Cessna 421 Golden Eagle Private Charter Flights and Prices
The Cessna 421 Golden Eagle is a development of the earlier Cessna 411 light, twin-engine personal transport aircraft. The main difference between the two models is that the 421 is pressurized. The 421 was first produced in May 1967. The 421A appeared in 1968 and the aircraft was redesigned in 1970 and marketed as the 421B. In 1975 the 421C appeared which featured wet wings, the absence of wing tip fuel tanks and landing gear that was changed from straight-leg to a trailing-link design. Production ended in 1985 after 1901 had been delivered.
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Aircraft Size
| Aircraft Size | English | Metric |
|---|---|---|
| Length | 36.38 ft | 11.09 m |
| Wing Span | 41.11 ft | 12.53 m |
| Height | 11.45 ft | 3.49 m |
| Bag. Capacity | 82 ft³ | 2 m³ |
Cabin Size
| Cabin Size | English | Metric |
|---|---|---|
| Length | 7.80 ft | 2.38 m |
| Width | 4.50 ft | 1.37 m |
| Height | 4.10 ft | 1.25 m |
| Area | 144 ft³ | 4 m³ |
Aircraft Seats
| Layout | Seats |
|---|---|
| Max Seating | 8 |
| Typical Seating | 6 |
| Pilots | 2 |
Average Prices
| Costs | USD | EUR |
|---|---|---|
| Purchase New | - | - |
| Purchase Used | - | - |
| Charter Rate | 1,500 USD/hour | 1,500 EUR/hour |
Performance Specifications
| Performance | English | Metric |
|---|---|---|
| IFR Range | 1,486 nm | 2,752 km |
| Cruise Speed | 240 KTAS | 444 km/h |
| Certified Ceiling | 30,200 ft | 9,205 m |
| Rate of Climb | 1,940 ft/m | 591 m/m |
| Takeoff Distance | 2,323 ft | 708 m |
| Landing Distance | 2,293 ft | 699 m |
| Max Takeoff Weight | 7,450 lbs | 3,379 kg |
| Max Landing Weight | 7,200 lbs | 3,266 kg |
| Useful Weight | 1,750 lbs | 794 kg |
| Payload with Full Fuel | - lbs | - kg |
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