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At a glance
Measured figures
Falcon 900B · Length
Single source20.21 m (66 ft 4 in)[source]
Length
Single sourceConfiguration
| Specification | Dassault Falcon 900 | PAC P-750 XSTOL |
|---|---|---|
| Type | Business jet[source] | Utility aircraft[source] |
| National origin | France[source] | New Zealand[source] |
| Manufacturer | Dassault Aviation[source] | Pacific Aerospace[source] |
| Status | Active service, in production[source] | Active, in production |
11.11 m (36 ft 5 in)[source]
1 × Pratt & Whitney Canada PT6 A-34 turboprop
Single source1 × Pratt & Whitney Canada PT6 A-34 turboprop , 560 kW (750 hp)[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]
1,067 ft/min
Single source5.42 m/s (1,067 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary users | French Air and Space Force Japan Coast Guard Nigerian Air Force Royal Malaysian Air Force[source] | — |
|---|
| Number built | >500[source] | 120[source] |
|---|
| Manufactured | 1984–present[source] | 2001–present[source] |
|---|
| First flight | 21 September 1984 ( 1984-09-21 )[source] | 2001[source] |
|---|
| Developed from | Dassault Falcon 50[source] | PAC Cresco[source] |
|---|
| Developed into | Dassault Falcon 2000 Dassault Falcon 7X[source] | — |
|---|
| Capacity | 19 passengers[source] | Pilot + nine passengers or 17 parachutists[source] |
|---|
| Fuel capacity | 8,690 kg (19,160 lb)[source] | — |
|---|
| Aspect ratio | 7.63:1[source] | 6.59[source] |
|---|
| Stall speed | 158 km/h (98 mph, 85 kn) (wheels and flaps down)[source] | 107 km/h (66 mph, 58 kn) Idle Power, Flaps Down[source] |
|---|
| Take-Off Ground Roll | — | 220 m (720 ft) (ISA, SL)[source] |
|---|
| Landing Ground Roll (excl. approach from 15 m AGL) | — | 166 m (545 ft) (SL)[source] |
|---|