Credit
Kiefer. from Frankfurt, Germany · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
Premier IA · Length
Single source46 ft 0 in (14.02 m)[source]
SR20-G3 · Length
Single sourceConfiguration
| Specification | Beechcraft Premier I | Cirrus SR20 |
|---|---|---|
| Type | Business Jet[source] | Light aircraft[source] |
| Manufacturer | Raytheon / Hawker Beechcraft[source] | Cirrus Aircraft[source] |
| Status | Active[source] | — |
| Number built | 292[source] | 2,084 (through 2025)[source] |
| Manufactured |
26 ft 0 in (7.92 m)[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]
Premier IA · 2 × Williams FJ44 -2A Turbofan thrust each
Single source2 × Williams FJ44 -2A Turbofan, 2,300 lbf (10.23 kN) thrust each[source]
Premier IA · Wing area
Single source246 sq ft (22.9 m 2 )[source]
Premier IA · Maximum payload
Single source1,400 lb / 635 kg[source]
SR20-G3 · 828 ft/min (
Single source828 ft/min (4.21 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
2001-2012[source] |
1999–present[source] |
| First flight | December 22, 1998[source] | 21 March 1995[source] |
|---|
| Capacity | 6 / 7[source] | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] |
|---|
| Aspect ratio | 8.03[source] | — |
|---|
| Fuel capacity | 3,670 lb / 1,665 kg[source] | — |
|---|
| Cabin Length × Width × Height | 13 ft 6 in × 5 ft 6 in × 5 ft 5 in (4.11 × 1.68 × 1.65 m)[source] | — |
|---|
| Hold | 76.9 cu. ft / 2.2 cu. m[source] | — |
|---|
| Wing loading | 50.6 lb/sq ft (247 kg/m 2 )[source] | — |
|---|
| Fuel consumption | 1.67 lb/mi (0.47 kg/km)[source] | — |
|---|
| Thrust/weight | 0.37[source] | — |
|---|
| Take-off (MTOW) | 3,792 ft / 1,156 m[source] | — |
|---|
| Landing (MLW) | 3,177 ft / 968 m[source] | — |
|---|
| Country of origin | United States[source]Beechcraft Premier I · literal inventory Origin field assigned to the exact equipment row linked in the primary inventory identity column; no operator, manufacturer location or parent/sibling specification inference | — |
|---|
| Developed into | — | Cirrus SR22[source] |
|---|
| Propellers | — | 3-bladed[source] |
|---|
| Stall speed | — | 56 kn (64 mph, 104 km/h) CAS[source] |
|---|
| National origin | — | United States[source] |
|---|