Airbus Helicopters H225 vs Bell 525 Relentless vs Dassault Falcon 8x vs Pilatus Pc 24
The Airbus H225 and Bell 525 Relentless are large helicopters built for vertical lift missions rather than point‑to‑point jet travel. The H225 is a heavy, long‑range twin‑engine rotorcraft typically carrying about 19 passengers in standard seating (more in high‑density), with practical mission ranges roughly in the 400–500+ nautical mile class depending on payload and reserves. The Bell 525 is a modern “super‑medium” helicopter, usually configured for around 16 passengers, with broadly similar order‑of‑magnitude range, often cited around the 500‑nautical‑mile class depending on configuration. The Dassault Falcon 8X is a long‑range, large‑cabin business jet designed for intercontinental missions, typically seating 12–16 passengers, with a range around 6,450 nautical miles. The Pilatus PC‑24 is a light jet optimized for versatility and short/rough runway access, generally seating 6–10 passengers, with range around 2,000 nautical miles (varies with load and reserves).
| Spec | AIRBUS H225 | Bell 525 Relentless | Dassault Falcon 8X | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | — | $ 7.66 | $ 3.71 |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 21 | 18 | 17 | 6 |
| Flight Rules | IFR | IFR | — | — |
| Manufacturer | Airbus Helicopters | Bell | Dassault Falcon | Pilatus |
| Aircraft Name | H225 | 525 Relentless | 8X | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 580 | 6450 | 2076 |
| DOC / nm / Seat | $ 0.99 | — | $ 0.64 | $ 0.62 |
| Max Cabin Seats | 28 | 16 | 16 | 10 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 6675 | 36900 | 6680 |
| Standard Cabin Seats | 19 | 16 | 14 | 6 |
| Direct Operating Cost | $ 2,963 | — | $ 3,805 | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Garmin G5000H | Honeywell Primus EASy II | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 160 | 516 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,000,000 | $ 62,500,000 | $11,800,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 21 | 18 | 17 | 6 |
| Max Cabin Seats | 28 | 16 | 16 | 10 |
| Standard Cabin Seats | 19 | 16 | 14 | 6 |
| Lavatory | — | — | 2 Enclosed Flushing | 1 Enclosed Flushing |
| Crew Rest | — | — | No | No |
| Jump Seat | — | — | Yes | No |
| Galley Location | — | — | FWD | FWD |
| Lavatory Location | — | — | FWD / AFT | FWD |
| Cabin Pressure (psi) | — | — | 10.2 | 9.3 |
| Galley / Refreshment | — | — | Galley | Optional Refreshment Center |
| SL Cabin Altitude (ft) | — | — | 29200 | 23500 |
| Max Cabin Altitude (ft) | — | — | 3900 | — |
| Cargo Door | — | — | — | Yes |
| Engine | ||||
| FADEC | Yes | Dual-Channel | Yes | Yes |
| Model | Makila 2A1 | CT7-2F1 | PW307D | FJ44-4A-QPM |
| Fuel Type | JetFuel | JetFuel | — | — |
| TBO (hrs) | 3500 | 4000 | On-Condition | 5000 |
| Horsepower | 2100 | 1800 | — | — |
| No. of Engines | 2 | 2 | 3 | 2 |
| Fuel Capacity (gal) | 684 | 641 | — | — |
| Flat Rating | — | — | ISA + 17 | ISA + 23 |
| Thrust (lbs) | — | — | 6722 | 3435 |
| Dimensions | ||||
| Length (ft) | 63.4 | 61.58 | 80.2 | 52.2 |
| Overall Height (ft) | 16.3 | 18.18 | 26.1 | 17.4 |
| Rotor Diameter (ft) | 53.2 | 54.5 | — | — |
| Cabin Volume (cu. ft) | 547 | — | 1695 | — |
| Width (ft) | — | 25.77 | — | — |
| Cabin Width (ft) | — | 7.58 | 7.7 | 5.6 |
| Cabin Height (ft) | — | 4.5 | 6.2 | 5.1 |
| Cabin Length (ft) | — | 15.5 | 42.7 | 23 |
| Baggage Volume Ext. (cu. ft) | — | 128 | — | — |
| Wingspan (ft) | — | — | 86.3 | 55.8 |
| Cabin Width - Floor (ft) | — | — | 6.3 | 3.8 |
| Cabin Length - Seating (ft) | — | — | 29.2 | 17 |
| Baggage Volume Int. (cu. ft) | — | — | 140 | 90 |
| Aisle Step (ft) | — | — | — | Flat Floor |