Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Dassault Falcon 8x vs Pilatus Pc 24
The Airbus H225 is a long‑range twin‑engine helicopter suited to offshore, search‑and‑rescue, and utility transport rather than high‑speed intercity travel. It typically carries around 16–19 passengers in a transport layout and has an approximate range in the 450–600 nautical mile class depending on configuration. The Boeing BBJ MAX 9 is a large VIP airliner based on a narrow‑body jet, optimized for intercontinental executive missions with very high cabin volume. Its range is roughly about 6,000–6,500 nautical miles, and typical VIP seating is often in the 25–50 passenger range (it can be configured for more). The Dassault Falcon 8X is an ultra‑long‑range business jet aimed at nonstop global city pairs with a quieter, smaller cabin than the BBJ but strong efficiency. It offers about 6,400 nautical miles of range and usually carries 12–16 passengers in executive layouts. The Pilatus PC‑24 is a light business jet designed for versatility and short/rough field capability. Its range is roughly about 1,800–2,000 nautical miles, with typical seating around 6–10 passengers.
| Spec | AIRBUS H225 | Boeing BBJ MAX 9 | Dassault Falcon 8X | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.74 | $ 7.66 | $ 3.71 |
| Min Crew | 2 | 4 | 2 | 1 |
| Total Seats | 21 | 12 | 17 | 6 |
| Flight Rules | IFR | — | — | — |
| Manufacturer | Airbus Helicopters | Boeing | Dassault Falcon | Pilatus |
| Aircraft Name | H225 | BBJ MAX 9 | 8X | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6376 | 6450 | 2076 |
| DOC / nm / Seat | $ 0.99 | $ 1.97 | $ 0.64 | $ 0.62 |
| Max Cabin Seats | 28 | 35 | 16 | 10 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 77120 | 36900 | 6680 |
| Standard Cabin Seats | 19 | 8 | 14 | 6 |
| Direct Operating Cost | $ 2,963 | $ 7,396 | $ 3,805 | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Honeywell | Honeywell Primus EASy II | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 470 | 516 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $107,700,000 | $ 62,500,000 | $11,800,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| Min Crew | 2 | 4 | 2 | 1 |
| Total Seats | 21 | 10 | 17 | 6 |
| Max Cabin Seats | 28 | 35 | 16 | 10 |
| Standard Cabin Seats | 19 | 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 | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | LEAP-1B | PW307D | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | On-Condition | On-Condition | 5000 |
| Horsepower | 2100 | — | — | — |
| No. of Engines | 2 | 2 | 3 | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 15 | ISA + 17 | ISA + 23 |
| Thrust (lbs) | — | 28000 | 6722 | 3435 |
| Dimensions | ||||
| Length (ft) | 63.4 | 138.4 | 80.2 | 52.2 |
| Overall Height (ft) | 16.3 | 40.3 | 26.1 | 17.4 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | 1695 | — |
| Wingspan (ft) | — | 117.9 | 86.3 | 55.8 |
| Aisle Step (ft) | — | Flat Floor | — | Flat Floor |
| Cabin Width (ft) | — | 11.6 | 7.7 | 5.6 |
| Cabin Height (ft) | — | 7.1 | 6.2 | 5.1 |
| Cabin Length (ft) | — | 107.2 | 42.7 | 23 |
| Cabin Width - Floor (ft) | — | 10.7 | 6.3 | 3.8 |
| Cabin Length - Seating (ft) | — | 100.6 | 29.2 | 17 |
| Baggage Volume Ext. (cu. ft) | — | 1485 | — | — |
| Baggage Volume Int. (cu. ft) | — | — | 140 | 90 |