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Encyclopedia - Cessna 303 Crusader
The Cessna Model 303 Clipper was first flown on 14 February 1978. It was a four-seat low-wing monoplane with retractable tricycle type undercarriage and swept vertical tail surfaces. Cessna superseded this model with the Model T303, which was a six-seater and became known as the Crusader. It had a high set tailplane and counter-rotating propellers.
The Crusader received its certification in August 1981, with first deliveries following in October. By the end of production in 1986 a total of 297 Crusaders had been delivered.
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Cessna T303 Crusader | Powerplant | | Number Of Engines : | Two | | Powerplant type : | Continental TSIO-520-AE and Continental LTSIO-520-AE turbocharged counter-rotating flat-six piston engines | | Max Power Rating : | 186kW (250hp) | Dimensions | | Length : | 9.27m (30ft 5in) | | Height : | 4.06m (13ft 4in) | | Wingspan : | 11.90m (39ft 0.5in) | | Wing Area : | 17.58m2 (189.20sq ft) | Weights | | Empty Weight : | 1,499kg (3,305lb) | | Max Take-off Weight : | 2,336kg (5,150lb) | Landing Gear | | Type : | Retractable tricycle type with a single wheel on each unit
| Performance | | Max Speed At Cruising Level : | 216kt (400km/h; 248mph) | | Cruising Speed : | 196kt (363km/h; 225 mph) | | Maximum Range : | 1,020nm (1,889km; 1,174nm) | | Service Ceiling : | 25,000ft (7,620m) |
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