Airbus Helicopters H225 vs Beechcraft King Air 360 Er vs Daher Tbm 960 vs Piper M600 Sls
The Airbus H225 is a large, twin‑engine helicopter designed for offshore, SAR, and utility missions. It typically carries around 19 passengers in a high‑density layout and offers roughly 450–500 nm of range depending on configuration and reserves, prioritizing vertical access over cruise efficiency. The Beechcraft King Air 360ER is a twin‑turboprop pressurized airplane aimed at long‑range utility and special missions. In passenger service it commonly seats about 6–9 (up to roughly 11 in some layouts) and can reach about 1,500 nm class range, trading speed for runway flexibility and redundancy. The Daher TBM 960 is a high‑performance single‑engine turboprop business aircraft. It usually seats 4–6 passengers (up to 6–7 including pilot seats depending on layout) with about 1,400–1,700 nm range, emphasizing fast point‑to‑point travel. The Piper M600 SLS is a single‑engine turboprop positioned below the TBM in speed and price. It typically carries 4–6 passengers with about 1,200–1,500 nm range, focusing on owner‑pilot operation and simpler missions.
| 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 |