FORCETALLY
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At a glance
Measured figures
Ambassador I · Length
Single source39 ft 6 + 1 ⁄ 4 in (12.046 m)[source]
SR20-G3 · Length
Single sourceConfiguration
| Specification | Cessna 404 Titan | Cirrus SR20 |
|---|---|---|
| Type | Light passenger/cargo aircraft[source] | Light aircraft[source] |
| National origin | United States[source] | United States[source] |
| Manufacturer | Cessna[source] | Cirrus Aircraft[source] |
| Number built | 396[source] | 2,084 (through 2025) |
26 ft 0 in (7.92 m)[source]
Cruise; Ambassador I · (econ cruise) at 20,000 ft (6,100 m)
Single sourceMaximum; Ambassador I · at 16,000 ft (4,900 m)
Single source267 mph (430 km/h, 232 kn) at 16,000 ft (4,900 m)[source]
188 mph (302 km/h, 163 kn) (econ cruise) at 20,000 ft (6,100 m)[source]
Cruise; SR20-G3 · TAS
Single source155 kn (178 mph, 287 km/h) TAS[source]
Ambassador I · Range
Single source2,120 mi (3,410 km, 1,840 nmi)[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]
Ambassador I · Wing area
Single source242.0 sq ft (22.48 m 2 )[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufactured | 1976–1982[source] | 1999–present[source] |
|---|
| Introduction date | 1976[source] | — |
|---|
| First flight | February 26, 1975[source] | 21 March 1995[source] |
|---|
| Developed from | Cessna 402[source] | — |
|---|
| Developed into | Reims-Cessna F406 Caravan II Cessna 441 Conquest II[source] | Cirrus SR22[source] |
|---|
| Capacity | 6–8 passengers[source] | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] |
|---|
| Aspect ratio | 9.0:1[source] | — |
|---|
| Fuel capacity | 340 US gal (280 imp gal; 1,300 L)[source] | — |
|---|
| Stall speed | 81 mph (130 km/h, 70 kn) flaps down, power off[source] | 56 kn (64 mph, 104 km/h) CAS[source] |
|---|
| Never exceed speed | 274 mph (441 km/h, 238 kn) ( Calibrated airspeed )[source] | — |
|---|
| Take-off run to 50 ft (15 m) | 2,367 ft (721 m)[source] | — |
|---|
| Landing run from 50 ft (15 m) | 2,130 ft (650 m)[source] | — |
|---|
| Propellers | — | 3-bladed[source] |
|---|