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.

Aircraft Size

Cabin Size

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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