Iran-140 (Antonov 140)
| Specifications | |
|---|---|
| Physical | |
| Aicraft Length | 22.605 m |
| Wingspan | 24.505 (25.505) m |
| Height | 8.232 m |
| Landing Gear Track | 3.18 m |
| Wheel Base | 8.162 m |
| Nose Wheels | 0.6 x 0.22 m |
| Main Wheels | 0.81 x 0.32 m |
| Under Floor Baggage Volume | 3 m3 |
| Transport Compartment Length | 14.51 m |
| Rear Baggage/Cargo Compartment Volume | 6.1 m3 |
| Rear Baggage/Cargo Compartment Volume | 6.1 m3 |
| Performance | |
| Maximum Take Off Weight | 21,000 (21,500) kg / 46,200 (47,300) lb3 |
| Maximum Landing Weight | 21,000 kg (46,200 lb)3 |
| Maximum Weight (Without Fuel) | 19,100 (19,200) kg / 42,020 (42,240) lb |
| Maximum Payload Weight | 6,000 kg (13,200 lb) |
| Maximum Fuel Weight | 4,370 kg (9,614 lb) |
| Take Off Run (1 Engine)* | 1,350 m (4,415 ft) |
| Take Off Distance (1 Engine)* | 1,750 (1,925) m / 5,740 (6,314) ft |
| Landing Distance* | 1,360 m (4,460 ft) |
| Climb (2 Engines)* | 410 m/min (1,345 ft/min) |
| Maximum Cruise Speed* | 533 km/h (285 KTAS) |
| Range (Cruise Speed)* | 2,100 km (1,134 nm) |
* - MTOW, ISA,SL
