Manufacturer | Cessna |
Model | Cessna 172(A-I) Skyhawk |
Modification | Cessna 172A |
Country | USA |
Years | 1955 |
Type | Light aircraft |
Main rotor diameter | - |
Tail rotor diameter | - |
Wingspan | 10.92 m |
Length | 8.20 m |
Height | 2.59 m |
Wing area | 16.20 m2 |
Zero fuel weight | - |
Empty weight | 572 kg |
Maximum takeoff weight | 998 kg |
Normal takeoff weight | - |
Flight duration | - |
Engine | 1 Continental O300A |
Power | 1 x 145 HP |
Thrust | - |
Maximum speed | 217 km/h |
Cruising speed | 200 km/h |
Rate of climb | - |
Practical range | 1000 km |
Service ceiling | 4572 m |
Hovering ceiling | - |
Crew | 1 |