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A140
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| − | {{ | + | {{Aircraft |
| − | | | + | |Name=An-140 |
| − | | | + | |Manufacturer=ANTONOV |
| − | | | + | |WTC=M |
| − | | | + | |Body=Narrow |
| − | | | + | |Wing=Fixed Wing |
| − | | | + | |Engine=Turboprop |
| − | + | |Engine_Amount=Multi | |
| + | |Type_Code=L2T | ||
| + | |Description=Twin turboprop regional airliner. First delivery in March 2002. Manufactured in Ukraine (Kharkov), Russian Federation (Samara) and Iran (under license, by HESA). A military version exists with patrol, surveillance, photographic and other variants for military operations. | ||
| + | |Wing_Span=25.51 | ||
| + | |Length=26.61 | ||
| + | |Heigth=8.23 | ||
| + | |Wing_position=High wing | ||
| + | |Engine_position=Underwing mounted | ||
| + | |Tail_configuration=Regular tail, low set | ||
| + | |Landing_gear=Tricycle retractable | ||
| + | |Powerplant=2 x 1839 kW (2466 shp) AI-30 Series 1 turbofans | ||
| − | + | or | |
| − | + | 2 x 1644 kW (2500 shp) PW127A turbofans | |
| − | + | }} | |
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Latest revision as of 17:18, 23 February 2018
| Aircraft | |||||
|---|---|---|---|---|---|
| Name | An-140 | ||||
| Manufacturer | ANTONOV | ||||
| Body | Narrow | ||||
| Wing | Fixed Wing | ||||
| Position | High wing | ||||
| Tail | Regular tail, low set | ||||
| WTC | Medium | ||||
| Type code | L2T | ||||
| Engine | Turboprop | ||||
| Engine count | Multi | ||||
| Position | Underwing mounted | ||||
| Landing gear | Tricycle retractable | ||||
| Mass group | 3 | ||||
|
| |||||
ANTONOV An-140
Description
Twin turboprop regional airliner. First delivery in March 2002. Manufactured in Ukraine (Kharkov), Russian Federation (Samara) and Iran (under license, by HESA). A military version exists with patrol, surveillance, photographic and other variants for military operations.
Technical Data
| Wing span | 25.51 m83.694 ft <br /> |
|---|---|
| Length | 26.61 m87.303 ft <br /> |
| Height | 8.23 m27.001 ft <br /> |
| Powerplant | 2 x 1839 kW (2466 shp) AI-30 Series 1 turbofans
or 2 x 1644 kW (2500 shp) PW127A turbofans |
| Engine model |
Performance Data
| Take-Off | Initial Climb (to 5000 ft) |
Initial Climb (to FL150) |
Initial Climb (to FL240) |
MACH Climb | Cruise | Initial Descent (to FL240) |
Descent (to FL100) |
Descent (FL100 & below) |
Approach | ||||||||||
| V2 (IAS) | kts | IAS | kts | IAS | kts | IAS | kts | MACH | TAS | 243 kts | MACH | IAS | kts | IAS | kts | Vapp (IAS) | 109 kts | ||
| Distance | 880 m | ROC | ft/min | ROC | ft/min | ROC | ft/min | ROC | ft/min | MACH | ROD | ft/min | ROD | ft/min | MCS | kts | Distance | 530 m | |
| MTOW | 2150021,500 kg <br />21.5 tonnes <br /> kg | Ceiling | FL200 | ROD | ft/min | APC | |||||||||||||
| WTC | M | Range | 12631,263 nm <br />2,339,076 m <br />2,339.076 km <br />7,674,133.864 ft <br /> NM | ||||||||||||||||
Accidents & Serious Incidents involving A140
- A140, vicinity Tehran Mehrabad Iran, 2014 (On 10 August 2014, one of the engines of an Antonov 140-100 departing Tehran Mehrabad ran down after V1 and prior to rotation. The takeoff was continued but the crew were unable to keep control and the aircraft stalled and crashed into terrain near the airport. The Investigation found that a faulty engine control unit had temporarily malfunctioned and that having taken off with an inappropriate flap setting, the crew had attempted an initial climb with a heavy aircraft without the failed engine propeller initially being feathered, with the gear remaining down and with the airspeed below V2.)