Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Embraer Legacy 650 E vs Pilatus Pc 24
The Airbus H225 is a heavy twin‑engine helicopter, best suited to vertical‑lift missions such as offshore transport and SAR rather than point‑to‑point jet travel. Its practical range is roughly 500–700 nautical miles depending on payload and reserves, and it typically carries about 16–19 passengers in an offshore-style layout, with higher densities possible in utility configurations. The Boeing BBJ MAX 9 is an airliner‑based VIP jet in the large‑cabin, ultra‑long‑range category. With auxiliary tanks it can fly roughly 6,000–7,000 nautical miles, and while the airframe can seat well over 150 in airline layout, VIP configurations commonly carry about 25–50 passengers (sometimes more) for comfort and amenities. The Embraer Legacy 650E is a long‑range super‑midsize business jet, typically around 3,900 nautical miles, usually arranged for about 13–14 passengers. The Pilatus PC‑24 is a light jet optimized for versatility and short/rough‑field access, with about 2,000 nautical miles of range and typically 6–10 passengers.
| Spec | AIRBUS H225 | Boeing BBJ MAX 9 | Pilatus PC-24 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.74 | $ 3.71 |
| Min Crew | 2 | 4 | 1 |
| Total Seats | 21 | 12 | 6 |
| Flight Rules | IFR | — | — |
| Manufacturer | Airbus Helicopters | Boeing | Pilatus |
| Aircraft Name | H225 | BBJ MAX 9 | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6376 | 2076 |
| DOC / nm / Seat | $ 0.99 | $ 1.97 | $ 0.62 |
| Max Cabin Seats | 28 | 35 | 10 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 77120 | 6680 |
| Standard Cabin Seats | 19 | 8 | 6 |
| Direct Operating Cost | $ 2,963 | $ 7,396 | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Honeywell | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 470 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $107,700,000 | $11,800,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 1 |
| Total Seats | 21 | 10 | 6 |
| Max Cabin Seats | 28 | 35 | 10 |
| Standard Cabin Seats | 19 | 8 | 6 |
| Configuration | — | Green Interior | — |
| Cabin Pressure (psi) | — | 9 | 9.3 |
| SL Cabin Altitude (ft) | — | 24000 | 23500 |
| Lavatory | — | — | 1 Enclosed Flushing |
| Crew Rest | — | — | No |
| Jump Seat | — | — | No |
| Cargo Door | — | — | Yes |
| Galley Location | — | — | FWD |
| Lavatory Location | — | — | FWD |
| Galley / Refreshment | — | — | Optional Refreshment Center |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Makila 2A1 | LEAP-1B | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | On-Condition | 5000 |
| Horsepower | 2100 | — | — |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — |
| Flat Rating | — | ISA + 15 | ISA + 23 |
| Thrust (lbs) | — | 28000 | 3435 |
| Dimensions | |||
| Length (ft) | 63.4 | 138.4 | 52.2 |
| Overall Height (ft) | 16.3 | 40.3 | 17.4 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | — |
| Wingspan (ft) | — | 117.9 | 55.8 |
| Aisle Step (ft) | — | Flat Floor | Flat Floor |
| Cabin Width (ft) | — | 11.6 | 5.6 |
| Cabin Height (ft) | — | 7.1 | 5.1 |
| Cabin Length (ft) | — | 107.2 | 23 |
| Cabin Width - Floor (ft) | — | 10.7 | 3.8 |
| Cabin Length - Seating (ft) | — | 100.6 | 17 |
| Baggage Volume Ext. (cu. ft) | — | 1485 | — |
| Baggage Volume Int. (cu. ft) | — | — | 90 |