Airbus Helicopters H225 vs Beechcraft King Air 360 Er vs Gulfstream G700 vs Piaggio Avanti Evo
| Spec | Gulfstream G700 | Beechcraft King Air 360ER | AIRBUS H225 | Piaggio Avanti EVO |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 3 | 2 | 2 | 2 |
| Min Crew | 4 | 1 | 2 | 1 |
| Total Seats | 16 | 10 | 21 | 8 |
| Manufacturer | Gulfstream | Beechcraft | Airbus Helicopters | Piaggio |
| Aircraft Name | G700 | KingAir 350ER | H225 | Avanti EVO |
| Certification | In Development | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 7500 | 2338 | 454 | 1530 |
| Max Cabin Seats | 19 | 9 | 28 | 7 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | Un-Verified |
| Standard Cabin Seats | 12 | 8 | 19 | 6 |
| Flight Deck (Base Spec) | Gulfstream Symmetry Flight Deck | Rockwell Collins Pro Line Fusion | EFIS | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 516 | 303 | 142 | 400 |
| Base Aircraft Price (USD) | $78,000,000 | $8,750,000 | $ 29,500,000 | $ 7,695,000 |
| DOC / nm | — | $ 4.37 | $ 20.87 | — |
| Flight Rules | — | IFR | IFR | IFR |
| DOC / nm / Seat | — | $ 0.55 | $ 0.99 | — |
| Useful Load (lbs) | — | 6585 | 11929 | 3775 |
| Direct Operating Cost | — | $ 1,324 | $ 2,963 | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 4 | 1 | 2 | 1 |
| Crew Rest | Optional | — | — | — |
| Jump Seat | Yes | — | — | — |
| Total Seats | 16 | 10 | 21 | 8 |
| Galley Location | FWD | FWD | — | — |
| Max Cabin Seats | 19 | 9 | 28 | 7 |
| Lavatory Location | FWD / AFT | AFT | — | — |
| Standard Cabin Seats | 12 | 8 | 19 | 6 |
| Lavatory | — | Yes (Belted Optional) | — | No |
| Cargo Door | — | Optional | — | — |
| Cabin Pressure (psi) | — | 6.5 | — | 9 |
| Galley / Refreshment | — | Refreshment Center | — | No |
| SL Cabin Altitude (ft) | — | — | — | 24000 |
| Max Cabin Altitude (ft) | — | — | — | 6600 |
| Engine | ||||
| Model | Pearl 700 | PT6A-60A | Makila 2A1 | PT6A–66B |
| TBO (hrs) | On Condition | 3600 | 3500 | 3600 |
| Thrust (lbs) | 18250 | — | — | — |
| No. of Engines | 2 | 1 | 2 | 2 |
| FADEC | — | Yes | Yes | Yes |
| Horsepower | — | 1050 | 2100 | 850 |
| Flat Rating | — | ISA + 10 | — | ISA + 28 |
| Fuel Capacity (gal) | — | 775 | 684 | — |
| Fuel Type | — | — | JetFuel | — |
| Fuel Burn (gph) | — | — | — | 100 |
| Dimensions | ||||
| Length (ft) | 109.9 | 46.7 | 63.4 | 47.3 |
| Wingspan (ft) | 103 | 57.9 | — | 47.1 |
| Aisle Step (ft) | Flat Floor | — | — | — |
| Cabin Width (ft) | 8.2 | 4.5 | — | 6.1 |
| Cabin Height (ft) | 6.25 | 4.8 | — | 5.8 |
| Cabin Length (ft) | 56.9 | 19.5 | — | 14.9 |
| Overall Height (ft) | 25.4 | 14.4 | 16.3 | 13.1 |
| Baggage Volume Int. (cu. ft) | 195 | 71 | — | 35.2 |
| Cabin Width - Floor (ft) | — | 4.1 | — | 3.5 |
| Cabin Length - Seating (ft) | — | 19.5 | — | — |
| Rotor Diameter (ft) | — | — | 53.2 | — |
| Cabin Volume (cu. ft) | — | — | 547 | — |