McDonnell Douglas MD-11

Length
61.5696 m
Flat Wing Span
51.816 m
Height
17.3736 m
Max Ceiling
13167.36 m
Number of Engines
3
Aircraft Engine
First Flight
1990-01-10
Entry Into service
1990-12-20
Number Built
200
Maximum Take-Off Weight
283.722 t (paragliders: kg)
Total Fuel Capacity
11356.24
Maximum Range
12454.7 km

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Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Total Fuel Capacity Maximum Range (km)
McDonnell Douglas MD-11 283.722 11356.24 12454.7

Similar airplanes

Name Aircraft Engine Length (m) Flat Wing Span (m) Max Seating
McDonnell Douglas KC-10 Extender General Electric CF6 55.1688 50.292 16 Compare
McDonnell Douglas DC-10 General Electric CF6 55.4736 47.244 270 Compare
Lockheed L-1011 TriStar Rolls-Royce RB211 53.9496 47.244 256 Compare
All data (23 fields)
Name
McDonnell Douglas MD-11
Manufacturer
McDonnell Douglas
Description
The McDonnell Douglas MD-11 is an American trijet wide-body airliner which was manufactured by McDonnell Douglas and later by Boeing.
ICAO Code
MD11
First Flight
1990-01-10
Entry Into service
1990-12-20
Production End
2000-01-01
Service End
2014-10-26
Designer
McDonnell Douglas
Type
Wide-body jet airliner
Length (m)
61.5696
Height (m)
17.3736
Max Ceiling (m)
13167.36
National Origin
United States of America
Number Built
200
Powerplant Description
PW4460/62 / General Electric CF6-80C2D1F
Primary Users
FedEx Express, Western Global Airlines , UPS Airlines (historical), Lufthansa Cargo (historical)
Status
In cargo service
Wikipedia Article (URL)
en.wikipedia.org/wiki/McDonnell_Douglas_MD-11
Flat Wing Span (m)
51.816
Wake Category
H
Aircraft Engine
Pratt & Whitney PW4000
Number of Engines
3