Airbus Helicopters H225 vs Bell 525 Relentless vs Pilatus Pc 24
The Airbus H225 and Bell 525 Relentless are large, long-range helicopters aimed at offshore transport, SAR, and VIP missions, while the Pilatus PC-24 is a light business jet designed for fast point-to-point travel, including operations from shorter or semi-prepared runways. In range terms, the H225 typically offers roughly 450–500 nautical miles depending on configuration, whereas the Bell 525 is designed for about 500–600 nautical miles. The PC-24 generally flies much farther, around 1,800–2,000 nautical miles, reflecting the efficiency and speed advantages of a fixed-wing jet for longer trips. Passenger capacity also differs by category: the H225 commonly seats about 19 passengers (with higher-density layouts possible), the Bell 525 is typically configured around 16 passengers, and the PC-24 is usually arranged for about 8–10 passengers in executive seating (with higher-density commuter-style options possible). Overall, the helicopters trade speed and range for vertical-lift access, while the PC-24 prioritizes range and cruise speed but needs a runway.
| Spec | AIRBUS H225 | Bell 525 Relentless | Pilatus PC-24 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | — | $ 3.71 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 21 | 18 | 6 |
| Flight Rules | IFR | IFR | — |
| Manufacturer | Airbus Helicopters | Bell | Pilatus |
| Aircraft Name | H225 | 525 Relentless | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 580 | 2076 |
| DOC / nm / Seat | $ 0.99 | — | $ 0.62 |
| Max Cabin Seats | 28 | 16 | 10 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 6675 | 6680 |
| Standard Cabin Seats | 19 | 16 | 6 |
| Direct Operating Cost | $ 2,963 | — | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Garmin G5000H | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 160 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,000,000 | $11,800,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 21 | 18 | 6 |
| Max Cabin Seats | 28 | 16 | 10 |
| Standard Cabin Seats | 19 | 16 | 6 |
| Lavatory | — | — | 1 Enclosed Flushing |
| Crew Rest | — | — | No |
| Jump Seat | — | — | No |
| Cargo Door | — | — | Yes |
| Galley Location | — | — | FWD |
| Lavatory Location | — | — | FWD |
| Cabin Pressure (psi) | — | — | 9.3 |
| Galley / Refreshment | — | — | Optional Refreshment Center |
| SL Cabin Altitude (ft) | — | — | 23500 |
| Engine | |||
| FADEC | Yes | Dual-Channel | Yes |
| Model | Makila 2A1 | CT7-2F1 | FJ44-4A-QPM |
| Fuel Type | JetFuel | JetFuel | — |
| TBO (hrs) | 3500 | 4000 | 5000 |
| Horsepower | 2100 | 1800 | — |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | 641 | — |
| Flat Rating | — | — | ISA + 23 |
| Thrust (lbs) | — | — | 3435 |
| Dimensions | |||
| Length (ft) | 63.4 | 61.58 | 52.2 |
| Overall Height (ft) | 16.3 | 18.18 | 17.4 |
| Rotor Diameter (ft) | 53.2 | 54.5 | — |
| Cabin Volume (cu. ft) | 547 | — | — |
| Width (ft) | — | 25.77 | — |
| Cabin Width (ft) | — | 7.58 | 5.6 |
| Cabin Height (ft) | — | 4.5 | 5.1 |
| Cabin Length (ft) | — | 15.5 | 23 |
| Baggage Volume Ext. (cu. ft) | — | 128 | — |
| Wingspan (ft) | — | — | 55.8 |
| Aisle Step (ft) | — | — | Flat Floor |
| Cabin Width - Floor (ft) | — | — | 3.8 |
| Cabin Length - Seating (ft) | — | — | 17 |
| Baggage Volume Int. (cu. ft) | — | — | 90 |