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         The Airbus A310 is a 
         medium- to long-range widebody airliner developed from the Airbus A300 
         and manufactured by Airbus Industrie. 
          
         Perhaps the greatest attribute of the A310 is that of range. The 
         A310-300's range exceeds all A300 models and the -200 exceeds all A300 
         models in range except the A300-600. This quality has led to the 
         aircraft being used extensively on transatlantic routes. The A300 and 
         A310 introduced the concept of commonality which has become one of the 
         Airbus family's greatest marketing points - A300-600 and A310 pilots 
         can qualify for the other aircraft with only one day of training. 
          
         Beginnings 
         The aircraft was formally launched in July 1978 for Lufthansa and 
         Swissair. A further development of the A300, the aircraft was initially 
         designated the A300 B10. Essentially a "baby" A300, the main 
         differences in the two aircraft are 
          
         Shortened fuselage - same cross section, providing capacity of about 
         200.  
         Redesigned wing - designed by British Aerospace who rejoined Airbus 
         consortium  
         Smaller vertical fin  
          
         Biman Airbus A310-300The A310 is marketed as an excellent introduction 
         to widebody operations for developing airlines. With the Airbus A330 
         now a major success, further orders for the A310 are unlikely. Between 
         1983 and 1997 255 A310s were delivered by Airbus. The A300 and A310 
         established Airbus as a major competitor to Boeing and allowed it to go 
         ahead with the more ambitious A330/A340 family. 
          
         Models 
         A310-200 
         The first A310 was the 162nd Airbus off the production line, the 
         aircraft made its maiden flight in April 1982 powered by Pratt & 
         Whitney JT9Ds. The -200 entered service with Swissair and Lufthansa a 
         year later.  
         A310-300 
         First flown in July 1985, the -300 has an increased MTOW and an 
         increase in range, provided by additional centre and horizontal 
         stabilizer (trim-tank) fuel tanks. This model also introduced winglets 
         to improve aerodynamic efficiency - since retrofitted to some -200s. 
         The aircraft entered service in 1986, again with Swissair.  
         A310-C 
         The convertible model can be produced from either model, taking the 
         designations A310-200C and -300C.  
         A310-F 
         No production freighters were produced, operators (e.g. FedEx) instead 
         adapting ex-airline A310s.  
         A310 MRTT 
         The A310 has long been operated by many of the world's air forces as a 
         pure transport, however some are now being converted to the Multi Role 
         Tanker Transport configuration by EADS, providing an aerial refuelling 
         capability. Six have been ordered; four by the German Luftwaffe and two 
         by the Canadian Forces. Deliveries began in 2004. Three are being 
         converted at EADS' Elbe Flugzeugwerke (EFW) in Dresden, Germany; the 
         other three at Lufthansa Technik in Hamburg, Germany.  
          
         Accident summary 
         Hull-loss Accidents: 6 with a total of 518 fatalities  
         Hijackings: 10 with a total of 5 fatalities  
         Other Incidents: Rudder partially fell off a Air Transat flight  
           
         Specifications (A310) 
           
         General characteristics 
         Crew: 2  
         Capacity: 220 (2 class) or 280 (1 class)  
         Length: 46.66 m (153 ft)  
         Wingspan: 43.9 m (144 ft)  
         Height: 15.8 m (51 ft)  
         Wing area: 219 m² (2360 ft²)  
         Empty: 80,800 kg ( lb)  
         Loaded: kg ( lb)  
         Maximum takeoff: 164,000 kg ( lb)  
         Powerplant: Two Pratt & Whitney PW4152 or General Electric 
         CF6-80 turbofans, 262 kN (59,000 lbf) thrust  
           
         Performance 
         Maximum speed: 897 km/h ( mph)  
         Range: 9,600 km (5,200 miles)  
         Service ceiling: 41,000 m (12,500 ft)  
         Rate of climb: m/min ( ft/min)  
         Wing loading: kg/m² ( lb/ft²)   |