Attribute | ![]() Cessna 182 × | ![]() Grob G-120A × |
---|---|---|
General | ||
Manufacturer | Cessna | Grob Aircraft |
Model | Cessna 182 | Grob G-120A |
Country | United States | Germany |
Manufactured from (year) | 1956 | 1999 |
Type | Private Single Engine | Aerobatic |
Icao | C182 | G120 |
Performance | ||
Engine | 1x Lycoming IO-540-AB1A5 | 1x 1 × Lycoming AEIO-540-D4D5 6-cylinder |
Power, hp (hp) | 230 | 260 |
Avionics | Garmin G1000 glass cockpit | IFR instrumentation with EFIS and King / Bendix components |
Max cruise speed (km/h) | 278 | 319 |
Approach speed (km/h) | 91 | 104 |
Travel range (km) | 1,695 | 1,537 |
Fuel economy (km/l) | 4.941 | 6.996 |
Service ceiling (m) | 5,517 | 5,486 |
Rate of climb (m/sec) | 4.69 | 6.5 |
Take off distance (m) | 461 | 707 |
Landing distance (m) | 411 | 562 |
Weights | ||
Max take off weight (kg) | 1,406 | 1,490 |
Max landing weight (kg) | 1,338 | 1,440 |
Max payload (kg) | 503 | 220 |
Fuel tank capacity (l) | 348 | 252 |
Baggage volume (m³) | 0.91 | - |
Dimensions | ||
Seats | 4 | 2 |
Cabin height (m) | 1.2 | - |
Cabin width (m) | 1.07 | - |
Cabin length (m) | 3.4 | - |
Exterior length (m) | 8.8 | 8.11 |
Tail height (m) | 2.8 | 2.66 |
Fuselage diameter (m) | 1.1 | 1.3 |
Wing span (m) | 10.97 | 10.18 |
Wing tips | No Winglets | No Winglets |