Airbus Helicopters H225 vs Daher Tbm 960 vs Embraer Legacy 650 E vs Piper M600 Sls
The Airbus H225 is a heavy twin‑engine helicopter rather than a fixed‑wing airplane, optimized for vertical lift missions such as offshore transport and SAR. Its practical range is on the order of roughly 400–500 nautical miles depending on fit and reserves, and it typically carries around 19 passengers in high‑density seating (fewer with mission equipment). The Daher TBM 960 is a single‑engine turboprop, aimed at fast owner‑pilot travel. It offers about 1,400–1,700 nautical miles of range in typical planning and usually seats 4–6 passengers plus the pilot (up to about 6 total seats in many configurations). The Embraer Legacy 650E is a large‑cabin business jet designed for long, comfortable trips. It spans roughly 3,900–4,000 nautical miles and commonly accommodates about 10–13 passengers (up to around 14 depending on layout) with a dedicated baggage hold. The Piper M600 SLS is a single‑engine turboprop positioned below the TBM in speed and cost, with roughly 1,000–1,400 nautical miles of range and typically 4–5 passengers plus the pilot (up to 6 seats).
| Spec | AIRBUS H225 | Daher TBM 960 | Piper M600 SLS |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 2.25 | $ 2.19 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 21 | 6 | 6 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Daher TBM | Piper |
| Aircraft Name | H225 | TBM 960 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1730 | 1406 |
| DOC / nm / Seat | $ 0.99 | $ 0.56 | $ 0.55 |
| Max Cabin Seats | 28 | — | — |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 2908 | 2200 |
| Standard Cabin Seats | 19 | 4 | 4 |
| Direct Operating Cost | $ 2,963 | $ 744 | $ 603 |
| Flight Deck (Base Spec) | EFIS | Garmin G3000 | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 330 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $4,450,000 | $3,081,400 |
| Aircraft Type | — | Turbo Prop | — |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 21 | 6 | 5 |
| Max Cabin Seats | 28 | — | — |
| Standard Cabin Seats | 19 | 4 | 4 |
| Lavatory | — | No | No |
| Galley Location | — | MID | MID |
| Cabin Pressure (psi) | — | 6.2 | 5.6 |
| SL Cabin Altitude (ft) | — | 14390 | 12600 |
| Galley / Refreshment | — | — | Refreshment Centre |
| Max Cabin Altitude (ft) | — | — | 8644 |
| Engine | |||
| FADEC | Yes | Yes | No |
| Model | Makila 2A1 | TBM 960 | PT6A-42A |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | 3500 | 3600 |
| Horsepower | 2100 | 850 | 600 |
| No. of Engines | 2 | — | 1 |
| Fuel Capacity (gal) | 684 | — | 260 |
| Flat Rating | — | ISA + 49 | ISA + 55 |
| Dimensions | |||
| Length (ft) | 63.4 | 35.3 | 29.7 |
| Overall Height (ft) | 16.3 | — | 11.3 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | 123 | 165 |
| Wingspan (ft) | — | 42.1 | 43.2 |
| Cabin Width (ft) | — | 4 | 4.1 |
| Cabin Height (ft) | — | 4.1 | 4 |
| Cabin Length (ft) | — | 13.4 | 12.3 |
| Baggage Volume Int. (cu. ft) | — | — | 20 |