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ANTONOV An-140

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A140
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


Manufacturered as:

ANTONOV An-140
HESA IRAN-140 Faraz
HESA Faraz


ANTONOV An-140

ANTONOV An-140 ANTONOV An-140 3D

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
Length 26.61 m87.303 ft
Height 8.23 m27.001 ft
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
21.5 tonnes
kg
Ceiling FL200 ROD ft/min APC
WTC M Range 12631,263 nm
2,339,076 m
2,339.076 km
7,674,133.864 ft
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.)