Cessna 421 Golden Eagle Private Jet Charter
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 category
Turboprop Aircraft
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Typical Seating
6
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Price per hour
1,850
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Nautical miles
1486
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.
The average hourly rental rate of the Cessna 421 Golden Eagle is around 1,850 USD per hour.
Aircraft Size
Aircraft size | English | Metric |
---|---|---|
Length | 36.38 ft | 11.1 m |
Wing Span | 41.12 ft | 12.52 m |
Height | 11.44 ft | 3.5 m |
Bag. Capacity | 82 ft³ | 2.32 m³ |
Cabin Size
Cabin size | English | Metric |
---|---|---|
Length | 7.8 ft | 2.38 m |
Width | 4.5 ft | 1.38 m |
Height | 4.1 ft | 1.25 m |
Area | 144.08 ft³ | 4.08 m³ |
Aircraft Seats
Layout | Seats |
---|---|
Max Seating | 8 |
Typical Seating | 6 |
Pilots | 2 |
Average Prices
Costs | USD | EUR |
---|---|---|
Purchase New | - | - |
Purchase Used | - | - |
Hourly rate | 1,850 USD/hour | 1,850 EUR/hour |
Performance Specifications
Performance | English | Metric |
---|---|---|
IFR Range | 1486 nm | 2752 km |
Cruise Speed | 240 KTAS | 444 km/h |
Certified Ceiling | 30200 ft | 9205 m |
Rate of Climb | 1940 ft/m | 591 m/m |
Takeoff Distance | 2323 ft | 708 m |
Landing Distance | 2293 ft | 699 m |
Max Takeoff Weight | 7450 lbs | 3379 kg |
Max Landing Weight | 7200 lbs | 3266 kg |
Useful Weight | 1750 lbs | 794 kg |
Payload with Full Fuel | - | - |