Single Engine • Cessna • Standard, A (Turbo), Super 207, Turbo 207
| Manufacturer | Cessna |
| Model | 207 |
| Category | Single Engine |
| Variants | Standard, A (Turbo), Super 207, Turbo 207 |
| Production Years | 1969 – 1989 |
| Seating | 6, 7 seats |
| Typical TTAF | 4,200 hours |
| Markets | United States, Canada, Alaska, Australia, New Zealand |
| Price Range | $120K – $680K |
The Cessna 207 is a high-performance, single-engine utility aircraft that evolved from the popular Cessna 206. Introduced in 1969, it features a distinctive "strut-braced" wing design and exceptional payload capacity, making it ideal for bush flying, cargo operations, and remote area access. The aircraft is renowned for its rugged construction, reliability, and ability to operate from unprepared airstrips with minimal facilities. The 207 typically accommodates 6-7 occupants and delivers impressive short-takeoff-and-landing (STOL) performance. Its spacious cabin and large cargo doors make it a preferred choice for operators in Alaska, Canada, and other regions requiring dependable utility aircraft. The Cessna 207 remains highly valued in both commercial and private aviation sectors for its versatility, ease of maintenance, and proven track record in demanding operational environments. Many examples continue flying after 50+ years of service.
Maximum Speed: 170 mph
Cruise Speed: 156 mph
Range: 960 nautical miles
Service Ceiling: 19,750 feet
Engine: Lycoming IO-360 or IO-390 (210-260 hp)
Maximum Takeoff Weight: 3,800 lbs
Useful Load: 1,500 lbs