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The Boeing MD-11 is considered a medium to long-range wide body airliner. It has 2 engines built on under wing pylons and a 3rd engine at the base of the vertical stabilizer. It is like the DC-10, but it comprises a stretched fuselage, greater wingspan with winglets. It has an all-digital glass cockpit which in turn decreases the crew to 2 from the 3 that is required on the DC-10.
It was launched on December on 1986. The initial orders came Alitalia; British Caledonian; Dragonair; FedEx Express; Finnair; Korean Air; Scandinavian Airlines System; Swissair; Thai Airways International and Varig and 2 leasing companies Guinness Peat Aviation and Mitsui).
The 1st MD-11 was delivered to Finnair on December 7 of 1990.
The variants are MD-11 (Passenger), MD-11CF (Convertible Freighter), MD-11F (Freighter), MD-11C (Combi), MD-11ER (Extended Range)
The specifications of the MD-11 are the ff:
Capacity
Passengers/Cargo 410 (1 class) 323 (2 class) 293 (3 class)
Dimension
Fuselage Length 192 ft 5 in (58.6 m)
Wingspan 169 ft 6 in (51.70 m)
Tail height 57 ft 9 in (17.60 m)
Weights
Max takeoff weight standard: 602,500 lb (273,300 kg) heavy: 630,500 lb (286,000 kg)
Max landing weight 430,000 lb (200,000 kg)
Take-off distance at MTOW 10,300 ft (3,100 m)
Speed and Range
Max range 6,840 NM (12,655 km)
Max cruise speed 0.88 Mach (587 mph, 945 km/h, 520 kn)v
Typical cruise speed Pratt & Whitney PW4460 - 60,000 lbf (270 kN)
Engines
(3x) PW4462 - 62,000 lbf (280 kN) General Electric CF6-80C2D1F - 61,500 lbf (274 kN)
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