| Technical data | |
|---|---|
| Type | An-14M |
| Function | Transport |
| Year | 1969 |
| Crew | 2 |
| Engines | 2*810hp TVD-650 turboprop |
| Fuel consumption (take-off) | 280g/hp/hour |
| Fuel consumption (cruise) | ?g/hp/hour |
| Length | 13.0m |
| Height | 4.6m |
| Wingspan | 22.0m |
| Wing area | 39.7m2 |
| Empty weight | 3500kg |
| Loaded weight (normal) | 5600kg |
| Wing Load (kg/m2) | 141 |
| Power load (kg/hp) | 3.46 |
| Cruising Speed at 2000m | 304km/h |
| Maximum Speed | 350km/h |
| Landing Speed | ?km/h |
| Landing Roll | 200m |
| Takeoff Roll | 215m |
| Operational Range | 1000km |
| Service Ceiling | 6000m |
| Payload | |
| Fuel | ?kg |
| Cabin size | 3.1x1.53x1.6m3 |
| Seats | 15 |
| Cargo | ?kg |
An-14M by O.K.Antonov 'Clod'
Turboprop development of the An-14 STOL transport. Flown first time in Kiev (September 1969) by V.Terskij, An-14M passed trials in the middle 1972. Except the cabin stretch (both forward and backward), the tail unit was redesigned again. One of intermediate configurations had retractable landing gear, but weigh drawback and reliability concerns resulted in revert to the original fixed type.
Like its predecessor, An-14M was also built following variants:
- passenger (15 seats);
- executive (6-7 seats);
- agricultural (1,300kg chemicals);
| References | Links |
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