| Summary |
| Cockpit | 2 | 2 |
| DOC / nm | $ 4.37 | $ 20.87 |
| Min Crew | 1 | 2 |
| Total Seats | 10 | 21 |
| Flight Rules | IFR | IFR |
| Manufacturer | Beechcraft | Airbus Helicopters |
| Aircraft Name | KingAir 350ER | H225 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 2338 | 454 |
| DOC / nm / Seat | $ 0.55 | $ 0.99 |
| Max Cabin Seats | 9 | 28 |
| OEM Verification | VERIFIED | Un-Verified |
| Useful Load (lbs) | 6585 | 11929 |
| Standard Cabin Seats | 8 | 19 |
| Direct Operating Cost | $ 1,324 | $ 2,963 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | EFIS |
| Max Cruise Speed (ktas) | 303 | 142 |
| Base Aircraft Price (USD) | $8,750,000 | $ 29,500,000 |
| Cabin |
| Cockpit | 2 | 2 |
| Lavatory | Yes (Belted Optional) | — |
| Min Crew | 1 | 2 |
| Cargo Door | Optional | — |
| Total Seats | 10 | 21 |
| Galley Location | FWD | — |
| Max Cabin Seats | 9 | 28 |
| Lavatory Location | AFT | — |
| Cabin Pressure (psi) | 6.5 | — |
| Galley / Refreshment | Refreshment Center | — |
| Standard Cabin Seats | 8 | 19 |
| Engine |
| FADEC | Yes | Yes |
| Model | PT6A-60A | Makila 2A1 |
| TBO (hrs) | 3600 | 3500 |
| Horsepower | 1050 | 2100 |
| Flat Rating | ISA + 10 | — |
| No. of Engines | 1 | 2 |
| Fuel Capacity (gal) | 775 | 684 |
| Fuel Type | — | JetFuel |
| Dimensions |
| Length (ft) | 46.7 | 63.4 |
| Wingspan (ft) | 57.9 | — |
| Cabin Width (ft) | 4.5 | — |
| Cabin Height (ft) | 4.8 | — |
| Cabin Length (ft) | 19.5 | — |
| Overall Height (ft) | 14.4 | 16.3 |
| Cabin Width - Floor (ft) | 4.1 | — |
| Cabin Length - Seating (ft) | 19.5 | — |
| Baggage Volume Int. (cu. ft) | 71 | — |
| Rotor Diameter (ft) | — | 53.2 |
| Cabin Volume (cu. ft) | — | 547 |
