Credit
Bill Larkins · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
2011 model G36 · Length
Single source27 ft 6 in (8.38 m)[source]
Falcon 900B · Length
Configuration
| Specification | Beechcraft Bonanza | Dassault Falcon 900 |
|---|---|---|
| Type | Civil utility aircraft[source] | Business jet[source] |
| National origin | United States[source] | France[source] |
| Manufacturer | Beechcraft[source] | Dassault Aviation[source] |
| Status | In service[source] | Active service, in production |
20.21 m (66 ft 4 in)[source]
2011 model G36 · Height
Single source8 ft 7 in (2.62 m)[source]
2011 model G36 · with full passenger load
Single sourceFerry; 2011 model G36 · Ferry range
Single source716 nmi (824 mi, 1,326 km) with full passenger load[source]
930 nmi (1,070 mi, 1,720 km)[source]
Falcon 900B · with 8 passengers
Single source7,400 km (4,600 mi, 4,000 nmi) with 8 passengers[source]
2011 model G36 · 1 × Continental IO-550-B
Single source1 × Continental IO-550-B , 300 hp (220 kW)[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]
2011 model G36 · 1,230 ft/min (
Single source1,230 ft/min (6.2 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Number built | 18,525 (at end of 2025)[source] | >500[source] |
|---|
| Manufactured | 1947–present[source] | 1984–present[source] |
|---|
| Introduction date | 1947[source] | — |
|---|
| First flight | December 22, 1945[source] | 21 September 1984 ( 1984-09-21 )[source] |
|---|
| Variant | Beechcraft QU-22 Pave Eagle[source] | — |
|---|
| Developed into | Beechcraft T-34 Mentor Beechcraft Travel Air Bay Super V Fuji KM-2[source] | Dassault Falcon 2000 Dassault Falcon 7X[source] |
|---|
| Capacity | five passengers[source] | 19 passengers[source] |
|---|
| Aspect ratio | 6.2[source] | 7.63:1[source] |
|---|
| Airfoil | Root:NACA 23016.5. Tip:23012[source] | — |
|---|
| Propellers | three-bladed Hartzell Propeller , 6 ft 8 in (2.03 m) diameter[source] | — |
|---|
| Wing loading | 20.16 lb/sq ft (98.4 kg/m 2 )[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] |
|---|
| Fuel capacity | — | 8,690 kg (19,160 lb)[source] |
|---|
| Stall speed | — | 158 km/h (98 mph, 85 kn) (wheels and flaps down)[source] |
|---|