An-26, O.K.Antonov 'Curl'
T actical transport, development of the An-24.
The An-26 like the An-24RV has an auxiliary turbojet in the right engine nacell, used for high-and-hot operations. The An-26 has
a rear loading ramp and decreased number of cabin windows..
| Technical data | ||
|---|---|---|---|
| Type | An-26 | ||
| Function | Passenger Cargo | ||
| Year | 1969 | ||
| Crew | 4...5 | ||
| Engines | 2*2820hp AI-24T
1*7.85kN RU-19-300 | ||
| Length | 23.8m | ||
| Height | 8.58m | ||
| Wingspan | 29.2m | ||
| Wing area | 75m2 | ||
| Empty weight | 14750kg | ||
| Maximum takeoff weight | 24000kg | ||
| Wing load | 320kg/m2 | ||
| Power load | 4.26kg/hp | ||
| Maximum Speed at 6000m | 540km/h | ||
| Cruise Speed at 6000m | 440km/h | ||
| Landing Speed | 175km/h | ||
| Landing Roll | 610m | ||
| Takeoff Roll | 640m | ||
| Ferry Range | 2250km | ||
| Range with maximum load | 980km | ||
| Ceiling | 7500m | ||
| Climb | |||
| at 0m | 3.3m/sec | ||
| Payload | |||
| Fuel | ?kg | ||
| Seats | 40 | ||
| Cargo | 5500kg | ||
| Created March 27, 1997
Modified March 11, 1999 by Alexandre Savine |
Back to Main Gate |