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Antonov An-140
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The as the IR.AN-140'''. It first flew in 1994 , and a total of eight or more have been built. It can carry a maximum of 60 passengers.
It has already had 2 hull-loss accidents where all onboard died, one in Iran and the other in Azerbaijan.


SPECIFICATIONS (AN-140)


  plane Or Copter plane
  jet Or Prop prop
  crew 2
  capacity 52 passengers
  length Main 2260 m
  length Alt 74 ft 2 in
  span Main 24505 m
  span Alt 80 ft 5 in
  height Main 823 m
  height Alt 27 ft 0 in
  area Main 51 m&sup2
  area Alt 549 ft&sup2
  empty Weight Main kg
  empty Weight Alt lb
  loaded Weight Main kg
  loaded Weight Alt lb
  max Takeoff Weight Main 19,150 kg
  max Takeoff Weight Alt 42,220 lb
  number Of Props 2
  engine (prop) Klimov TW3-117WMA-SBM1
  type Of Prop Turboprop s
  power Main 1,838 kW
  power Alt 2,466 shp)
  max Speed Main 575 km/h
  max Speed Alt 310 kt, 357 mph
  cruise Speed Main 460-540 km/h
  cruise Speed Alt 250-290 kt, 290-340 mi
  range Main <br>
  range Alt 490 nm, 560 mi)At 520 km/h (280 kt, 320 mph) at 7,200 m (24,000 ft) with a 6,000 kg (13,000) payload
  ceiling Main m
  ceiling Alt ft
  climb Rate Main m/s
  climb Rate Alt ft/min
  loading Main kg/m&sup2
  loading Alt lb/ft&sup2
  power/mass Main W/kg
  power/mass Alt hp/lb



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