Antonov An-218

Infobox Aircraft
infoboxwidth=16
name=Antonov An-218


caption=
type=Widebody airliner
manufacturer=Antonov
designer=
first flight=
introduced=
retired=
status=Cancelled
primary user=
more users=
produced=
number built=0
unit cost=
variants with their own articles=The Antonov An-218 was a proposal by the Antonov Design Bureau for a widebody commercial airliner. A twin-engined design, it was intended to carry approximately 350 passengers, but was never put into production.

pecifications (An-218-100, as designed)

aircraft specifications

plane or copter?=plane
jet or prop?=jet

crew=2
capacity=300/350/400 passengers (depending on chair spacing)
length main=59.79 m
length alt=196 ft 1 in
span main=50.0 m
span alt=164 ft
height main=15.7 m
height alt=51 ft 6 in
area main=270 m²
area alt=2,900 ft²
empty weight main=90,000-91,000 kg
empty weight alt=20,000 lb
loaded weight main=
loaded weight alt=
max takeoff weight main=170,000 kg
max takeoff weight alt=370,000 lb

number of jets=2
engine (jet)=Progress D18T1
type of jet=turbofans
thrust main=255 kN
thrust alt=57,000 lbf

max speed main=870 km/h
max speed alt=470 kt, 540 mph
range main=11,500 km
range alt=6,200 nm, 7,200 mi
ceiling main=
ceiling alt=
climb rate main=
climb rate alt=
loading main=
loading alt=
thrust/weight=

References

* [http://babelfish.altavista.com/babelfish/trurl_load?lp=ru_en&url=http%3A%2F%2Fwww.aviaport.ru%2Fdirectory%2Faviation%2F264.html Aircraft facts (translated)] ( [http://www.aviaport.ru/directory/aviation/264.html original page] )

ee also

aircontent

similar aircraft=
* Airbus A330
* Boeing 767
* Ilyushin Il-96
* Tupolev Tu-304

An-400