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]
Super 748 · Length
Single sourceConfiguration
| Specification | Cirrus SR20 | Hawker Siddeley HS 748 |
|---|---|---|
| Type | Light aircraft[source] | Airliner[source] |
| Manufacturer | Cirrus Aircraft[source] | Avro Hawker Siddeley Hindustan Aeronautics[source] |
| Number built | 2,084 (through 2025)[source] | 380[source] |
| Manufactured | 1999–present[source] | 1961–1988 |
67 ft 0 in (20.42 m)[source]
Super 748 · with max payload
Single source926 nmi (1,066 mi, 1,715 km) (with max payload)[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]
Super 748 · 2 × Rolls-Royce RDa.7 Dart Mk 536-2 turboprop engines, 2,280 shp ( ) each equivalent
Single source2 × Rolls-Royce RDa.7 Dart Mk 536-2 turboprop engines, 2,280 shp (1,700 kW) each equivalent[source]
SR20-G3 · 828 ft/min (
Single source828 ft/min (4.21 m/s)[source]
Super 748 · Wing area
Single source829 sq ft (77.0 m 2 )[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] | 24 June 1960[source] |
|---|
| Developed into | Cirrus SR22[source] | Hawker Siddeley Andover BAe ATP[source] |
|---|
| Capacity | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] | 40–58 passengers / 11,323 lb (5,136 kg) payload[source] |
|---|
| Propellers | 3-bladed[source] | 4-bladed Dowty Rotol constant-speed fully-feathering propellers, 12 ft 0 in (3.66 m) diameter[source] |
|---|
| Stall speed | 56 kn (64 mph, 104 km/h) CAS[source] | — |
|---|
| National origin | United States[source] | United Kingdom[source] |
|---|
| Status | — | In limited service with the Indian Air Force[source] |
|---|
| Primary users | — | British Airways Air Creebec Dan-Air Air North Varig[source] |
|---|
| Fuel capacity | — | 1,440 imp gal (1,730 US gal; 6,500 L) in two wing integral tanks[source] |
|---|
| Aspect ratio | — | 11.967[source] |
|---|
| Airfoil | — | root: NACA 23018 ; tip: NACA 4412[source] |
|---|
| Wing loading | — | 56.1 lb/sq ft (274 kg/m 2 )[source] |
|---|
| Power/mass | — | 0.0981 hp/lb (0.1613 kW/kg)[source] |
|---|
| Take-off distance to 50 ft (15 m) | — | 3,800 ft (1,200 m)[source] |
|---|
| Landing distance from 50 ft (15 m) | — | 2,034 ft (620 m)[source] |
|---|
| Take-off distance | — | 2,624 ft (800 m)[source] |
|---|
| Landing distance | — | 1,968 ft (600 m)[source] |
|---|