Credit
Markus Eigenheer from Genève, Schweiz · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
Citation Latitude · Length
Single source62 ft 3 in (18.97 m)[source]
Falcon 900B · Length
Configuration
| Specification | Cessna Citation Latitude | Dassault Falcon 900 |
|---|---|---|
| Type | Corporate jet[source] | Business jet[source] |
| National origin | United States[source] | France[source] |
| Manufacturer | Textron Aviation[source] | Dassault Aviation[source] |
| Status | In production[source] | Active service, in production |
20.21 m (66 ft 4 in)[source]
Citation Latitude · Height
Single source20 ft 11 in (6.38 m)[source]
Empty; Citation Latitude · Empty weight
Single sourceMaximum take-off; Citation Latitude · Max takeoff weight
Single source18,656 lb (8,462 kg)[source]
30,800 lb (13,971 kg)[source]
Empty; Falcon 900B · Empty weight
Single sourceMaximum take-off; Falcon 900B · Max takeoff weight
Single sourceCitation Latitude · 2 × Pratt Whitney Canada PW306D1 turbofan thrust each
Single source2 × Pratt Whitney Canada PW306D1 turbofan, 5,907 lbf (26.28 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]
Citation Latitude · 2,313 ft/min ( ) to FL370
Single source2,313 ft/min (11.75 m/s) to FL370[source]
Citation Latitude · Maximum payload
Single source2,544 lb (1,154 kg)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Number built | 400 by May 2024[source] | >500[source] |
|---|
| Manufactured | 2014–present[source] | 1984–present[source] |
|---|
| First flight | 18 February 2014[source] | 21 September 1984 ( 1984-09-21 )[source] |
|---|
| Developed from | Cessna Citation Sovereign[source] | Dassault Falcon 50[source] |
|---|
| Developed into | Cessna Citation Longitude[source] | Dassault Falcon 2000 Dassault Falcon 7X[source] |
|---|
| Capacity | 19 passengers[source] |
|---|
| Fuel capacity | 11,394 lb (5,168 kg)[source] | 8,690 kg (19,160 lb)[source] |
|---|
| Aspect ratio | 9.64[source] | 7.63:1[source] |
|---|
| Airfoil | 16.3° sweep[source] | — |
|---|
| Cabin | 72 in (1.83 m) height × 77 in (1.96 m) width[source] | — |
|---|
| Never exceed speed | 460 kn (530 mph, 850 km/h) Mach .80[source] | — |
|---|
| Time to altitude | 16 min to FL370[source] | — |
|---|
| Wing loading | 56.7 lb/sq ft (277 kg/m 2 ) MTOW[source] | — |
|---|
| Thrust/weight | 0.38[source] | — |
|---|
| Takeoff | 3,580 ft (1,091 m)[source] | — |
|---|
| Landing | 2,480 ft (756 m)[source] | — |
|---|
| Primary users | — | French Air and Space Force Japan Coast Guard Nigerian Air Force Royal Malaysian Air Force[source] |
|---|
| Stall speed | — | 158 km/h (98 mph, 85 kn) (wheels and flaps down)[source] |
|---|