BEECHCRAFT 35-C33
The Beechcraft 35-C33 Debonair is a four-seat, single-engine aircraft with a conventional tail and either a 225 hp (IO-470J) or 285 hp (IO-520B) engine, depending on the specific model year. Key specifications include a cruise speed of about 174 KIAS, a max takeoff weight of 3,300 lbs (for the C33A), a service ceiling of up to 18,300 ft, and a range of approximately 520 NM.
| Specification | C33 (1965-1967) | C33A (1966-1967) |
|---|---|---|
| Engine | Continental IO-470J (225 hp) | Continental IO-520-B (285 hp) |
| Wingspan | 32 ft 10 in | 32 ft 10 in |
| Length | 26 ft 8 in | 26 ft 8 in |
| Height | 8 ft 3 in | 8 ft 3 in |
| Max Takeoff Weight | 3,050 lbs | 3,300 lbs |
| Fuel Capacity | 74 gallons | 74 gallons |
| Empty Weight | 1,854 lbs | 1,775 lbs |
| Crew + Passengers | 1 + 4 | 1 + 4 |
| Best Cruise Speed | 161 kts | 174 KIAS |
| Stall Speed | 52 knots | 53 KIAS |
| Max Altitude | 18,400 ft | 18,300 ft |
| Rate of Climb | 960 fpm | 1,200 fpm |
| Takeoff Distance | 982 ft | 880 ft |
| Landing Distance | 643 ft | 632 ft |
| Range | 1140 nm (max) | 520 NM |