Airbus Helicopters H225 vs Bombardier Global 7500 vs Daher Tbm 960 vs Pilatus Pc 24
The Airbus H225 is a heavy twin‑engine helicopter (rotary‑wing) optimized for offshore, SAR, and utility missions. Its range is roughly 450–650 nautical miles depending on configuration and reserves, and it typically carries about 16–19 passengers in a transport layout (higher-density seating is possible with mission tradeoffs). The Bombardier Global 7500 is an ultra‑long‑range business jet designed for intercontinental nonstop travel. It offers about 7,700 nautical miles of range and usually seats 14–19 passengers in a multi‑zone executive cabin (certified maximum can be higher depending on layout). The Daher TBM 960 is a single‑engine turboprop, best suited to fast, efficient owner‑operation and short business trips. Its typical range is about 1,400–1,700 nautical miles, and it generally seats 4–6 passengers plus a pilot, depending on interior and payload. The Pilatus PC‑24 is a twin‑engine light jet with strong short/rough‑field capability. It has around 2,000 nautical miles of range and typically carries 6–10 passengers, with flexibility for mixed passenger/cargo missions.
| Spec | AIRBUS H225 | Bombardier Global 7500 | Daher TBM 960 | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 9.50 | $ 2.25 | $ 3.71 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 14 | 6 | 6 |
| Flight Rules | IFR | — | IFR | — |
| Manufacturer | Airbus Helicopters | Bombardier | Daher TBM | Pilatus |
| Aircraft Name | H225 | Global 7500 | TBM 960 | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 7700 | 1730 | 2076 |
| DOC / nm / Seat | $ 0.99 | $ 0.79 | $ 0.56 | $ 0.62 |
| Max Cabin Seats | 28 | 19 | — | 10 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | — | 2908 | 6680 |
| Standard Cabin Seats | 19 | 12 | 4 | 6 |
| Direct Operating Cost | $ 2,963 | $ 4,900 | $ 744 | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Bombardier Vision (Pro Line Fusion) | Garmin G3000 | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 516 | 330 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $75,000,000 | $4,450,000 | $11,800,000 |
| Aircraft Type | — | Business Jet | Turbo Prop | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 14 | 6 | 6 |
| Max Cabin Seats | 28 | 19 | — | 10 |
| Standard Cabin Seats | 19 | 12 | 4 | 6 |
| Lavatory | — | 2 Enclosed Flushing | No | 1 Enclosed Flushing |
| Crew Rest | — | Yes | — | No |
| Jump Seat | — | Yes | — | No |
| Galley Location | — | FWD | MID | FWD |
| Lavatory Location | — | FWD / AFT | — | FWD |
| Galley / Refreshment | — | Galley | — | Optional Refreshment Center |
| Max Cabin Altitude (ft) | — | 4500 | — | — |
| Cabin Pressure (psi) | — | — | 6.2 | 9.3 |
| SL Cabin Altitude (ft) | — | — | 14390 | 23500 |
| Cargo Door | — | — | — | Yes |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | Passport | TBM 960 | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | On-Condition | 3500 | 5000 |
| Horsepower | 2100 | — | 850 | — |
| No. of Engines | 2 | 2 | — | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 15 | ISA + 49 | ISA + 23 |
| Thrust (lbs) | — | 18920 | — | 3435 |
| Dimensions | ||||
| Length (ft) | 63.4 | 111 | 35.3 | 52.2 |
| Overall Height (ft) | 16.3 | 27 | — | 17.4 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | 123 | — |
| Wingspan (ft) | — | 104 | 42.1 | 55.8 |
| Cabin Width (ft) | — | 8 | 4 | 5.6 |
| Cabin Height (ft) | — | 6.2 | 4.1 | 5.1 |
| Cabin Length (ft) | — | 54.5 | 13.4 | 23 |
| Aisle Step (ft) | — | — | — | Flat Floor |
| Cabin Width - Floor (ft) | — | — | — | 3.8 |
| Cabin Length - Seating (ft) | — | — | — | 17 |
| Baggage Volume Int. (cu. ft) | — | — | — | 90 |