Cessna 401
Overview
The Cessna 401 is a general aviation aircraft manufactured by Cessna, with the profile centered on its personal/training/utility role. It first flew in 1965 and entered service in 1967. Production is recorded as ending in 1972. The listed configuration provides for a crew of 1 and passenger capacity of 7. Power is provided by 2 Continental IO-520 engines. Recorded dimensions include length 36 ft 1 in, wingspan 39 ft 11 in, height 11 ft 4 in. Maximum takeoff weight is listed as 6300. Listed performance includes cruise speed 198 mph kt. Its ICAO type designator is C401. 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 | C401 |
|---|---|
| First Flight | 1965 |
| Introduction Date | 1967 |
| Crew | 1 |
| Passenger Capacity | 7 |
| Length | 36 ft 1 in |
| Wingspan / Rotor Diameter | 39 ft 11 in |
| Height | 11 ft 4 in |
| Empty Weight | 4000 lb |
| Max Takeoff Weight | 6300 lb |
| Cruise Speed | 198 mph |
| Engine Manufacturer | Continental |
| Engine Model | IO-520 |
| Engine Count | 2 |
Data verification status: Partially Verified
Source: Wikipedia - Cessna 400 series