Airbus Helicopters H225 vs Beechcraft King Air 360 Er vs Gulfstream G700 vs Pilatus Pc 24
The Airbus H225 is a heavy twin‑engine helicopter optimized for vertical lift missions rather than point‑to‑point cruise; its typical range is roughly 450–550 nautical miles (depending on payload and reserves) and it commonly carries about 16–19 passengers in offshore/utility layouts (more in high‑density configurations). The Beechcraft King Air 360ER is a twin‑turboprop utility aircraft suited to short and midsize regional missions; it offers about 1,500–1,800 nautical miles of range and usually seats 6–9 passengers in executive trim (more in commuter/utility layouts). The Gulfstream G700 is an ultra‑long‑range large‑cabin business jet designed for intercontinental travel; it reaches about 7,500 nautical miles and typically carries around 13–19 passengers depending on cabin configuration. The Pilatus PC‑24 is a light jet with strong short/rough‑field capability; it delivers about 1,700–2,000 nautical miles of range and generally seats 6–10 passengers. Overall, the G700 leads on range and cabin size, the H225 trades speed and range for VTOL access, and the King Air 360ER and PC‑24 sit in the middle as versatile regional platforms.
| Spec | AIRBUS H225 | Gulfstream G700 | Pilatus PC-24 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 3 | 2 |
| DOC / nm | $ 20.87 | — | $ 3.71 |
| Min Crew | 2 | 4 | 1 |
| Total Seats | 21 | 16 | 6 |
| Flight Rules | IFR | — | — |
| Manufacturer | Airbus Helicopters | Gulfstream | Pilatus |
| Aircraft Name | H225 | G700 | PC-24 |
| Certification | FAA / EASA | In Development | FAA / EASA |
| Max Range (nm) | 454 | 7500 | 2076 |
| DOC / nm / Seat | $ 0.99 | — | $ 0.62 |
| Max Cabin Seats | 28 | 19 | 10 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | — | 6680 |
| Standard Cabin Seats | 19 | 12 | 6 |
| Direct Operating Cost | $ 2,963 | — | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Gulfstream Symmetry Flight Deck | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 516 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $78,000,000 | $11,800,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 1 |
| Total Seats | 21 | 16 | 6 |
| Max Cabin Seats | 28 | 19 | 10 |
| Standard Cabin Seats | 19 | 12 | 6 |
| Crew Rest | — | Optional | No |
| Jump Seat | — | Yes | No |
| Galley Location | — | FWD | FWD |
| Lavatory Location | — | FWD / AFT | FWD |
| Lavatory | — | — | 1 Enclosed Flushing |
| Cargo Door | — | — | Yes |
| Cabin Pressure (psi) | — | — | 9.3 |
| Galley / Refreshment | — | — | Optional Refreshment Center |
| SL Cabin Altitude (ft) | — | — | 23500 |
| Engine | |||
| FADEC | Yes | — | Yes |
| Model | Makila 2A1 | Pearl 700 | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | On Condition | 5000 |
| Horsepower | 2100 | — | — |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — |
| Thrust (lbs) | — | 18250 | 3435 |
| Flat Rating | — | — | ISA + 23 |
| Dimensions | |||
| Length (ft) | 63.4 | 109.9 | 52.2 |
| Overall Height (ft) | 16.3 | 25.4 | 17.4 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | — |
| Wingspan (ft) | — | 103 | 55.8 |
| Aisle Step (ft) | — | Flat Floor | Flat Floor |
| Cabin Width (ft) | — | 8.2 | 5.6 |
| Cabin Height (ft) | — | 6.25 | 5.1 |
| Cabin Length (ft) | — | 56.9 | 23 |
| Baggage Volume Int. (cu. ft) | — | 195 | 90 |
| Cabin Width - Floor (ft) | — | — | 3.8 |
| Cabin Length - Seating (ft) | — | — | 17 |