Ad
related to: 180 hp cessna 172 performance specs
Search results
Results from the WOW.Com Content Network
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.
The 1954 model year introduced a 225 hp (168 kW) O-470-J engine and interior refinements. 1956 introduced a 230 hp (172 kW) O-470-K engine with a new air intake duct. Certified on 23 December 1952. 641 (1953), 620 (1954), 891 (1955), and 512 (1956) built. [5] [6] A 1957 Cessna on display at Hullavington Airfield, England. 180A
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.
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
Carburetor-equipped model with a thin wall front main bearing journal crankshaft, for a fixed pitch propeller, and a conical engine mount for a front propeller governor, that produces 180 hp (134 kW) at 2700 rpm, with a compression ratio of 8.5:1 and with a basic dry weight of 291 lb (132 kg). [2] O-360-B1A2
180 hp (134 kW) at 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 9.00:1. Similar to the E1AD except with Bendix D4RN-2200 retard breaker magnetos in place of the Bendix D4RN-2021 impulse coupling magneto. [1] O-360-E2BD 180 hp (134 kW) at 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 9.00:1.
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.
Aviat A-1C-180 Husky. The Husky comes in six versions: [4] Husky A-1 Certified on 1 May 1987. Maximum gross weight is 1,800 lb (816 kg). Powered by a Lycoming 0-360-A1P or a Lycoming O-360-C1G of 180 hp (134 kW) [5] Husky A-1A Certified on 28 January 1998. Maximum gross weight is 1,890 lb (857 kg). Powered by a Lycoming 0-360-A1P of 180 hp (134 ...
Ad
related to: 180 hp cessna 172 performance specs