Airbus Helicopters H225 vs Bell 525 Relentless vs Bombardier Global 7500 vs Pilatus Pc 24
The Airbus H225 and Bell 525 Relentless are large, long-range helicopters aimed at offshore, SAR, and executive transport, while the Bombardier Global 7500 and Pilatus PC-24 are fixed‑wing business jets for fast, high‑altitude travel. In range terms, the Global 7500 is in a different league, offering roughly 7,700 nautical miles, enabling ultra‑long‑haul intercontinental missions. The PC‑24 is a light jet with a much shorter range, roughly around 2,000 nautical miles class, but it stands out for operating from shorter or unimproved runways compared with most business jets. The H225 typically offers around 450–500 nautical miles depending on configuration and reserves, whereas the Bell 525 targets a similar but often somewhat higher range bracket, roughly around 550–650 nautical miles. For passenger capacity, the Global 7500 commonly seats about 14–19 in executive layouts, the PC‑24 typically around 6–10, the H225 can carry a large cabin load (often around 16–19 and higher in high‑density utility layouts), and the Bell 525 is generally in the mid‑teens for typical passenger seating.
| Spec | AIRBUS H225 | Bell 525 Relentless | Bombardier Global 7500 | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | — | $ 9.50 | $ 3.71 |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 21 | 18 | 14 | 6 |
| Flight Rules | IFR | IFR | — | — |
| Manufacturer | Airbus Helicopters | Bell | Bombardier | Pilatus |
| Aircraft Name | H225 | 525 Relentless | Global 7500 | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 580 | 7700 | 2076 |
| DOC / nm / Seat | $ 0.99 | — | $ 0.79 | $ 0.62 |
| Max Cabin Seats | 28 | 16 | 19 | 10 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 6675 | — | 6680 |
| Standard Cabin Seats | 19 | 16 | 12 | 6 |
| Direct Operating Cost | $ 2,963 | — | $ 4,900 | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Garmin G5000H | Bombardier Vision (Pro Line Fusion) | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 160 | 516 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,000,000 | $75,000,000 | $11,800,000 |
| Aircraft Type | — | — | Business Jet | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 21 | 18 | 14 | 6 |
| Max Cabin Seats | 28 | 16 | 19 | 10 |
| Standard Cabin Seats | 19 | 16 | 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 | Dual-Channel | Yes | Yes |
| Model | Makila 2A1 | CT7-2F1 | Passport | FJ44-4A-QPM |
| Fuel Type | JetFuel | JetFuel | — | — |
| TBO (hrs) | 3500 | 4000 | On-Condition | 5000 |
| Horsepower | 2100 | 1800 | — | — |
| No. of Engines | 2 | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | 641 | — | — |
| Flat Rating | — | — | ISA + 15 | ISA + 23 |
| Thrust (lbs) | — | — | 18920 | 3435 |
| Dimensions | ||||
| Length (ft) | 63.4 | 61.58 | 111 | 52.2 |
| Overall Height (ft) | 16.3 | 18.18 | 27 | 17.4 |
| Rotor Diameter (ft) | 53.2 | 54.5 | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | — |
| Width (ft) | — | 25.77 | — | — |
| Cabin Width (ft) | — | 7.58 | 8 | 5.6 |
| Cabin Height (ft) | — | 4.5 | 6.2 | 5.1 |
| Cabin Length (ft) | — | 15.5 | 54.5 | 23 |
| Baggage Volume Ext. (cu. ft) | — | 128 | — | — |
| Wingspan (ft) | — | — | 104 | 55.8 |
| Aisle Step (ft) | — | — | — | Flat Floor |
| Cabin Width - Floor (ft) | — | — | — | 3.8 |
| Cabin Length - Seating (ft) | — | — | — | 17 |
| Baggage Volume Int. (cu. ft) | — | — | — | 90 |