Cessna 421 Golden Eagle
Overview
The Cessna 421 Golden Eagle is a general aviation aircraft manufactured by Cessna, with the profile centered on its personal/training/utility role. It first flew in 1967-05 and entered service in 1968. Production is recorded as ending in 1985. The listed configuration provides for a crew of 1 and passenger capacity of 9. Power is provided by 2 Continental GTSIO-520 engines. Recorded dimensions include length 36 ft 10 in, wingspan 41 ft 2 in, height 11.5 ft. Maximum takeoff weight is listed as 7450. Listed performance includes cruise speed 240 kt, maximum speed 256 kt, range 1487 nautical miles, service ceiling 30200 ft. Its ICAO type designator is C421. Figures shown here describe the listed type or configuration and may vary by sub-variant, certification basis, or operator fit.
Quick Facts
Specifications
| ICAO Type Code | C421 |
|---|---|
| First Flight | May 1967 |
| Introduction Date | 1968 |
| Crew | 1 |
| Passenger Capacity | 9 |
| Length | 36 ft 10 in |
| Wingspan / Rotor Diameter | 41 ft 2 in |
| Height | 11.5 ft |
| Empty Weight | 4501 lb |
| Max Takeoff Weight | 7450 lb |
| Cruise Speed | 240 kt |
| Max Speed | 256 kt |
| Range | 1487 nm |
| Service Ceiling | 30200 ft |
| Engine Manufacturer | Continental |
| Engine Model | GTSIO-520 |
| Engine Count | 2 |
Data verification status: Partially Verified
Source: AOPA - Cessna 421 Golden Eagle