Manufacturer | Cessna |
Model | T-41 Mescalero |
Modification | T-41A |
Country | USA |
Years | 1965 |
Type | Other |
Main rotor diameter | - |
Tail rotor diameter | - |
Wingspan | 10.92 m |
Length | 8.72 m |
Height | 2.72 m |
Wing area | 16.16 m2 |
Zero fuel weight | - |
Empty weight | 815 kg |
Maximum takeoff weight | 1406 kg |
Normal takeoff weight | 1043 kg |
Flight duration | - |
Engine | 1 Continental O-300-C |
Power | 1 x 145 HP |
Thrust | - |
Maximum speed | 223 km/h |
Cruising speed | 188 km/h |
Rate of climb | - |
Practical range | 1160 km |
Service ceiling | 4000 m |
Hovering ceiling | - |
Crew | 2 |