Airbus Helicopters H225 vs Piaggio Avanti Evo vs Pilatus Pc 24 vs Piper M600 Sls
The Airbus H225 is a heavy twin‑engine helicopter designed for vertical lift missions rather than point‑to‑point airplane travel. It typically carries a large cabin load, often around 16–19 passengers depending on configuration, and offers useful range on the order of roughly 400–500 nautical miles, with the key advantage being access to helipads and confined areas. The Piaggio Avanti EVO is a high‑speed turboprop airplane optimized for efficient regional trips. It generally seats about 6–7 passengers (plus crew) and typically supports ranges around 1,400–1,800 nautical miles, trading helicopter flexibility for much higher cruise speed and runway operations. The Pilatus PC‑24 is a light business jet aimed at versatile, longer‑range travel and short/rough‑field capability for a jet. It commonly carries about 6–10 passengers and offers roughly 1,800–2,000 nautical miles of range, emphasizing speed and cabin flexibility. The Piper M600 SLS is a single‑engine turboprop for owner‑operators, typically seating about 5–6 passengers with a range around 1,400 nautical miles, prioritizing simplicity and cost efficiency over cabin size and redundancy.
| Spec | AIRBUS H225 | Piaggio Avanti EVO | Pilatus PC-24 | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | — | $ 3.71 | $ 2.19 |
| Min Crew | 2 | 1 | 1 | 1 |
| Total Seats | 21 | 8 | 6 | 6 |
| Flight Rules | IFR | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Piaggio | Pilatus | Piper |
| Aircraft Name | H225 | Avanti EVO | PC-24 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1530 | 2076 | 1406 |
| DOC / nm / Seat | $ 0.99 | — | $ 0.62 | $ 0.55 |
| Max Cabin Seats | 28 | 7 | 10 | — |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 3775 | 6680 | 2200 |
| Standard Cabin Seats | 19 | 6 | 6 | 4 |
| Direct Operating Cost | $ 2,963 | — | $ 1,619 | $ 603 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 400 | 440 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $ 7,695,000 | $11,800,000 | $3,081,400 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 | 1 |
| Total Seats | 21 | 8 | 6 | 5 |
| Max Cabin Seats | 28 | 7 | 10 | — |
| Standard Cabin Seats | 19 | 6 | 6 | 4 |
| Lavatory | — | No | 1 Enclosed Flushing | No |
| Cabin Pressure (psi) | — | 9 | 9.3 | 5.6 |
| Galley / Refreshment | — | No | Optional Refreshment Center | Refreshment Centre |
| SL Cabin Altitude (ft) | — | 24000 | 23500 | 12600 |
| Max Cabin Altitude (ft) | — | 6600 | — | 8644 |
| Crew Rest | — | — | No | — |
| Jump Seat | — | — | No | — |
| Cargo Door | — | — | Yes | — |
| Galley Location | — | — | FWD | MID |
| Lavatory Location | — | — | FWD | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | Makila 2A1 | PT6A–66B | FJ44-4A-QPM | PT6A-42A |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | 3600 | 5000 | 3600 |
| Horsepower | 2100 | 850 | — | 600 |
| No. of Engines | 2 | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | — | 260 |
| Flat Rating | — | ISA + 28 | ISA + 23 | ISA + 55 |
| Fuel Burn (gph) | — | 100 | — | — |
| Thrust (lbs) | — | — | 3435 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 47.3 | 52.2 | 29.7 |
| Overall Height (ft) | 16.3 | 13.1 | 17.4 | 11.3 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | 165 |
| Wingspan (ft) | — | 47.1 | 55.8 | 43.2 |
| Cabin Width (ft) | — | 6.1 | 5.6 | 4.1 |
| Cabin Height (ft) | — | 5.8 | 5.1 | 4 |
| Cabin Length (ft) | — | 14.9 | 23 | 12.3 |
| Cabin Width - Floor (ft) | — | 3.5 | 3.8 | — |
| Baggage Volume Int. (cu. ft) | — | 35.2 | 90 | 20 |
| Aisle Step (ft) | — | — | Flat Floor | — |
| Cabin Length - Seating (ft) | — | — | 17 | — |