A140
ANTONOV An-140
ANTONOV An-140
Aircraft
Name
An-140
Manufacturer
Body
Narrow
Wing
Fixed Wing
Position
High wing
Tail
Regular tail, low set
WTC
M
Type Code
L2T
Engine
Turboprop
Engine Count
Multi
Position
Underwing mounted
Landing gear
Tricycle retractable
Manufactured as
HESA IRAN-140 Faraz
HESA Faraz
ANTONOV An-140
A140
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 (metric)
25.51 m
Length (metric)
26.61 m
Height (metric)
8.23 m
Powerplant
2 x 1839 kW (2466 shp) AI-30 Series 1 turbofans
Indicative Performance Data
Take-Off
V2
n/a
Distance
880 m
MTOW
21500 kg
Initial Climb (to 5000 ft)
IAS
n/a
ROC
n/a
Initial Climb (to FL150)
IAS
n/a
ROC
n/a
Initial Climb (to FL240)
IAS
n/a
ROC
n/a
MACH Climb
MACH
n/a
ROC
n/a
Cruise
TAS
243 kts
MACH
n/a
Ceiling
200
Range
1263 NM
Initial Descent (to FL240)
MACH
n/a
ROD
n/a
Descent (to FL100)
IAS
n/a
ROD
n/a
Descent (FL100 & below)
IAS
n/a
MCS
n/a
ROD
n/a
Approach
Vapp (IAS)
109 kts
Distance
530 m
