FORCETALLY
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At a glance
Measured figures
Falcon 900B · Length
Single source20.21 m (66 ft 4 in)[source]
Phenom 100EV · Length
Single sourceConfiguration
| Specification | Dassault Falcon 900 | Embraer Phenom 100 |
|---|---|---|
| Type | Business jet[source] | Very light business jet[source] |
| National origin | France[source] | Brazil[source] |
| Manufacturer | Dassault Aviation[source] | Embraer[source] |
| Status | Active service, in production[source] | In production, in service |
12.82 m (42 ft 1 in)[source]
Phenom 100EV · Height
Single source4.35 m (14 ft 3 in)[source]
Empty; Falcon 900B · Empty weight
Single sourceMaximum take-off; Falcon 900B · Max takeoff weight
Single source10,255 kg (22,608 lb)[source]
20,640 kg (45,503 lb)[source]
Empty; Phenom 100EV · Empty weight
Single sourceMaximum take-off; Phenom 100EV · Max takeoff weight
Single sourceFalcon 900B · with 8 passengers
Single source7,400 km (4,600 mi, 4,000 nmi) with 8 passengers[source]
Phenom 100EV · alternate
Single sourcePhenom 100EV · LRC, four 91 kg (200 lb) occupants, NBAA IFR reserves with
Single source2,182 km (1,356 mi, 1,178 nmi) (LRC, four 91 kg (200 lb) occupants, NBAA IFR reserves with 185 km (115 mi; 100 nmi) alternate)[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]
Phenom 100EV · 2 × Pratt & Whitney Canada PW617F1-E turbofan engines thrust each at ISA + 8°C
Single source2 × Pratt & Whitney Canada PW617F1-E turbofan engines, 7.7 kN (1,730 lbf) thrust each at ISA + 8°C[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] | 439 (H1 2026)[source] |
|---|
| Manufactured | 1984–present[source] | December 2008–present[source] |
|---|
| First flight | 21 September 1984 ( 1984-09-21 )[source] | 26 July 2007[source] |
|---|
| Developed from | Dassault Falcon 50[source] | — |
|---|
| Developed into | Dassault Falcon 2000 Dassault Falcon 7X[source] | — |
|---|
| Capacity | 19 passengers[source] | 4 or 5 passengers (standard configurations); 7 passengers maximum (with passenger in cockpit, optional side-facing seat, and optional belted lavatory)[source] |
|---|
| Fuel capacity | 8,690 kg (19,160 lb)[source] | 1,272 kg (2,804 lb)[source] |
|---|
| Aspect ratio | 7.63:1[source] | — |
|---|
| Stall speed | 158 km/h (98 mph, 85 kn) (wheels and flaps down)[source] | — |
|---|
| Variant | — | Embraer Phenom 300[source] |
|---|
| Cabin height | — | 1.5 m (4 ft 11 in)[source] |
|---|
| Cabin length | — | 3.35 m (11 ft)[source] |
|---|
| Minimum control speed | — | 180 km/h (110 mph, 97 kn)[source] |
|---|
| Cabin altitude | — | 2,438 m (8,000 ft) at 12,497 m (41,000 ft)[source] |
|---|
| Take-off run | — | 975 m (3,199 ft) (MTOW, SL, ISA)[source] |
|---|
| Landing run | — | 741 m (2,431 ft) (SL, ISA, four 91 kg (200 lb) occupants, NBAA IFR reserves with 185 km (115 mi; 100 nmi) alternate)[source] |
|---|
| Hourly fuel burn | — | (1,111 km (690 mi; 600 nmi) trip, four 91 kg (200 lb) occupants, NBAA IFR Reserves. SL Takeoff, ISA) 1st hour – 414 L/h (109 gal/h; 91 imp gal/h) (take-off and climb to cruise) 2nd hour – 292 L/h (77 gal/h; 64 imp gal/h) (cruise)[source] |
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