Airbus Helicopters H225 vs Bombardier Global 7500 vs Daher Tbm 960 vs Piper M600 Sls
The Airbus H225 is a heavy twin‑engine helicopter optimized for vertical lift missions rather than point‑to‑point speed; it typically carries roughly 16–19 passengers in an offshore/utility layout, with practical range on the order of about 400–700 nautical miles depending on payload and reserves. The Bombardier Global 7500 is an ultra‑long‑range business jet built for intercontinental travel, generally seating about 8–19 (often 10–16 in typical executive configurations) and offering roughly 7,700 nautical miles of range. The Daher TBM 960 is a high‑performance single‑engine turboprop, usually configured for about 4–6 passengers plus a pilot, and commonly quoted around 1,400–1,700 nautical miles of range depending on power settings and reserves. The Piper M600 SLS is also a single‑engine turboprop but positioned a step below the TBM in speed and reach; it typically carries about 4–5 passengers plus a pilot and offers roughly 600–1,000 nautical miles of range. Overall, the Global 7500 dominates range, the H225 dominates lift and access to unimproved/vertical sites, and the TBM 960 and M600 SLS trade jet‑like utility for lower operating costs and simpler infrastructure.
| Spec | AIRBUS H225 | Bombardier Global 7500 | Daher TBM 960 | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 9.50 | $ 2.25 | $ 2.19 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 14 | 6 | 6 |
| Flight Rules | IFR | — | IFR | IFR |
| Manufacturer | Airbus Helicopters | Bombardier | Daher TBM | Piper |
| Aircraft Name | H225 | Global 7500 | TBM 960 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 7700 | 1730 | 1406 |
| DOC / nm / Seat | $ 0.99 | $ 0.79 | $ 0.56 | $ 0.55 |
| Max Cabin Seats | 28 | 19 | — | — |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | — | 2908 | 2200 |
| Standard Cabin Seats | 19 | 12 | 4 | 4 |
| Direct Operating Cost | $ 2,963 | $ 4,900 | $ 744 | $ 603 |
| Flight Deck (Base Spec) | EFIS | Bombardier Vision (Pro Line Fusion) | Garmin G3000 | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 516 | 330 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $75,000,000 | $4,450,000 | $3,081,400 |
| Aircraft Type | — | Business Jet | Turbo Prop | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 14 | 6 | 5 |
| Max Cabin Seats | 28 | 19 | — | — |
| Standard Cabin Seats | 19 | 12 | 4 | 4 |
| Lavatory | — | 2 Enclosed Flushing | No | No |
| Crew Rest | — | Yes | — | — |
| Jump Seat | — | Yes | — | — |
| Galley Location | — | FWD | MID | MID |
| Lavatory Location | — | FWD / AFT | — | — |
| Galley / Refreshment | — | Galley | — | Refreshment Centre |
| Max Cabin Altitude (ft) | — | 4500 | — | 8644 |
| Cabin Pressure (psi) | — | — | 6.2 | 5.6 |
| SL Cabin Altitude (ft) | — | — | 14390 | 12600 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | Makila 2A1 | Passport | TBM 960 | PT6A-42A |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | On-Condition | 3500 | 3600 |
| Horsepower | 2100 | — | 850 | 600 |
| No. of Engines | 2 | 2 | — | 1 |
| Fuel Capacity (gal) | 684 | — | — | 260 |
| Flat Rating | — | ISA + 15 | ISA + 49 | ISA + 55 |
| Thrust (lbs) | — | 18920 | — | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 111 | 35.3 | 29.7 |
| Overall Height (ft) | 16.3 | 27 | — | 11.3 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | 123 | 165 |
| Wingspan (ft) | — | 104 | 42.1 | 43.2 |
| Cabin Width (ft) | — | 8 | 4 | 4.1 |
| Cabin Height (ft) | — | 6.2 | 4.1 | 4 |
| Cabin Length (ft) | — | 54.5 | 13.4 | 12.3 |
| Baggage Volume Int. (cu. ft) | — | — | — | 20 |