FORCETALLY
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At a glance
Measured figures
Cessna Citation I · Length
Single source43 ft 6 in (13.26 m)[source]
Falcon 900B · Length
Configuration
| Specification | Cessna Citation I | Dassault Falcon 900 |
|---|---|---|
| Type | Corporate jet[source] | Business jet[source] |
| National origin | United States[source] | France[source] |
| Manufacturer | Cessna[source] | Dassault Aviation[source] |
| Number built | 689, 688 delivered[source] | >500 |
20.21 m (66 ft 4 in)[source]
Cessna Citation I · Height
Single source14 ft 4 in (4.37 m)[source]
Empty; Cessna Citation I · Empty weight
Single sourceMaximum take-off; Cessna Citation I · Max takeoff weight
Single source6,631 lb (3,008 kg)[source]
11,850 lb (5,375 kg)[source]
Empty; Falcon 900B · Empty weight
Single sourceMaximum take-off; Falcon 900B · Max takeoff weight
Single sourceCessna Citation I · at 41,000 ft (12,000 m) (45 min reserves, 1,562 lb (709 kg) payload)
Single source1,328 nmi (1,528 mi, 2,459 km) at 41,000 ft (12,000 m) (45 min reserves, 1,562 lb (709 kg) payload)[source]
Falcon 900B · with 8 passengers
Single source7,400 km (4,600 mi, 4,000 nmi) with 8 passengers[source]
Cessna Citation I · 2 × Pratt & Whitney Canada JT15D -1B turbofans thrust each
Single source2 × Pratt & Whitney Canada JT15D -1B turbofans , 2,200 lbf (9.8 kN) thrust each[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]
Cessna Citation I · 2,719 ft/min (
Single source2,719 ft/min (13.81 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufactured | 1971–1985[source] | 1984–present[source] |
|---|
| First flight | September 15, 1969 (FanJet 500)[source] | 21 September 1984 ( 1984-09-21 )[source] |
|---|
| Developed into | Cessna Citation II[source] | Dassault Falcon 2000 Dassault Falcon 7X[source] |
|---|
| Capacity | 5 passengers[source] | 19 passengers[source] |
|---|
| Aspect ratio | 7.83:1[source] | 7.63:1[source] |
|---|
| Fuel capacity | 564 US gal (470 imp gal; 2,130 L) usable fuel[source] | 8,690 kg (19,160 lb)[source] |
|---|
| Stall speed | 82 kn (94 mph, 152 km/h) ( CAS )[source] | 158 km/h (98 mph, 85 kn) (wheels and flaps down)[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] |
|---|
| Developed from | — | Dassault Falcon 50[source] |
|---|