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