Airbus Helicopters H225 vs Bombardier Global 7500 vs Daher Tbm 960 vs Sikorsky S 92
The Airbus H225 and Sikorsky S‑92 are large twin‑engine helicopters aimed at offshore transport, search and rescue, and utility missions. They typically carry around 16–19 passengers in standard transport layouts, with higher-density configurations possible, and offer practical ranges roughly in the 450–550 nautical mile class depending on payload, reserves, and mission equipment. The H225 generally edges toward slightly higher capacity and lift, while the S‑92 is widely used for similar roles with comparable mission radius. The Bombardier Global 7500 is an ultra‑long‑range business jet designed for intercontinental travel, with a range about 7,700 nautical miles and a typical executive passenger load around 8–19 (maximum seating can be higher depending on configuration). It trades vertical‑lift flexibility for speed, altitude, and vastly greater range. The Daher TBM 960 is a high‑performance single‑engine turboprop in the personal/business aircraft category, seating up to about six passengers, with a range roughly around 1,400 nautical miles, positioned between helicopters and large jets in both capacity and reach.
| Spec | AIRBUS H225 | Bombardier Global 7500 | Daher TBM 960 | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 9.50 | $ 2.25 | $ 19.79 |
| Min Crew | 2 | 2 | 1 | 2 |
| Total Seats | 21 | 14 | 6 | 21 |
| Flight Rules | IFR | — | IFR | IFR |
| Manufacturer | Airbus Helicopters | Bombardier | Daher TBM | Sikorsky |
| Aircraft Name | H225 | Global 7500 | TBM 960 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 7700 | 1730 | 439 |
| DOC / nm / Seat | $ 0.99 | $ 0.79 | $ 0.56 | $ 0.94 |
| Max Cabin Seats | 28 | 19 | — | 19 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | — | 2908 | 7417 |
| Standard Cabin Seats | 19 | 12 | 4 | 19 |
| Direct Operating Cost | $ 2,963 | $ 4,900 | $ 744 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Bombardier Vision (Pro Line Fusion) | Garmin G3000 | EFIS |
| Max Cruise Speed (ktas) | 142 | 516 | 330 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $75,000,000 | $4,450,000 | $30,650,000 |
| Aircraft Type | — | Business Jet | Turbo Prop | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 2 |
| Total Seats | 21 | 14 | 6 | 21 |
| Max Cabin Seats | 28 | 19 | — | 19 |
| Standard Cabin Seats | 19 | 12 | 4 | 19 |
| Lavatory | — | 2 Enclosed Flushing | No | — |
| Crew Rest | — | Yes | — | — |
| Jump Seat | — | Yes | — | — |
| Galley Location | — | FWD | MID | — |
| Lavatory Location | — | FWD / AFT | — | — |
| Galley / Refreshment | — | Galley | — | — |
| Max Cabin Altitude (ft) | — | 4500 | — | — |
| Cabin Pressure (psi) | — | — | 6.2 | — |
| SL Cabin Altitude (ft) | — | — | 14390 | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | Passport | 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) | — | 18920 | — | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 111 | 35.3 | — |
| Overall Height (ft) | 16.3 | 27 | — | 17.8 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | 123 | 775 |
| Wingspan (ft) | — | 104 | 42.1 | — |
| Cabin Width (ft) | — | 8 | 4 | — |
| Cabin Height (ft) | — | 6.2 | 4.1 | — |
| Cabin Length (ft) | — | 54.5 | 13.4 | — |
| Baggage Volume Ext. (cu. ft) | — | — | — | 140 |