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The Cessna 180 Skywagon is a four- or six-seat, fixed conventional gear general aviation airplane which was produced between 1953 and 1981. Though the design is no longer in production, many of these aircraft are still in use as personal aircraft and in utility roles such as bush flying .
Cessna 525: 1991 2,000+ Twin jet engine monoplane business airplane Cessna 526 CitationJet: 1993 2 Twin jet engine monoplane trainer Cessna E530: 2013 4 Twin jet engine monoplane trainer Cessna 550 Citation II: 1977 Twin jet engine monoplane business airplane Cessna 551 Citation II/SP: 94 [3] Twin jet engine monoplane business airplane Cessna ...
The Cessna Skymaster is an American twin-engine civil utility aircraft built in a push-pull configuration. Its engines are mounted in the nose and rear of its pod-style fuselage. Twin booms extend aft of the wings to the vertical stabilizers , with the rear engine between them.
Media in category "Images of Cessna aircraft" This category contains only the following file. Cessna177BCardinal02.jpg 350 × 247; ...
The Model 526 CitationJet was a twin-engine, two-seat tandem military trainer developed from the Model 525 as a candidate for the Joint Primary Aircraft Training System competition (JPATS). The two models share 75% of their parts, including wing, engines, landing gear, and other systems.
A 180 degree straight-twin engine has a secondary imbalance (similar to an inline-four engine); however, the lower reciprocating mass means that this often does not require treatment. A 180° crankshaft engine suffers fewer pumping losses than a 360° twin, because displacement of the crankcase is relatively unchanged as the pistons move.
The Cessna 310 is an American four-to-six-seat, low-wing, twin-engine monoplane produced by Cessna between 1954 and 1980. It was the second twin-engine aircraft that Cessna put into production; the first was the Cessna T-50. [1] It was used by the U.S. military as the L-27, after 1962, U-3. Over six thousand Cessna 310 and 320 aircraft were ...
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 ...