Credit
Ptrump16 · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
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At a glance
Measured figures
A310-325 · Length
Single source46.66 m (153 ft 1 in)[source]
SR20-G3 · Length
Single sourceConfiguration
| Specification | Airbus A310 | Cirrus SR20 |
|---|---|---|
| Role | Wide-body aircraft[source] | — |
| National origin | Multi-national[source] | United States[source] |
| Manufacturer | Airbus[source] | Cirrus Aircraft[source] |
| Status | In limited service[source] | — |
| Primary users | Mahan Air ULS Airlines Cargo Iran Air Ariana Afghan Airlines[source] |
26 ft 0 in (7.92 m)[source]
A310-325 · Width
Single source5.640 m (18 ft 6 in)[source]
A310-325 · Range
Single source9,540 km (5,930 mi, 5,150 nmi)[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]
A310-325 · 2 × Pratt & Whitney PW4156A high bypass turbofan thrust each
Single source2 × Pratt & Whitney PW4156A high bypass turbofan , 249.08 kN (56,000 lbf) thrust each[source]
A310-325 · Wing area
Single source219.00 m 2 (2,357.3 sq ft)[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 | 255[source] | 2,084 (through 2025)[source] |
|---|
| Manufactured | 1981–1998[source] | 1999–present[source] |
|---|
| Introduction date | April 1983 with Swissair[source] | — |
|---|
| First flight | 3 April 1982 ( 1982-04-03 )[source] | 21 March 1995[source] |
|---|
| Developed from | Airbus A300[source] | — |
|---|
| Variants | Airbus A310 MRTT Airbus CC-150 Polaris[source] | — |
|---|
| Capacity | 243 passengers, 112.2 m 3 (3,962 cu ft) cargo volume[source] | 3 passengers (4 using 60/40 flex seating in post-2012 models)[source] |
|---|
| Fuel capacity | 61,070 L (16,132 US gal), 47,940 kg (105,689 lb) usable fuel[source] | — |
|---|
| Type | — | Light aircraft[source] |
|---|
| Developed into | — | Cirrus SR22[source] |
|---|
| Propellers | — | 3-bladed[source] |
|---|
| Stall speed | — | 56 kn (64 mph, 104 km/h) CAS[source] |
|---|