Cessna 303 Crusader
Overview
The Cessna 303 Crusader is a general aviation aircraft manufactured by Cessna, with the profile centered on its general aviation role. It first flew in 1978 and entered service in 1982. Production is recorded as ending in 1984. The listed configuration provides for a crew of 1 and passenger capacity of 5. Power is provided by 2 Continental TSIO-520 engines. Recorded dimensions include length 30.4 ft, wingspan 39 ft, height 13.3 ft. Maximum takeoff weight is listed as 5,150 lb. Its ICAO type designator is C303. Figures shown here describe the listed type or configuration and may vary by sub-variant, certification basis, or operator fit.
Quick Facts
First Flight
1978
Crew
1
Passengers
5
Specifications
| ICAO Type Code | C303 |
|---|---|
| First Flight | 1978 |
| Introduction Date | 1982 |
| Crew | 1 |
| Passenger Capacity | 5 |
| Length | 30.4 ft |
| Wingspan / Rotor Diameter | 39 ft |
| Height | 13.3 ft |
| Empty Weight | 3200 lb |
| Max Takeoff Weight | 5,150 lb |
| Engine Manufacturer | Continental |
| Engine Model | TSIO-520 |
| Engine Count | 2 |
Data verification status: Partially Verified