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Follow-on to DC-10; revealed at Paris Air Show 1985; British Caledonian ordered nine 3 December 1986;
official programme launch 30 December 1986; five aircraft in flight test programme (four with GE engines,
one with P&W); first flight (N111MD) 10 January 1990 powered by CF6s; first flight of third prototype
powered by P&W PW4460s, 26 April 1990; certified 8 November 1990; first delivery to Finnair 29 November
1990, entering service 20 December. 100th MD-11 delivered 30 June 1993. Certification with R-R Trent 650
discontinued. Fuselage production line moved from San Diego to Long Beach during early 1996. Production
terminated at 200th aircraft (D-ALCN) which delivered to Lufthansa Cargo on 22 February 2001.
| MODEL | MD-11P |
| CREW | 2 |
| PASSENGERS | 293-405 |
| ENGINE | 3 x General Electric CF6-80C2D1F turbofans, 273kN |
| WEIGHTS |
| Take-off weight | 273300 kg | 602527 lb |
| Empty weight | 125870 kg | 277497 lb |
| DIMENSIONS |
| Wingspan | 51.6 m | 169 ft 3 in |
| Length | 61.2 m | 200 ft 9 in |
| Height | 17.6 m | 57 ft 9 in |
| Wing area | 338.9 m2 | 3647.89 sq ft |
| PERFORMANCE |
| Max. speed | 962 km/h | 598 mph |
| Cruise speed | 876 km/h | 544 mph |
| Ceiling | 11000 m | 36100 ft |
| Range w/max.fuel | 11000 km | 6835 miles |
| Range w/max.payload | 9270 km | 5760 miles |
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