Twin Engine • Cessna • 414 (normally aspirated), 414A (pressurized), 414A II (improved avionics), T414A (turbocharged)
| Manufacturer | Cessna |
| Model | 414 Chancellor |
| Category | Twin Engine |
| Variants | 414 (normally aspirated), 414A (pressurized), 414A II (improved avionics), T414A (turbocharged) |
| Production Years | 1970 – 1985 |
| Seating | 6, 7, 8 seats |
| Typical TTAF | 4,200 hours |
| Markets | United States, Canada, Australia, Germany, France |
| Price Range | $125K – $450K |
The Cessna 414 Chancellor is a twin-engine, low-wing monoplane designed for business travel, personal transportation, and light cargo operations. Introduced in 1970, it represents a significant step up from single-engine aircraft, offering greater payload capacity, reliability through redundancy, and enhanced performance capabilities. The aircraft features pressurization in later models, allowing operations at higher altitudes to avoid weather and achieve better fuel efficiency. The 414 is equipped with two Continental IO-520 engines, providing robust power and dependable performance across various operational environments. Known for its spacious cabin, the Chancellor accommodates 6-8 occupants depending on configuration, making it popular among small charter operators, corporate flight departments, and affluent private owners. The aircraft gained recognition for its stability, ease of handling, and relatively forgiving characteristics, even for pilots transitioning from single-engine aircraft. Its construction quality and longevity have made it a staple in the general aviation market, with many examples remaining in active service decades after manufacture. The 414 established itself as a practical workhorse for missions requiring twin-engine performance without the operational complexity of larger twin-engine aircraft.
Maximum Speed: 235 mph
Cruise Speed: 202 mph
Range: 1,635 nautical miles
Service Ceiling: 20,000 feet (414A pressurized: 24,000 feet)
Engines: 2x Continental IO-520-C (310 hp each)
Maximum Takeoff Weight: 6,000 lbs
Empty Weight: 4,065 lbs
Fuel Capacity: 102 gallons
Rate of Climb: 1,560 feet per minute (single engine: 300 fpm)