Airbus Helicopters H225 vs Daher Tbm 960 vs Piaggio Avanti Evo vs Pilatus Pc 24
The Airbus H225 is a heavy twin‑engine helicopter, optimized for vertical lift missions rather than point‑to‑point speed. Its typical range is roughly 450–500 nautical miles, and it commonly carries around 16–19 passengers (higher in dense seating), making it suitable for offshore, SAR, and utility transport where runways are unavailable. The Daher TBM 960 is a single‑engine turboprop business aircraft focused on efficient personal and executive travel. It offers about 1,400–1,700 nautical miles of range depending on reserves and loading, with seating typically 4–6 passengers (up to about 6–7 including pilot configuration). The Piaggio Avanti EVO is a twin‑engine turboprop with jet‑like cruise speed and a quiet, spacious cabin for its class. Range is generally around 1,400–1,700 nautical miles, with a typical passenger load of about 6–7 (up to 8–9 including crew/optional seating). The Pilatus PC‑24 is a light business jet designed for versatility, including operation from shorter or less‑prepared runways. Range is roughly 2,000 nautical miles, and it typically carries 6–8 passengers (up to about 10 in high‑density layouts).
| Spec | AIRBUS H225 | Daher TBM 960 | Piaggio Avanti EVO | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 2.25 | — | $ 3.71 |
| Min Crew | 2 | 1 | 1 | 1 |
| Total Seats | 21 | 6 | 8 | 6 |
| Flight Rules | IFR | IFR | IFR | — |
| Manufacturer | Airbus Helicopters | Daher TBM | Piaggio | Pilatus |
| Aircraft Name | H225 | TBM 960 | Avanti EVO | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1730 | 1530 | 2076 |
| DOC / nm / Seat | $ 0.99 | $ 0.56 | — | $ 0.62 |
| Max Cabin Seats | 28 | — | 7 | 10 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 2908 | 3775 | 6680 |
| Standard Cabin Seats | 19 | 4 | 6 | 6 |
| Direct Operating Cost | $ 2,963 | $ 744 | — | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Garmin G3000 | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 330 | 400 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $4,450,000 | $ 7,695,000 | $11,800,000 |
| Aircraft Type | — | Turbo Prop | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 | 1 |
| Total Seats | 21 | 6 | 8 | 6 |
| Max Cabin Seats | 28 | — | 7 | 10 |
| Standard Cabin Seats | 19 | 4 | 6 | 6 |
| Lavatory | — | No | No | 1 Enclosed Flushing |
| Galley Location | — | MID | — | FWD |
| Cabin Pressure (psi) | — | 6.2 | 9 | 9.3 |
| SL Cabin Altitude (ft) | — | 14390 | 24000 | 23500 |
| Galley / Refreshment | — | — | No | Optional Refreshment Center |
| Max Cabin Altitude (ft) | — | — | 6600 | — |
| Crew Rest | — | — | — | No |
| Jump Seat | — | — | — | No |
| Cargo Door | — | — | — | Yes |
| Lavatory Location | — | — | — | FWD |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | TBM 960 | PT6A–66B | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | 3500 | 3600 | 5000 |
| Horsepower | 2100 | 850 | 850 | — |
| No. of Engines | 2 | — | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 49 | ISA + 28 | ISA + 23 |
| Fuel Burn (gph) | — | — | 100 | — |
| Thrust (lbs) | — | — | — | 3435 |
| Dimensions | ||||
| Length (ft) | 63.4 | 35.3 | 47.3 | 52.2 |
| Overall Height (ft) | 16.3 | — | 13.1 | 17.4 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | 123 | — | — |
| Wingspan (ft) | — | 42.1 | 47.1 | 55.8 |
| Cabin Width (ft) | — | 4 | 6.1 | 5.6 |
| Cabin Height (ft) | — | 4.1 | 5.8 | 5.1 |
| Cabin Length (ft) | — | 13.4 | 14.9 | 23 |
| Cabin Width - Floor (ft) | — | — | 3.5 | 3.8 |
| Baggage Volume Int. (cu. ft) | — | — | 35.2 | 90 |
| Aisle Step (ft) | — | — | — | Flat Floor |
| Cabin Length - Seating (ft) | — | — | — | 17 |