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The Cessna 172 may be modified via a wide array of supplemental type certificates (STCs), including increased engine power and higher gross weights. Available STC engine modifications increase power from 180 to 210 hp (134 to 157 kW), add constant-speed propellers, or allow the use of automobile gasoline.
Cessna 172 : June 12, 1955 Cessna 175 : April 23, 1956: Developed from: Cessna 172 Cessna 175 Skylark: ... was a commercial off-the-shelf 172 with few modifications.
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 ...
The case of high-wing configuration wing was different. Full scale testing of a modified Cessna 172 showed that the outboard leading-edge cuff alone was not sufficient to prevent a spin departure, the aircraft lacking directional stability at high angles of attack. With a ventral fin added, the aircraft entered a controlled spiral in lieu of a ...
The Cessna 177 (originally Model 341) [3] was designed in the mid-1960s when the engineers at Cessna were asked to create a "futuristic 1970s successor to the Cessna 172". The resulting aircraft featured newer technology such as a cantilever wing lacking the lift struts of previous models, and a new laminar flow airfoil.
Cessna 172 Skyhawk: 1955 44,000+ Single piston engine monoplane utility airplane Cessna 175 Skylark: 1956 2,106 Single piston engine monoplane utility airplane