Bell 525 Relentless vs Boeing Bbj Max 9 vs Dassault Falcon 8x vs Pilatus Pc 24
The Bell 525 Relentless is a super‑medium helicopter, best suited to point‑to‑point missions with vertical access. It typically carries about 16 passengers in an offshore-style layout (often fewer in executive fit) and offers roughly 500–600 nautical miles of range, trading speed and range for hover capability and access to helipads. The Boeing BBJ MAX 9 is a large, long‑range VIP airliner. It can be configured for a few dozen passengers in luxury (while the airframe is capable of far more in airline seating) and delivers intercontinental range on the order of about 6,000–6,500 nautical miles, emphasizing space, payload, and global legs. The Dassault Falcon 8X is an ultra‑long‑range business jet, typically carrying around 12–16 passengers with range around 6,400 nautical miles, balancing nonstop intercontinental capability with business-jet operating flexibility. The Pilatus PC‑24 is a light jet aimed at versatility, commonly seating about 6–10 passengers and offering roughly 2,000 nautical miles of range, with the standout advantage of operating from shorter, more rugged runways than most jets.
| Spec | Bell 525 Relentless | Boeing BBJ MAX 9 | Dassault Falcon 8X | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 2 | 1 |
| Total Seats | 18 | 12 | 17 | 6 |
| Flight Rules | IFR | — | — | — |
| Manufacturer | Bell | Boeing | Dassault Falcon | Pilatus |
| Aircraft Name | 525 Relentless | BBJ MAX 9 | 8X | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 6376 | 6450 | 2076 |
| Max Cabin Seats | 16 | 35 | 16 | 10 |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 6675 | 77120 | 36900 | 6680 |
| Standard Cabin Seats | 16 | 8 | 14 | 6 |
| Flight Deck (Base Spec) | Garmin G5000H | Honeywell | Honeywell Primus EASy II | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 160 | 470 | 516 | 440 |
| Base Aircraft Price (USD) | $15,000,000 | $107,700,000 | $ 62,500,000 | $11,800,000 |
| DOC / nm | — | $ 15.74 | $ 7.66 | $ 3.71 |
| DOC / nm / Seat | — | $ 1.97 | $ 0.64 | $ 0.62 |
| Direct Operating Cost | — | $ 7,396 | $ 3,805 | $ 1,619 |
| Cabin | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| Min Crew | 2 | 4 | 2 | 1 |
| Total Seats | 18 | 10 | 17 | 6 |
| Max Cabin Seats | 16 | 35 | 16 | 10 |
| Standard Cabin Seats | 16 | 8 | 14 | 6 |
| Configuration | — | Green Interior | — | — |
| Cabin Pressure (psi) | — | 9 | 10.2 | 9.3 |
| SL Cabin Altitude (ft) | — | 24000 | 29200 | 23500 |
| Lavatory | — | — | 2 Enclosed Flushing | 1 Enclosed Flushing |
| Crew Rest | — | — | No | No |
| Jump Seat | — | — | Yes | No |
| Galley Location | — | — | FWD | FWD |
| Lavatory Location | — | — | FWD / AFT | FWD |
| Galley / Refreshment | — | — | Galley | Optional Refreshment Center |
| Max Cabin Altitude (ft) | — | — | 3900 | — |
| Cargo Door | — | — | — | Yes |
| Engine | ||||
| FADEC | Dual-Channel | Yes | Yes | Yes |
| Model | CT7-2F1 | LEAP-1B | PW307D | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 4000 | On-Condition | On-Condition | 5000 |
| Horsepower | 1800 | — | — | — |
| No. of Engines | 2 | 2 | 3 | 2 |
| Fuel Capacity (gal) | 641 | — | — | — |
| Flat Rating | — | ISA + 15 | ISA + 17 | ISA + 23 |
| Thrust (lbs) | — | 28000 | 6722 | 3435 |
| Dimensions | ||||
| Width (ft) | 25.77 | — | — | — |
| Length (ft) | 61.58 | 138.4 | 80.2 | 52.2 |
| Cabin Width (ft) | 7.58 | 11.6 | 7.7 | 5.6 |
| Cabin Height (ft) | 4.5 | 7.1 | 6.2 | 5.1 |
| Cabin Length (ft) | 15.5 | 107.2 | 42.7 | 23 |
| Overall Height (ft) | 18.18 | 40.3 | 26.1 | 17.4 |
| Rotor Diameter (ft) | 54.5 | — | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | 1485 | — | — |
| Wingspan (ft) | — | 117.9 | 86.3 | 55.8 |
| Aisle Step (ft) | — | Flat Floor | — | Flat Floor |
| Cabin Width - Floor (ft) | — | 10.7 | 6.3 | 3.8 |
| Cabin Length - Seating (ft) | — | 100.6 | 29.2 | 17 |
| Cabin Volume (cu. ft) | — | — | 1695 | — |
| Baggage Volume Int. (cu. ft) | — | — | 140 | 90 |