Airbus Helicopters H225 vs Beechcraft King Air 360 Er vs Bombardier Global 7500 vs Pilatus Pc 24
The Airbus H225 is a heavy twin‑engine helicopter, best suited to offshore, SAR, and utility missions. Its range is roughly in the 500–650 nm class (mission dependent), and it typically carries about 16–19 passengers in high‑density seating (fewer in mission or VIP layouts). The Beechcraft King Air 360ER is a twin‑turboprop aircraft optimized for efficient regional and special‑mission flying. It offers long endurance for its class with range around 1,500–1,800 nm (configuration dependent) and commonly seats 8–11 passengers in executive layouts. The Pilatus PC‑24 is a light jet designed for versatility, including operations from shorter or semi‑prepared runways. Its range is about 2,000 nm and typical seating is around 6–10 passengers depending on cabin configuration. The Bombardier Global 7500 is an ultra‑long‑range large‑cabin business jet aimed at intercontinental travel. It can fly roughly 7,700 nm and usually accommodates about 14–19 passengers, with multiple living zones in high‑end layouts.
| Spec | AIRBUS H225 | Bombardier Global 7500 | Pilatus PC-24 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 9.50 | $ 3.71 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 21 | 14 | 6 |
| Flight Rules | IFR | — | — |
| Manufacturer | Airbus Helicopters | Bombardier | Pilatus |
| Aircraft Name | H225 | Global 7500 | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 7700 | 2076 |
| DOC / nm / Seat | $ 0.99 | $ 0.79 | $ 0.62 |
| Max Cabin Seats | 28 | 19 | 10 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | — | 6680 |
| Standard Cabin Seats | 19 | 12 | 6 |
| Direct Operating Cost | $ 2,963 | $ 4,900 | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Bombardier Vision (Pro Line Fusion) | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 516 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $75,000,000 | $11,800,000 |
| Aircraft Type | — | Business Jet | — |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 21 | 14 | 6 |
| Max Cabin Seats | 28 | 19 | 10 |
| Standard Cabin Seats | 19 | 12 | 6 |
| Lavatory | — | 2 Enclosed Flushing | 1 Enclosed Flushing |
| Crew Rest | — | Yes | No |
| Jump Seat | — | Yes | No |
| Galley Location | — | FWD | FWD |
| Lavatory Location | — | FWD / AFT | FWD |
| Galley / Refreshment | — | Galley | Optional Refreshment Center |
| Max Cabin Altitude (ft) | — | 4500 | — |
| Cargo Door | — | — | Yes |
| Cabin Pressure (psi) | — | — | 9.3 |
| SL Cabin Altitude (ft) | — | — | 23500 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Makila 2A1 | Passport | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | On-Condition | 5000 |
| Horsepower | 2100 | — | — |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — |
| Flat Rating | — | ISA + 15 | ISA + 23 |
| Thrust (lbs) | — | 18920 | 3435 |
| Dimensions | |||
| Length (ft) | 63.4 | 111 | 52.2 |
| Overall Height (ft) | 16.3 | 27 | 17.4 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | — |
| Wingspan (ft) | — | 104 | 55.8 |
| Cabin Width (ft) | — | 8 | 5.6 |
| Cabin Height (ft) | — | 6.2 | 5.1 |
| Cabin Length (ft) | — | 54.5 | 23 |
| Aisle Step (ft) | — | — | Flat Floor |
| Cabin Width - Floor (ft) | — | — | 3.8 |
| Cabin Length - Seating (ft) | — | — | 17 |
| Baggage Volume Int. (cu. ft) | — | — | 90 |