Honda Aircraft Hondajet Elite vs Piaggio Avanti Evo vs Cirrus Sf50 G2
The Honda Aircraft HondaJet Elite and the Cirrus SF50 G2 are both single‑pilot certified very light jets, while the Piaggio Avanti EVO is a larger, twin‑turboprop with a distinctly different mission profile. In category terms, the HondaJet Elite emphasizes efficient short‑to‑medium business hops with jet speed in a compact airframe; the SF50 G2 targets owner‑pilots seeking jet simplicity and a signature whole‑aircraft parachute; the Avanti EVO sits in a step‑up class, offering turboprop economics with near‑light‑jet cruise performance. On range, the SF50 G2 generally leads among these three, with typical published capability around 1,200 nautical miles, while the HondaJet Elite is usually quoted around 1,100–1,200 nautical miles depending on variant and reserves. The Avanti EVO typically offers roughly 1,400–1,700 nautical miles, varying with payload and speed settings, and can be very competitive for longer legs at efficient cruise. Passenger capacity differs most: the HondaJet Elite and SF50 G2 commonly seat about 4–5 passengers plus a pilot, whereas the Avanti EVO is typically configured for about 6–7 passengers plus crew, with a roomier cabin.
| Spec | Honda Aircraft HondaJet Elite | Piaggio Avanti EVO |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 2.73 | — |
| Min Crew | 1 | 1 |
| Total Seats | 6 | 8 |
| Manufacturer | Honda Aircraft | Piaggio |
| Aircraft Name | HondaJet Elite | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1495 | 1530 |
| DOC / nm / Seat | $ 0.68 | — |
| Max Cabin Seats | 6 | 7 |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 3432 | 3775 |
| Standard Cabin Seats | 4 | 6 |
| Direct Operating Cost | $ 1,135 | — |
| Flight Deck (Base Spec) | Garmin G3000 | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 419 | 400 |
| Base Aircraft Price (USD) | $ 5,400,000 | $ 7,695,000 |
| Flight Rules | — | IFR |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | 1 Enclosed Flushing | No |
| Min Crew | 1 | 1 |
| Crew Rest | No | — |
| Jump Seat | No | — |
| Total Seats | 6 | 8 |
| Galley Location | FWD | — |
| Max Cabin Seats | 6 | 7 |
| Lavatory Location | AFT | — |
| Cabin Pressure (psi) | 8.8 | 9 |
| Galley / Refreshment | Galley | No |
| Standard Cabin Seats | 4 | 6 |
| SL Cabin Altitude (ft) | 23060 | 24000 |
| Max Cabin Altitude (ft) | — | 6600 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | HF120-H1A | PT6A–66B |
| TBO (hrs) | 5000 | 3600 |
| Flat Rating | ISA + 10 | ISA + 28 |
| Thrust (lbs) | 2050 | — |
| No. of Engines | 2 | 2 |
| Fuel Capacity (gal) | 439 | — |
| Horsepower | — | 850 |
| Fuel Burn (gph) | — | 100 |
| Dimensions | ||
| Length (ft) | 42.7 | 47.3 |
| Wingspan (ft) | 39.8 | 47.1 |
| Aisle Step (ft) | 0.4 | — |
| Cabin Width (ft) | 5 | 6.1 |
| Cabin Height (ft) | 4.8 | 5.8 |
| Cabin Length (ft) | 12.1 | 14.9 |
| Overall Height (ft) | 14.9 | 13.1 |
| Cabin Length - Seating (ft) | 10.2 | — |
| Baggage Volume Ext. (cu. ft) | 66 | — |
| Cabin Width - Floor (ft) | — | 3.5 |
| Baggage Volume Int. (cu. ft) | — | 35.2 |