Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Daher Tbm 960 vs Sikorsky S 92
The Airbus H225 and Sikorsky S-92 are heavy, twin‑engine helicopters aimed at offshore transport, SAR, and utility missions. Both typically carry around 16–19 passengers in an offshore layout (higher in dense seating), and their practical range is in the roughly 450–600 nautical mile class depending on payload, reserves, and cabin fit; the H225 is often cited with slightly longer ferry potential, while the S‑92 is widely optimized for offshore reliability and cabin volume. The Boeing BBJ MAX 9 is a long‑range, large‑cabin business jet based on the 737 MAX 9, designed for executive/VIP travel with airline‑level speed and intercity reach. In VIP configurations it commonly seats a few dozen passengers (often around 25–50), and it can fly on the order of about 3,200–3,500 nautical miles. The Daher TBM 960 is a single‑engine turboprop business aircraft for owner‑operators, typically seating about 4–6 passengers, with a range roughly around 1,400–1,700 nautical miles depending on power setting and payload.
| Spec | AIRBUS H225 | Boeing BBJ MAX 9 | Daher TBM 960 | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.74 | $ 2.25 | $ 19.79 |
| Min Crew | 2 | 4 | 1 | 2 |
| Total Seats | 21 | 12 | 6 | 21 |
| Flight Rules | IFR | — | IFR | IFR |
| Manufacturer | Airbus Helicopters | Boeing | Daher TBM | Sikorsky |
| Aircraft Name | H225 | BBJ MAX 9 | TBM 960 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6376 | 1730 | 439 |
| DOC / nm / Seat | $ 0.99 | $ 1.97 | $ 0.56 | $ 0.94 |
| Max Cabin Seats | 28 | 35 | — | 19 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | 77120 | 2908 | 7417 |
| Standard Cabin Seats | 19 | 8 | 4 | 19 |
| Direct Operating Cost | $ 2,963 | $ 7,396 | $ 744 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Honeywell | Garmin G3000 | EFIS |
| Max Cruise Speed (ktas) | 142 | 470 | 330 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $107,700,000 | $4,450,000 | $30,650,000 |
| Aircraft Type | — | — | Turbo Prop | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 1 | 2 |
| Total Seats | 21 | 10 | 6 | 21 |
| Max Cabin Seats | 28 | 35 | — | 19 |
| Standard Cabin Seats | 19 | 8 | 4 | 19 |
| Configuration | — | Green Interior | — | — |
| Cabin Pressure (psi) | — | 9 | 6.2 | — |
| SL Cabin Altitude (ft) | — | 24000 | 14390 | — |
| Lavatory | — | — | No | — |
| Galley Location | — | — | MID | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | LEAP-1B | TBM 960 | CT7-8A |
| Fuel Type | JetFuel | — | — | JetFuel |
| TBO (hrs) | 3500 | On-Condition | 3500 | 4000 |
| Horsepower | 2100 | — | 850 | 2520 |
| No. of Engines | 2 | 2 | — | 1 |
| Fuel Capacity (gal) | 684 | — | — | 760 |
| Flat Rating | — | ISA + 15 | ISA + 49 | — |
| Thrust (lbs) | — | 28000 | — | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 138.4 | 35.3 | — |
| Overall Height (ft) | 16.3 | 40.3 | — | 17.8 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | 123 | 775 |
| Wingspan (ft) | — | 117.9 | 42.1 | — |
| Aisle Step (ft) | — | Flat Floor | — | — |
| Cabin Width (ft) | — | 11.6 | 4 | — |
| Cabin Height (ft) | — | 7.1 | 4.1 | — |
| Cabin Length (ft) | — | 107.2 | 13.4 | — |
| Cabin Width - Floor (ft) | — | 10.7 | — | — |
| Cabin Length - Seating (ft) | — | 100.6 | — | — |
| Baggage Volume Ext. (cu. ft) | — | 1485 | — | 140 |