Airbus A310-300
Overview
The Airbus A310-300 is a commercial aircraft manufactured by Airbus, with the profile centered on its passenger/cargo role. Its recorded first flight is 1985-07-08. The current production-status field is listed as In Production. The listed configuration provides for a crew of 2 and passenger capacity of 220 typical; 247 maximum. Power is provided by 2 General Electric or Pratt & Whitney CF6-80C2A2/CF6-80C2A8 or PW4152/PW4156A engines. Recorded dimensions include length 153.2 ft, wingspan 144 ft, height 52.3 ft. Maximum takeoff weight is listed as 317,465 lb. Listed performance includes cruise speed 480 kt (Mach 0.80) kt, range 5,100 nmi nautical miles, service ceiling 40,000 ft ft. Its ICAO type designator is A310. Figures shown here describe the listed type or configuration and may vary by sub-variant, certification basis, or operator fit.
Quick Facts
Specifications
| ICAO Type Code | A310 |
|---|---|
| First Flight | Jul 8, 1985 |
| Crew | 2 |
| Passenger Capacity | 220 typical; 247 maximum |
| Length | 153.2 ft |
| Wingspan / Rotor Diameter | 144 ft |
| Height | 52.3 ft |
| Empty Weight | 174,528–174,619 lb estimated OEW, engine-dependent |
| Max Takeoff Weight | 317,465 lb |
| Cruise Speed | 480 kt (Mach 0.80) |
| Range | 5,100 nmi |
| Service Ceiling | 40,000 ft |
| Engine Manufacturer | General Electric or Pratt & Whitney |
| Engine Model | CF6-80C2A2/CF6-80C2A8 or PW4152/PW4156A |
| Engine Count | 2 |
Data verification status: Partially Verified