Single-engine pistonutility aircraft model by Cessna
Cessna T303 Crusader
The Cessna T303 Crusader is an American six-place light twin-engined aircraft built by Cessna Aircraft Company. Production ceased in 1986.
Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.
- Manufacturer
- Cessna
- Category
- Single-engine piston
- First flight
- 1978-02-14
- Length
- 9.27 m
- Wingspan
- 11.48 m
Specifications
- Cruise speed
- 196 kt
- Max speed
- 216 kt
- Range
- 1,020 nm
- Service ceiling
- 25,000 ft
- Rate of climb
- 1,480 ft/min
- Max takeoff weight
- 5,150 lb
- Empty weight
- 3,305 lb
- Fuel capacity
- 153 US gal
- Powerplant
- 2 × Continental TSIO-520-AE/LTSIO-520-AE turbocharged air-cooled flat-six piston engine
- Engines
- 2
- Seats
- 6
- Length
- 30.4 ft
- Wingspan
- 39 ft
- Height
- 13.3 ft
- Number built
- 297
Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).
Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.