Airbus Helicopters H225 vs Daher Tbm 960 vs Dassault Falcon 8x vs Piper M600 Sls
The Airbus H225 is a large twin‑engine helicopter built for utility and offshore transport rather than point‑to‑point speed; it typically carries around 16–19 passengers in a transport layout and has a practical range on the order of roughly 400–500 nautical miles, depending heavily on payload and reserves. The Daher TBM 960 is a high‑performance single‑engine turboprop in the personal/corporate category, usually flown with 4–6 passengers plus a pilot, offering long legs for its class at about 1,400–1,700 nautical miles. The Dassault Falcon 8X is a long‑range large‑cabin business jet designed for intercontinental missions, commonly seating 8–14 passengers (with higher‑density options), and delivering roughly 6,000+ nautical miles of range. The Piper M600 SLS is a pressurized single‑engine turboprop positioned as an owner‑pilot aircraft, typically carrying 4–5 passengers plus a pilot, with range generally around 1,200–1,500 nautical miles. Overall, the H225 prioritizes vertical access and lift, the M600 and TBM emphasize efficient regional travel, and the Falcon 8X leads in speed, comfort, and global reach.
| Spec | AIRBUS H225 | Daher TBM 960 | Dassault Falcon 8X | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 2.25 | $ 7.66 | $ 2.19 |
| Min Crew | 2 | 1 | 2 | 1 |
| Total Seats | 21 | 6 | 17 | 6 |
| Flight Rules | IFR | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Daher TBM | Dassault Falcon | Piper |
| Aircraft Name | H225 | TBM 960 | 8X | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1730 | 6450 | 1406 |
| DOC / nm / Seat | $ 0.99 | $ 0.56 | $ 0.64 | $ 0.55 |
| Max Cabin Seats | 28 | — | 16 | — |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 2908 | 36900 | 2200 |
| Standard Cabin Seats | 19 | 4 | 14 | 4 |
| Direct Operating Cost | $ 2,963 | $ 744 | $ 3,805 | $ 603 |
| Flight Deck (Base Spec) | EFIS | Garmin G3000 | Honeywell Primus EASy II | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 330 | 516 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $4,450,000 | $ 62,500,000 | $3,081,400 |
| Aircraft Type | — | Turbo Prop | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| Min Crew | 2 | 1 | 2 | 1 |
| Total Seats | 21 | 6 | 17 | 5 |
| Max Cabin Seats | 28 | — | 16 | — |
| Standard Cabin Seats | 19 | 4 | 14 | 4 |
| Lavatory | — | No | 2 Enclosed Flushing | No |
| Galley Location | — | MID | FWD | MID |
| Cabin Pressure (psi) | — | 6.2 | 10.2 | 5.6 |
| SL Cabin Altitude (ft) | — | 14390 | 29200 | 12600 |
| Crew Rest | — | — | No | — |
| Jump Seat | — | — | Yes | — |
| Lavatory Location | — | — | FWD / AFT | — |
| Galley / Refreshment | — | — | Galley | Refreshment Centre |
| Max Cabin Altitude (ft) | — | — | 3900 | 8644 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | Makila 2A1 | TBM 960 | PW307D | PT6A-42A |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | 3500 | On-Condition | 3600 |
| Horsepower | 2100 | 850 | — | 600 |
| No. of Engines | 2 | — | 3 | 1 |
| Fuel Capacity (gal) | 684 | — | — | 260 |
| Flat Rating | — | ISA + 49 | ISA + 17 | ISA + 55 |
| Thrust (lbs) | — | — | 6722 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 35.3 | 80.2 | 29.7 |
| Overall Height (ft) | 16.3 | — | 26.1 | 11.3 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | 123 | 1695 | 165 |
| Wingspan (ft) | — | 42.1 | 86.3 | 43.2 |
| Cabin Width (ft) | — | 4 | 7.7 | 4.1 |
| Cabin Height (ft) | — | 4.1 | 6.2 | 4 |
| Cabin Length (ft) | — | 13.4 | 42.7 | 12.3 |
| Cabin Width - Floor (ft) | — | — | 6.3 | — |
| Cabin Length - Seating (ft) | — | — | 29.2 | — |
| Baggage Volume Int. (cu. ft) | — | — | 140 | 20 |