Credit
Rijkswaterstaat · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
402C Businessliner · Length
Single source36 ft 4 + 1 ⁄ 2 in (11.09 m)[source]
SR20-G3 · Length
Single sourceConfiguration
| Specification | Cessna 402 | Cirrus SR20 |
|---|---|---|
| Type | Corporate transport and airliner[source] | Light aircraft[source] |
| National origin | United States[source] | United States[source] |
| Manufacturer | Cessna[source] | Cirrus Aircraft[source] |
| Status | In service[source] | — |
26 ft 0 in (7.92 m)[source]
Cruise; 402C Businessliner · at 10,000 ft (3,000 m) (econ cruise)
Single sourceMaximum; 402C Businessliner · at 16,000 ft (4,900 m)
Single source231 kn (266 mph, 428 km/h) at 16,000 ft (4,900 m)[source]
142 kn (163 mph, 263 km/h) at 10,000 ft (3,000 m) (econ cruise)[source]
Cruise; SR20-G3 · TAS
Single source155 kn (178 mph, 287 km/h) TAS[source]
402C Businessliner · at 10,000 ft (3,000 m), econ cruise
Single source1,273 nmi (1,465 mi, 2,358 km) at 10,000 ft (3,000 m), econ cruise[source]
402C Businessliner · 2 × Continental TSIO-520-VB air-cooled turbocharged flat-six engines each
Single source2 × Continental TSIO-520-VB air-cooled turbocharged flat-six engines, 325 hp (242 kW) each[source]
SR20-G3 · 1 × Continental IO-360-ES six cylinder, horizontally-opposed piston aircraft engine
Single source1 × Continental IO-360-ES six cylinder, horizontally-opposed piston aircraft engine , 200 hp (150 kW)[source]
402C Businessliner · Wing area
Single source225.8 sq ft (20.98 m 2 )[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary user |
|---|
Cape Air[source] |
| — |
| Number built | 2,000+[source] | 2,084 (through 2025)[source] |
|---|
| Manufactured | 1966–1985[source] | 1999–present[source] |
|---|
| Introduction date | 1967[source] | — |
|---|
| First flight | August 26, 1965[source] | 21 March 1995[source] |
|---|
| Developed from | Cessna 411[source] | — |
|---|
| Developed into | Cessna 404 Titan Cessna 414[source] | Cirrus SR22[source] |
|---|
| Capacity | Six passengers[source] | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] |
|---|
| Airfoil | NACA 23018 (root) NACA 23015 (tip)[source] | — |
|---|
| Fuel capacity | 206 US gal (172 imp gal; 780 L) usable fuel[source] | — |
|---|
| Propellers | 3-bladed McCauley 0850334-34 constant speed propeller[source] | 3-bladed[source] |
|---|
| Stall speed | 68 kn (78 mph, 126 km/h) (flaps down, power off) (CAS)[source] | 56 kn (64 mph, 104 km/h) CAS[source] |
|---|
| Never exceed speed | 231 kn (266 mph, 428 km/h) ( CAS )[source] | — |
|---|
| Takeoff distance to 50 ft (15m) | 2,195 ft (669 m)[source] | — |
|---|
| Landing distance from 50 ft (15m) | 2,485 ft (757 m)[source] | — |
|---|