Airbus Helicopters H225 vs Daher Tbm 960 vs Piaggio Avanti Evo vs Piper M600 Sls
The Airbus H225 is a large twin‑engine helicopter, best suited to offshore, SAR, and utility work rather than point‑to‑point business travel. It typically carries a high passenger load (often around 16–19 depending on fit) but has the shortest range of this group, generally a few hundred nautical miles with reserves. The Daher TBM 960, Piaggio Avanti EVO, and Piper M600 SLS are pressurized single‑pilot turboprop airplanes optimized for fast cross‑country travel. The TBM 960 is a high‑performance single‑engine turboprop with long range for its class (roughly 1,000–1,700 nm depending on speed/payload), usually seating 4–6 in comfort (up to about 6). The Avanti EVO is a twin‑engine turboprop with a larger cabin and typically 6–7 passengers, offering strong range (about 1,000–1,500 nm) and cruise efficiency. The M600 SLS is a simpler, lower‑cost single‑engine option, typically 4–6 seats, with midrange capability (about 1,000–1,400 nm).
| Spec | AIRBUS H225 | Daher TBM 960 | Piaggio Avanti EVO | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 2.25 | — | $ 2.19 |
| Min Crew | 2 | 1 | 1 | 1 |
| Total Seats | 21 | 6 | 8 | 6 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Daher TBM | Piaggio | Piper |
| Aircraft Name | H225 | TBM 960 | Avanti EVO | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1730 | 1530 | 1406 |
| DOC / nm / Seat | $ 0.99 | $ 0.56 | — | $ 0.55 |
| Max Cabin Seats | 28 | — | 7 | — |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 2908 | 3775 | 2200 |
| Standard Cabin Seats | 19 | 4 | 6 | 4 |
| Direct Operating Cost | $ 2,963 | $ 744 | — | $ 603 |
| Flight Deck (Base Spec) | EFIS | Garmin G3000 | Rockwell Collins Pro Line 21 | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 330 | 400 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $4,450,000 | $ 7,695,000 | $3,081,400 |
| Aircraft Type | — | Turbo Prop | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 | 1 |
| Total Seats | 21 | 6 | 8 | 5 |
| Max Cabin Seats | 28 | — | 7 | — |
| Standard Cabin Seats | 19 | 4 | 6 | 4 |
| Lavatory | — | No | No | No |
| Galley Location | — | MID | — | MID |
| Cabin Pressure (psi) | — | 6.2 | 9 | 5.6 |
| SL Cabin Altitude (ft) | — | 14390 | 24000 | 12600 |
| Galley / Refreshment | — | — | No | Refreshment Centre |
| Max Cabin Altitude (ft) | — | — | 6600 | 8644 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | Makila 2A1 | TBM 960 | PT6A–66B | PT6A-42A |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | 3500 | 3600 | 3600 |
| Horsepower | 2100 | 850 | 850 | 600 |
| No. of Engines | 2 | — | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | — | 260 |
| Flat Rating | — | ISA + 49 | ISA + 28 | ISA + 55 |
| Fuel Burn (gph) | — | — | 100 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 35.3 | 47.3 | 29.7 |
| Overall Height (ft) | 16.3 | — | 13.1 | 11.3 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | 123 | — | 165 |
| Wingspan (ft) | — | 42.1 | 47.1 | 43.2 |
| Cabin Width (ft) | — | 4 | 6.1 | 4.1 |
| Cabin Height (ft) | — | 4.1 | 5.8 | 4 |
| Cabin Length (ft) | — | 13.4 | 14.9 | 12.3 |
| Cabin Width - Floor (ft) | — | — | 3.5 | — |
| Baggage Volume Int. (cu. ft) | — | — | 35.2 | 20 |