Cessna 402
Overview
The Cessna 402 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 1985. The listed configuration provides for a crew of 1 and passenger capacity of 8. Power is provided by 2 Continental TSIO-520 engines. Recorded dimensions include length 36 ft 4 in, wingspan 44 ft 2 in, height 11 ft 6 in. Maximum takeoff weight is listed as 6850. Listed performance includes cruise speed 198 mph kt. Its ICAO type designator is C402. 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 | C402 |
|---|---|
| First Flight | 1965 |
| Introduction Date | 1967 |
| Crew | 1 |
| Passenger Capacity | 8 |
| Length | 36 ft 4 in |
| Wingspan / Rotor Diameter | 44 ft 2 in |
| Height | 11 ft 6 in |
| Empty Weight | 4300 lb |
| Max Takeoff Weight | 6850 lb |
| Cruise Speed | 198 mph |
| Engine Manufacturer | Continental |
| Engine Model | TSIO-520 |
| Engine Count | 2 |
Data verification status: Partially Verified
Source: Wikipedia - Cessna 400 series