Grob G-120A [+]Compare [E]dit [H]istory
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| Attribute | Value |
|---|---|
| General | |
| Manufacturer | Grob Aircraft |
| Model | Grob G-120A |
| Country | Germany |
| Manufactured from | 1999 year |
| Manufactured to | Add |
| Type | Aerobatic |
| Icao | G120 |
| Performance | |
| Engine | 1x 1 × Lycoming AEIO-540-D4D5 6-cylinder |
| Power, hp | 260 hp |
| Power, lbf | Add |
| Avionics | IFR instrumentation with EFIS and King / Bendix components |
| Max cruise speed | 319 km/h |
| Approach speed | 104 km/h |
| Travel range | 1,537 km |
| Fuel economy | 6.996 km/l |
| Service ceiling | 5,486 m |
| Rate of climb | 6.5 m/sec |
| Take off distance | 707 m |
| Landing distance | 562 m |
| Weights | |
| Max take off weight | 1,490 kg |
| Max landing weight | 1,440 kg |
| Max payload | 220 kg |
| Fuel tank capacity | 252 l |
| Baggage volume | Add |
| Dimensions | |
| Seats | 2 |
| Seats - business class | Add |
| Seats - first class | Add |
| Cabin height | Add |
| Cabin width | Add |
| Cabin length | Add |
| Exterior length | 8.11 m |
| Tail height | 2.66 m |
| Fuselage diameter | 1.3 m |
| Wing span | 10.18 m |
| Wing tips | No Winglets |
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There was one edit, no edits waiting approval. Last edited by qjast(1747), Oct 25, 2021 (42 fields were changed)
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