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Measured figures
Falcon 900B · Length
Single source20.21 m (66 ft 4 in)[source]
Configuration
| Specification | Cessna Citation family | Dassault Falcon 900 |
|---|---|---|
| Type | Business jet[source]Citation family | Business jet[source] |
| Manufacturer | Cessna[source]Citation family | Dassault Aviation[source] |
| Number built | 8,000[source]Citation family | >500[source] |
| Introduction date | 1972[source] |
Falcon 900B · Wingspan
Single source19.33 m (63 ft 5 in)[source]
Falcon 900B · Crew
Single sourceFalcon 900B · with 8 passengers
Single source7,400 km (4,600 mi, 4,000 nmi) with 8 passengers[source]
Falcon 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]
Falcon 900B · Wing area
Single source49.0 m 2 (527 sq ft)[source]
Falcon 900B · Service ceiling
Single source15,500 m (50,900 ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| First flight | 15 September 1969[source]Citation family | 21 September 1984 ( 1984-09-21 )[source] |
|---|
| Variants | Citation I / I/SP Citation II/SII/Bravo Citation III-VI-VII Cessna Citation V/Ultra/Encore Citation Excel/XLS/XLS+/Ascend CitationJet/CJ series Citation Mustang Citation X Citation Sovereign Citation Latitude Citation Longitude Citation Hemisphere[source]Citation family | — |
|---|
| Country of origin | United States[source]Inventory Origin column; table 13, row 8, cell 3; revision 1374043591; retrieved 2026-09-30 | — |
|---|
| National origin | — | France[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] |
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| Manufactured | — | 1984–present[source] |
|---|
| Developed from | — | Dassault Falcon 50[source] |
|---|
| Developed into | — | Dassault Falcon 2000 Dassault Falcon 7X[source] |
|---|
| Capacity | — | 19 passengers[source] |
|---|
| Fuel capacity | — | 8,690 kg (19,160 lb)[source] |
|---|
| Aspect ratio | — | 7.63:1[source] |
|---|
| Stall speed | — | 158 km/h (98 mph, 85 kn) (wheels and flaps down)[source] |
|---|