Credit
Adrian Pingstone ( Arpingstone ) · Public domain · Resized · Public domain · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
Jetstream 41 · Length
Single source63 ft 2 in (19.25 m)[source]
SR20-G3 · Length
Configuration
| Specification | British Aerospace Jetstream 41 | Cirrus SR20 |
|---|---|---|
| Type | Regional airliner /Feederliner[source] | Light aircraft[source] |
| National origin | United Kingdom[source] | United States[source] |
| Manufacturer | British Aerospace[source] | Cirrus Aircraft[source] |
| Status | In service[source] | — |
26 ft 0 in (7.92 m)[source]
Cruise; Jetstream 41 · max at 20,000 ft (6,100 m)
Single sourceMaximum; Jetstream 41 · at 20,000 ft (6,100 m)
Single source295 kn (339 mph, 546 km/h) at 20,000 ft (6,100 m)[source]
295 kn (339 mph, 546 km/h) max at 20,000 ft (6,100 m)[source]
Cruise; SR20-G3 · TAS
Single source155 kn (178 mph, 287 km/h) TAS[source]
Jetstream 41 · with 29 pax + IFR reserves
Single source774 nmi (891 mi, 1,433 km) with 29 pax + IFR reserves[source]
Jetstream 41 · 2 × Allied Signal TPE331-14GR/HR turboprop engines, 1,650 shp ( ) each (handed GR / HR
Single source2 × Allied Signal TPE331-14GR/HR turboprop engines, 1,650 shp (1,230 kW) each (handed GR / HR)[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]
Jetstream 41 · Wing area
Single source350.8 sq ft (32.59 m 2 )[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary users | Guna Airlines Proflight Zambia[source] | — |
|---|
| Number built | 100[source] | 2,084 (through 2025)[source] |
|---|
| Manufactured | 1992–1997[source] | 1999–present[source] |
|---|
| Introduction date | 25 November 1992[source] | — |
|---|
| First flight | 25 September 1991[source] | 21 March 1995[source] |
|---|
| Developed from | British Aerospace Jetstream 31[source] | — |
|---|
| Capacity | 29 passengers[source] | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] |
|---|
| Airfoil | root: NACA 63A418 ; tip: NACA 63A412[source] | — |
|---|
| Maximum zero-fuel weight | 21,400 lb (9,707 kg)[source] | — |
|---|
| Maximum ramp weight | 24,100 lb (10,932 kg)[source] | — |
|---|
| Maximum landing weight | 23,300 lb (10,569 kg)[source] | — |
|---|
| Fuel capacity | 727 imp gal (873 US gal; 3,305 L) / 5,960 lb (2,703 kg) maximum[source] | — |
|---|
| Propellers | 5-bladed McCauley , 9 ft 6 in (2.9 m) diameter (handed GR / HR) constant-speed feathering metal propellers[source] | 3-bladed[source] |
|---|
| Never exceed speed | 315 kn (362 mph, 583 km/h) CAS sea level to 17,400 ft (5,300 m)[source] | — |
|---|
| Service ceiling on one engine | 15,000 ft (4,600 m)[source] | — |
|---|
| Wing loading | 68.42 lb/sq ft (334.1 kg/m 2 )[source] | — |
|---|
| Power/mass | 0.1375 shp/lb (0.2260 kW/kg)[source] | — |
|---|
| Take-off run | 5,000 ft (1,500 m)[source] | — |
|---|
| Landing run | 4,200 ft (1,300 m)[source] | — |
|---|
| Developed into | — | Cirrus SR22[source] |
|---|
| Stall speed | — | 56 kn (64 mph, 104 km/h) CAS[source] |
|---|