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At a glance
Measured figures
Ambassador I · Length
Single source39 ft 6 + 1 ⁄ 4 in (12.046 m)[source]
Falcon 900B · Length
Configuration
| Specification | Cessna 404 Titan | Dassault Falcon 900 |
|---|---|---|
| Type | Light passenger/cargo aircraft[source] | Business jet[source] |
| National origin | United States[source] | France[source] |
| Manufacturer | Cessna[source] | Dassault Aviation[source] |
| Number built | 396[source] | >500 |
20.21 m (66 ft 4 in)[source]
Ambassador I · Height
Single source13 ft 3 in (4.04 m)[source]
Empty; Ambassador I · Empty weight
Single sourceMaximum take-off; Ambassador I · Max takeoff weight
Single source4,816 lb (2,185 kg)[source]
8,400 lb (3,810 kg)[source]
Empty; Falcon 900B · Empty weight
Single sourceMaximum take-off; Falcon 900B · Max takeoff weight
Single sourceFalcon 900B · 3 × Honeywell TFE731 -5BR-1C turbofans thrust each
Single source3 × Honeywell TFE731 -5BR-1C turbofans , 21.13 kN (4,750 lbf) thrust each[source]
Ambassador I · 1,575 ft/min (
Single source1,575 ft/min (8.00 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufactured | 1976–1982[source] | 1984–present[source] |
|---|
| Introduction date | 1976[source] | — |
|---|
| First flight | February 26, 1975[source] | 21 September 1984 ( 1984-09-21 )[source] |
|---|
| Developed from | Cessna 402[source] | Dassault Falcon 50[source] |
|---|
| Developed into | Reims-Cessna F406 Caravan II Cessna 441 Conquest II[source] | Dassault Falcon 2000 Dassault Falcon 7X[source] |
|---|
| Capacity | 6–8 passengers[source] | 19 passengers[source] |
|---|
| Aspect ratio | 9.0:1[source] | 7.63:1[source] |
|---|
| Fuel capacity | 340 US gal (280 imp gal; 1,300 L)[source] | 8,690 kg (19,160 lb)[source] |
|---|
| Stall speed | 81 mph (130 km/h, 70 kn) flaps down, power off[source] | 158 km/h (98 mph, 85 kn) (wheels and flaps down)[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] | — |
|---|
| Status | — | Active service, in production[source] |
|---|
| Primary users | — | French Air and Space Force Japan Coast Guard Nigerian Air Force Royal Malaysian Air Force[source] |
|---|