MTOW lb Empty lb Cruise knots Range nmi American Champion Citabria: L. O-235/320/360: 118-180: 2: 165-172 ...
Cessna thought that a less expensive four-seater aircraft than the existing Cessna 172 would have good market potential. The company designed a simplified four-seat high-wing aircraft using non-tapering wings, extensive use of heavily beaded wing and fuselage skins as well as free-castering nose gear to save weight and decrease the man-hours required for construction.
220 hp (164 kW) at 2600 rpm, Minimum fuel grade 100 or 100LL avgas, RH95/130 or B95/130 CIS, compression ratio 7.50:1. Same as the TSIO-360-KB except the manifold pressure is controlled with a wastegate controller, an intercooler is installed in the induction system, and uses a Precision Airmotive RSA-5AD2 fuel injection servo.
With the use of the Lycoming O-320 at 150–160 hp, the Cub's allowable gross weight increased to 1,750 lb while retaining the capability of a mere 200 feet (61 m) required for takeoff. The PA-18 has developed a very dedicated following in the bush-flying community, and many modifications have been developed for it, to the point where it is ...
Certified four-cylinder, fuel-injected, horizontally opposed, air-cooled direct drive, 390 cubic inches (6.39 litres), 215 hp (160 kW) at 2,700 rpm, dry weight 296 lb (134 kg). This model is the same as the C3A6, except that the propeller governor is located on left front of the crankcase. Used on Cirrus SR20 G6. [6] [11]
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