Credit
Tomás Del Coro from Las Vegas, Nevada, USA · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
SR20-G3 · Length
Single source26 ft 0 in (7.92 m)[source]
Phenom 100EV · Length
Single sourceConfiguration
| Specification | Cirrus SR20 | Embraer Phenom 100 |
|---|---|---|
| Type | Light aircraft[source] | Very light business jet[source] |
| Manufacturer | Cirrus Aircraft[source] | Embraer[source] |
| Number built | 2,084 (through 2025)[source] | 439 (H1 2026)[source] |
| Manufactured | 1999–present[source] | December 2008–present |
12.82 m (42 ft 1 in)[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]
SR20-G3 · 1 × Continental IO-360-ES six cylinder, horizontally-opposed piston aircraft engine
Single source1 × Continental IO-360-ES six cylinder, horizontally-opposed piston aircraft engine , 200 hp (150 kW)[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]
SR20-G3 · 828 ft/min (
Single source828 ft/min (4.21 m/s)[source]
Phenom 100EV · Wing area
Single source18.76 m 2 (201.9 sq ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| First flight | 21 March 1995[source] | 26 July 2007[source] |
|---|
| Developed into | Cirrus SR22[source] | — |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | 4 or 5 passengers (standard configurations); 7 passengers maximum (with passenger in cockpit, optional side-facing seat, and optional belted lavatory)[source] |
|---|
| Propellers | 3-bladed[source] | — |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | — |
|---|
| National origin | United States[source] | Brazil[source] |
|---|
| Status | — | In production, in service[source] |
|---|
| Variant | — | Embraer Phenom 300[source] |
|---|
| Fuel capacity | — | 1,272 kg (2,804 lb)[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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