Airbus Helicopters H225 vs Bombardier Global 7500 vs Leonardo Aw189 vs Piper M600 Sls
The Airbus H225 and Leonardo AW189 are twin‑engine helicopters aimed at offshore, search‑and‑rescue, and utility transport, trading speed and range for vertical lift and flexible access to remote sites. The H225 is the larger/heavier category, typically carrying around 16–19 passengers in transport layouts and offering roughly 450–500 nautical miles of range depending on mission fit and reserves. The AW189 sits a size class below, commonly configured for about 16–19 passengers as well, with a broadly similar but often slightly shorter practical range, roughly 400–500 nautical miles. The Bombardier Global 7500 is an ultra‑long‑range business jet built for intercontinental point‑to‑point travel. It typically carries 8–19 passengers depending on cabin layout, with an advertised range around 7,700 nautical miles, far exceeding rotorcraft or turboprops. The Piper M600 SLS is a single‑engine pressurized turboprop in the personal/light business category. It usually seats 1 pilot plus about 5 passengers (up to 6 total), with typical range around 1,400 nautical miles, offering much more reach than helicopters but far less than the Global 7500.
| Spec | AIRBUS H225 | Bombardier Global 7500 | AGUSTA / LEONARDO AW189 | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 9.50 | $ 15.57 | $ 2.19 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 14 | 21 | 6 |
| Flight Rules | IFR | — | IFR | IFR |
| Manufacturer | Airbus Helicopters | Bombardier | Leonardo | Piper |
| Aircraft Name | H225 | Global 7500 | AW189 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 7700 | 651 | 1406 |
| DOC / nm / Seat | $ 0.99 | $ 0.79 | $ 0.74 | $ 0.55 |
| Max Cabin Seats | 28 | 19 | 19 | — |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | — | — | 2200 |
| Standard Cabin Seats | 19 | 12 | 19 | 4 |
| Direct Operating Cost | $ 2,963 | $ 4,900 | $ 2,413 | $ 603 |
| Flight Deck (Base Spec) | EFIS | Bombardier Vision (Pro Line Fusion) | EFIS | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 516 | 155 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $75,000,000 | $2,413,000 | $3,081,400 |
| Aircraft Type | — | Business Jet | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 14 | 21 | 5 |
| Max Cabin Seats | 28 | 19 | 19 | — |
| Standard Cabin Seats | 19 | 12 | 19 | 4 |
| Lavatory | — | 2 Enclosed Flushing | — | No |
| Crew Rest | — | Yes | — | — |
| Jump Seat | — | Yes | — | — |
| Galley Location | — | FWD | — | MID |
| Lavatory Location | — | FWD / AFT | — | — |
| Galley / Refreshment | — | Galley | — | Refreshment Centre |
| Max Cabin Altitude (ft) | — | 4500 | — | 8644 |
| Cabin Pressure (psi) | — | — | — | 5.6 |
| SL Cabin Altitude (ft) | — | — | — | 12600 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | Makila 2A1 | Passport | CT7-2E1 | PT6A-42A |
| Fuel Type | JetFuel | — | JetFuel | — |
| TBO (hrs) | 3500 | On-Condition | 4000 | 3600 |
| Horsepower | 2100 | — | 1983 | 600 |
| No. of Engines | 2 | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | — | 260 |
| Flat Rating | — | ISA + 15 | — | ISA + 55 |
| Thrust (lbs) | — | 18920 | — | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 111 | 57.8 | 29.7 |
| Overall Height (ft) | 16.3 | 27 | 16.6 | 11.3 |
| Rotor Diameter (ft) | 53.2 | — | 48 | — |
| Cabin Volume (cu. ft) | 547 | — | 395 | 165 |
| Wingspan (ft) | — | 104 | — | 43.2 |
| Cabin Width (ft) | — | 8 | — | 4.1 |
| Cabin Height (ft) | — | 6.2 | — | 4 |
| Cabin Length (ft) | — | 54.5 | — | 12.3 |
| Baggage Volume Ext. (cu. ft) | — | — | 85 | — |
| Baggage Volume Int. (cu. ft) | — | — | — | 20 |