Antonov An-140

Antonov An-140

Infobox Aircraft
name=Antonov An-140


caption=Antonov An-140. Gostomel, Ukraine, 2008
type=Airliner
manufacturers=Antonov KSAMC HESA
designer=
first flight=17 September 1997
introduced=
retired=
status=Operational
primary user=Ukraine
more users=Iran
Russia
produced=1997-present
number built=28
unit cost=US$9 million
variants with their own articles=HESA IrAn-140
The Antonov An-140 is a short-range turboprop airliner, first flown on September 17 1997. Apart from the main production line in Kharkiv, Ukraine by KSAMC, aircraft are being produced in Russia and under licence by HESA in Iran as the IR.AN-140 or Iran-140. It can carry a maximum of 52 passengers.

Civil operators

In August 2006 a total of 11 Antonov An-140 aircraft are in airline service, with a further 16 firm orders. It is currently operated by:

pecifications (An-140)

aircraft specifications

ref=www.antonov.com [cite web|url=http://www.antonov.com/products/air/air-liner/AN-140/|title=Antonov An-140|accessdate=2006-08-22]

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

crew=2
capacity=52 passengers
length main=22.60 m
length alt=74 ft 2 in
span main=24.505 m
span alt=80 ft 5 in
height main=8.23 m
height alt=27 ft 0 in
area main=51 m²
area alt=549 ft²
empty weight main=12,810 kg
empty weight alt=28,240 lb
loaded weight main=
loaded weight alt=
useful load main=
useful load alt=
max takeoff weight main=19,150 kg
max takeoff weight alt=42,220 lb

number of props=2
engine (prop)=Klimov TV3-117WMA-SBM1
type of prop=turboprops
power main=1,838 kW
power alt=2,466 shp) each
* Alternate powerplant: Pratt & Whitney Canada PW127A turboprops, 1,900 kW (2,500

max speed main=575 km/h
max speed alt=310 knots, 357 mph
cruise speed main=460
cruise speed alt=250 knots, 290 mi
range main=1380 km
range alt=745 nm, 860 mi
range more= [At 520 km/h (280 kt, 320 mph) at 7,200 m (24,000 ft) with a 6,000 kg (13,000) payload.]
ferry range main=3,680 km
ferry range alt=1,990 nm, 2,290 mi
ceiling main=7200 m
ceiling alt=23600 ft
climb rate main= m/s
climb rate alt= 1,345 ft/min
loading main=
loading alt=
power/mass main=
power/mass alt=

Accidents

The An-140 has suffered two accidents where all onboard died, one in Iran (2002) and the other in Azerbaijan (2005). Investigation results were never published.

References

Notes

* [http://www.antonov.com/products/air/air-liner/AN-140/its.xml Official website]
* [http://www.ksamc.com/production/index.php?page=An-140-100_main.htm AN-140 at KSAMC]
* [http://www.hesaco.com/iran140/characteristics.htm Iran-140 Characteristics]

ee also

aircontent

related=

similar aircraft=
* ATR 42
* Fokker F50
* Ilyushin Il-114

sequence=
* An-72 - An-74 - An-124 - An-140 - An-148 - An-174 - An-180

lists=
* List of airliners
* List of civil aircraft of the Soviet Union and the CIS

see also=


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