Credit
Ptrump16 · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
A310-325 · Length
Single source46.66 m (153 ft 1 in)[source]
Falcon 900B · Length
Single sourceConfiguration
| Specification | Airbus A310 | Dassault Falcon 900 |
|---|---|---|
| Role | Wide-body aircraft[source] | — |
| National origin | Multi-national[source] | France[source] |
| Manufacturer | Airbus[source] | Dassault Aviation[source] |
| Status | In limited service[source] | Active service, in production[source] |
| Primary users |
20.21 m (66 ft 4 in)[source]
A310-325 · Width
Single source5.640 m (18 ft 6 in)[source]
A310-325 · at operating empty weight
Single source15.867 m (52 ft 0.7 in) at operating empty weight[source]
Empty; A310-325 · Empty weight
Single sourceMaximum take-off; A310-325 · Max takeoff weight
Single source79,166 kg (174,528 lb)[source]
164,000 kg (361,557 lb)[source]
Empty; Falcon 900B · Empty weight
Single sourceMaximum take-off; Falcon 900B · Max takeoff weight
Single sourceA310-325 · 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]
Falcon 900B · 3 × Honeywell TFE731 -5BR-1C turbofans thrust each
Single source3 × Honeywell TFE731 -5BR-1C turbofans , 21.13 kN (4,750 lbf) thrust each[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Mahan Air ULS Airlines Cargo Iran Air Ariana Afghan Airlines[source] |
French Air and Space Force Japan Coast Guard Nigerian Air Force Royal Malaysian Air Force[source] |
| Number built | 255[source] | >500[source] |
|---|
| Manufactured | 1981–1998[source] | 1984–present[source] |
|---|
| Introduction date | April 1983 with Swissair[source] | — |
|---|
| First flight | 3 April 1982 ( 1982-04-03 )[source] | 21 September 1984 ( 1984-09-21 )[source] |
|---|
| Developed from | Airbus A300[source] | Dassault Falcon 50[source] |
|---|
| Variants | Airbus A310 MRTT Airbus CC-150 Polaris[source] | — |
|---|
| Capacity | 243 passengers, 112.2 m 3 (3,962 cu ft) cargo volume[source] | 19 passengers[source] |
|---|
| Fuel capacity | 61,070 L (16,132 US gal), 47,940 kg (105,689 lb) usable fuel[source] | 8,690 kg (19,160 lb)[source] |
|---|
| Type | — | Business jet[source] |
|---|
| Developed into | — | Dassault Falcon 2000 Dassault Falcon 7X[source] |
|---|
| Aspect ratio | — | 7.63:1[source] |
|---|
| Stall speed | — | 158 km/h (98 mph, 85 kn) (wheels and flaps down)[source] |
|---|