Attribute | Piper PA-28 Cherokee × | Grob G-120A × |
---|---|---|
General | ||
Manufacturer | Piper Aircraft | Grob Aircraft |
Model | Piper PA-28 Cherokee | Grob G-120A |
Country | United States | Germany |
Manufactured from (year) | 1961 | 1999 |
Type | Private Single Engine | Aerobatic |
Icao | PA28 | G120 |
Performance | ||
Engine | 1x Lycoming O-320-E2A | 1x 1 × Lycoming AEIO-540-D4D5 6-cylinder |
Power, hp (hp) | 150 | 260 |
Avionics | - | IFR instrumentation with EFIS and King / Bendix components |
Max cruise speed (km/h) | 200 | 319 |
Approach speed (km/h) | 87 | 104 |
Travel range (km) | 861 | 1,537 |
Fuel economy (km/l) | - | 6.996 |
1↑Service ceiling (m) | 4,359 | 5,486 |
Rate of climb (m/sec) | 3.35 | 6.5 |
Take off distance (m) | 502 | 707 |
Landing distance (m) | 564 | 562 |
Weights | ||
Max take off weight (kg) | 975 | 1,490 |
Max landing weight (kg) | 975 | 1,440 |
Max payload (kg) | 421 | 220 |
Fuel tank capacity (l) | 189 | 252 |
Baggage volume (m³) | 0.6 | - |
Dimensions | ||
Seats | 4 | 2 |
Cabin height (m) | 1.09 | - |
Cabin width (m) | 1.01 | - |
Cabin length (m) | 2.5 | - |
Exterior length (m) | 7.1 | 8.11 |
Tail height (m) | 2.22 | 2.66 |
Fuselage diameter (m) | 1.15 | 1.3 |
Wing span (m) | 9.14 | 10.18 |
Wing tips | No Winglets | No Winglets |