| Technical data | |
|---|---|
| Type | An-2P |
| Function | Passenger |
| Year | 1968 |
| Crew | 2 |
| Engines | 1*1000hp ASh-62IR |
| Length | 12.74m |
| Wingspan | 18.18m |
| Wing area | 71.5m2 |
| Empty weight | 3450kg |
| Loaded weight | 5500kg |
| Wing Load (kg/m2) | 76.9 |
| Power load (kg/hp) | 5.5 |
| Speed at 0m | km/h |
| Max Speed at 1750m | 258km/h |
| Economy Speed | 185km/h |
| T-O Speed | 80km/h |
| Landing Speed | 85km/h |
| Landing Roll (hard and grass runways) | 170m 185m |
| Takeoff Roll (hard and grass runways) | 150m 170m |
| Range | 900km |
| Service Ceiling | 4400m |
| Climb | |
| at 0m | 210m/min |
| Payload | |
| Seats | 12...14 |
| Load (baggage) | 200kg |
An-2P, O.K.Antonov
 |
Dedicated passenger version of the An-2. Unlike transport and agricultural variants, An-2P cabin walls are covered with sound absorbing mats. Built in Poland with new propeller and spinner, weight-saving instruments and equipment.
12 light passenger seats are installed in four rows of three with center aisle. Two foldable seats for children in aisle between first and second rows. Toilet at rear cabin on starboard side. Overhead racks for up to 160kg of baggage, with space for coats and additional 40kg of baggage between rear pair of seats and toilet.
Emergency exit on starboard side at rear. Cabin ventilation by ram-air intakes.
| References | ||
|---|---|---|
|
||
| Links | ||
|
|
|
