Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Dassault Falcon 8x vs Sikorsky S 92
The Airbus H225 and Sikorsky S-92 are heavy twin‑engine helicopters suited to offshore, SAR, and utility work rather than long‑distance executive travel. Their typical range is a few hundred nautical miles (about 450–550 nm depending on payload and reserves), and capacity is generally in the high‑teens to around 20 passengers in transport layouts, though VIP fits usually carry fewer for comfort. The Boeing BBJ MAX 9 is a long‑range VIP airliner based on the 737 MAX 9, optimized for intercontinental missions. With auxiliary fuel tanks it is commonly cited around 6,000–6,500 nm range, and while the airframe can seat well over 150 in airline configuration, BBJ interiors usually carry roughly 25–50 passengers with lounges and bedrooms. The Dassault Falcon 8X is a purpose‑built ultra‑long‑range business jet. It offers about 6,450 nm range and typically seats about 8–16 passengers in a high‑end cabin, prioritizing nonstop city‑pairs and access to smaller airports over sheer cabin volume.
| Spec | AIRBUS H225 | Boeing BBJ MAX 9 | Dassault Falcon 8X | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.74 | $ 7.66 | $ 19.79 |
| Min Crew | 2 | 4 | 2 | 2 |
| Total Seats | 21 | 12 | 17 | 21 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Airbus Helicopters | Boeing | Dassault Falcon | Sikorsky |
| Aircraft Name | H225 | BBJ MAX 9 | 8X | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6376 | 6450 | 439 |
| DOC / nm / Seat | $ 0.99 | $ 1.97 | $ 0.64 | $ 0.94 |
| Max Cabin Seats | 28 | 35 | 16 | 19 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 77120 | 36900 | 7417 |
| Standard Cabin Seats | 19 | 8 | 14 | 19 |
| Direct Operating Cost | $ 2,963 | $ 7,396 | $ 3,805 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Honeywell | Honeywell Primus EASy II | EFIS |
| Max Cruise Speed (ktas) | 142 | 470 | 516 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $107,700,000 | $ 62,500,000 | $30,650,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| Min Crew | 2 | 4 | 2 | 2 |
| Total Seats | 21 | 10 | 17 | 21 |
| Max Cabin Seats | 28 | 35 | 16 | 19 |
| Standard Cabin Seats | 19 | 8 | 14 | 19 |
| Configuration | — | Green Interior | — | — |
| Cabin Pressure (psi) | — | 9 | 10.2 | — |
| SL Cabin Altitude (ft) | — | 24000 | 29200 | — |
| Lavatory | — | — | 2 Enclosed Flushing | — |
| Crew Rest | — | — | No | — |
| Jump Seat | — | — | Yes | — |
| Galley Location | — | — | FWD | — |
| Lavatory Location | — | — | FWD / AFT | — |
| Galley / Refreshment | — | — | Galley | — |
| Max Cabin Altitude (ft) | — | — | 3900 | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | LEAP-1B | PW307D | CT7-8A |
| Fuel Type | JetFuel | — | — | JetFuel |
| TBO (hrs) | 3500 | On-Condition | On-Condition | 4000 |
| Horsepower | 2100 | — | — | 2520 |
| No. of Engines | 2 | 2 | 3 | 1 |
| Fuel Capacity (gal) | 684 | — | — | 760 |
| Flat Rating | — | ISA + 15 | ISA + 17 | — |
| Thrust (lbs) | — | 28000 | 6722 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 138.4 | 80.2 | — |
| Overall Height (ft) | 16.3 | 40.3 | 26.1 | 17.8 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | 1695 | 775 |
| Wingspan (ft) | — | 117.9 | 86.3 | — |
| Aisle Step (ft) | — | Flat Floor | — | — |
| Cabin Width (ft) | — | 11.6 | 7.7 | — |
| Cabin Height (ft) | — | 7.1 | 6.2 | — |
| Cabin Length (ft) | — | 107.2 | 42.7 | — |
| Cabin Width - Floor (ft) | — | 10.7 | 6.3 | — |
| Cabin Length - Seating (ft) | — | 100.6 | 29.2 | — |
| Baggage Volume Ext. (cu. ft) | — | 1485 | — | 140 |
| Baggage Volume Int. (cu. ft) | — | — | 140 | — |