Airbus Helicopters H225 vs Daher Tbm 960 vs Dassault Falcon 8x vs Piaggio Avanti Evo
The Airbus H225 is a twin‑engine heavy helicopter, best suited to offshore or utility missions where vertical lift matters more than speed. Its typical range is roughly 450–700 nm depending on load and reserves, and it generally carries about 16–19 passengers in high‑density seating (fewer in VIP layouts). The Daher TBM 960 is a single‑engine turboprop business aircraft optimized for fast, efficient point‑to‑point travel; it typically offers about 1,500–1,700 nm of range and seats 4–6 passengers in executive comfort (up to about 8 including auxiliary seating, depending on configuration). The Dassault Falcon 8X is a long‑range, three‑engine business jet designed for intercontinental missions, with about 6,400–6,450 nm of range and a typical cabin seating of 12–16 (up to around 19 depending on layout). The Piaggio Avanti EVO is a twin‑turboprop business aircraft known for high cruise efficiency and speed for its class; it typically reaches about 1,400–1,800 nm and carries about 6–8 passengers.
| Spec | AIRBUS H225 | Daher TBM 960 | Dassault Falcon 8X | Piaggio Avanti EVO |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 2.25 | $ 7.66 | — |
| Min Crew | 2 | 1 | 2 | 1 |
| Total Seats | 21 | 6 | 17 | 8 |
| Flight Rules | IFR | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Daher TBM | Dassault Falcon | Piaggio |
| Aircraft Name | H225 | TBM 960 | 8X | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1730 | 6450 | 1530 |
| DOC / nm / Seat | $ 0.99 | $ 0.56 | $ 0.64 | — |
| Max Cabin Seats | 28 | — | 16 | 7 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 2908 | 36900 | 3775 |
| Standard Cabin Seats | 19 | 4 | 14 | 6 |
| Direct Operating Cost | $ 2,963 | $ 744 | $ 3,805 | — |
| Flight Deck (Base Spec) | EFIS | Garmin G3000 | Honeywell Primus EASy II | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 142 | 330 | 516 | 400 |
| Base Aircraft Price (USD) | $ 29,500,000 | $4,450,000 | $ 62,500,000 | $ 7,695,000 |
| Aircraft Type | — | Turbo Prop | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| Min Crew | 2 | 1 | 2 | 1 |
| Total Seats | 21 | 6 | 17 | 8 |
| Max Cabin Seats | 28 | — | 16 | 7 |
| Standard Cabin Seats | 19 | 4 | 14 | 6 |
| Lavatory | — | No | 2 Enclosed Flushing | No |
| Galley Location | — | MID | FWD | — |
| Cabin Pressure (psi) | — | 6.2 | 10.2 | 9 |
| SL Cabin Altitude (ft) | — | 14390 | 29200 | 24000 |
| Crew Rest | — | — | No | — |
| Jump Seat | — | — | Yes | — |
| Lavatory Location | — | — | FWD / AFT | — |
| Galley / Refreshment | — | — | Galley | No |
| Max Cabin Altitude (ft) | — | — | 3900 | 6600 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | TBM 960 | PW307D | PT6A–66B |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | 3500 | On-Condition | 3600 |
| Horsepower | 2100 | 850 | — | 850 |
| No. of Engines | 2 | — | 3 | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 49 | ISA + 17 | ISA + 28 |
| Thrust (lbs) | — | — | 6722 | — |
| Fuel Burn (gph) | — | — | — | 100 |
| Dimensions | ||||
| Length (ft) | 63.4 | 35.3 | 80.2 | 47.3 |
| Overall Height (ft) | 16.3 | — | 26.1 | 13.1 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | 123 | 1695 | — |
| Wingspan (ft) | — | 42.1 | 86.3 | 47.1 |
| Cabin Width (ft) | — | 4 | 7.7 | 6.1 |
| Cabin Height (ft) | — | 4.1 | 6.2 | 5.8 |
| Cabin Length (ft) | — | 13.4 | 42.7 | 14.9 |
| Cabin Width - Floor (ft) | — | — | 6.3 | 3.5 |
| Cabin Length - Seating (ft) | — | — | 29.2 | — |
| Baggage Volume Int. (cu. ft) | — | — | 140 | 35.2 |