| General Information |
|---|
| Type |
An-180 |
| Function |
Passenger |
| Year |
Project started in
1991 |
| Crew |
2 + attendants |
| Powerplant |
|---|
| Type |
2*D-27 "Progress" |
| Power at ?m |
2*13880hp |
| Fuel consumption |
14.5 g/passenger/km |
| Size |
|---|
| Length |
43.0m |
| Wingspan |
35.6m |
| Wing area |
127m2 |
| Weights and loads |
|---|
| Empty |
42,500kg |
| Normal Takeoff |
67,500kg |
| Maximum Takeoff |
71,700kg |
| Wing Load (kg/m2) |
532 |
| Power load (kg/hp) |
2.43 |
| Speed |
|---|
| Cruise |
800km/h |
| Runway for takeoff |
|---|
| Normal load |
1950m |
| Maximum load |
2300m |
| Range (normal takeoff weight / maximum takeoff weight) |
|---|
| Maximum payload |
1800/3300km |
| 175 passengers |
2400/3900km |
| 163 passengers |
3060/4500km |
| Maximum fuel and 52/95 passengers |
7700/7500km |
| Ceiling |
|---|
| Cruise |
10,100m |
| Payload |
|---|
| Fuel |
?kg |
| Maximum Payload |
18,000kg |
| Cabin size LxWxH |
m3 |
| Seats (810mm) |
163 |
| Seats (750mm) |
175 |
Highly
economical medium-size mid-range passenger
aircraft. Powerplant arrangement is
quite unusual - two tractor turbofans on the tips of a tailplane. Some pictures
show An-180 with T-tail and raised wingtips, other - with normal wing and tail,
while the engines are attached to toward-swept outer parts of a tailplane.
Project started in
1991.
Original milestones were first flight in
1995
and entering commercial service in
1997.
Still in a project stage...
