Credit
Dmitry A. Mottl · Public domain · Resized · Public domain · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
A310 MRTT · Length
Single source47.4 m (155 ft 6 in)[source]
SR20-G3 · Length
Single sourceConfiguration
| Specification | Airbus A310 MRTT | Cirrus SR20 |
|---|---|---|
| Type | Multi-role tanker / transport[source] | Light aircraft[source] |
| Manufacturer | Airbus Military SAS , Airbus Deutschland, Lufthansa Technik[source] | Cirrus Aircraft[source] |
| Designer | Airbus Military SAS[source] | — |
| Status | Active service[source] | — |
| Primary users | German Air Force Royal Canadian Air Force[source] |
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]
A310 MRTT · 2 × General Electric CF6-80C2 or Pratt & Whitney PW4152 turbofan jet engines thrust each
Single source2 × General Electric CF6-80C2 or Pratt & Whitney PW4152 turbofan jet engines , 262 kN (59,000 lbf) thrust each[source]
SR20-G3 · Service ceiling
Single source17,500 ft (5,300 m)[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.
| — |
| Number built | 6, (from existing A310-300C airframes)[source] | 2,084 (through 2025)[source] |
|---|
| Introduction date | October 2004[source] | — |
|---|
| First flight | December 2003[source] | 21 March 1995[source] |
|---|
| Developed from | Airbus A310-300C[source] | — |
|---|
| Variant | Airbus CC-150 Polaris[source] | — |
|---|
| Successors | Airbus A330 MRTT[source] | — |
|---|
| Capacity | 214 passengers / 40,000 kg (88,000 lb) deliverable fuel / 36,000 kg (79,000 lb) cargo[source] | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] |
|---|
| Manufactured | — | 1999–present[source] |
|---|
| 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] |
|---|