Airbus Helicopters H225 vs Leonardo Aw189 vs Pilatus Pc 24 vs Piper M600 Sls
The Airbus H225 and Leonardo AW189 are large, twin‑engine helicopters designed for offshore, SAR, and utility missions, trading speed for vertical access and hover capability. The H225 is the heavier category with generally longer endurance and higher payload potential; typical mission ranges are on the order of roughly 450–800+ km depending on reserves and configuration, and seating commonly runs about 16–19 passengers. The AW189 is a slightly smaller super‑medium, typically offering around 8–16 seats and broadly comparable mission ranges in the mid‑hundreds of kilometers, often somewhat less than an H225 when similarly equipped. The Pilatus PC‑24 is a twin‑engine light jet focused on fast point‑to‑point travel from shorter or less‑prepared runways. It generally offers about 6–10 passengers with ranges roughly around 3,000–3,700 km, depending on payload and reserves. The Piper M600 SLS is a single‑engine turboprop, best for efficient owner‑operator flying, typically carrying about 4–6 passengers with range around 2,000–2,800 km.
| Spec | AIRBUS H225 | AGUSTA / LEONARDO AW189 | Pilatus PC-24 | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.57 | $ 3.71 | $ 2.19 |
| Min Crew | 2 | 1 | 1 | 1 |
| Total Seats | 21 | 21 | 6 | 6 |
| Flight Rules | IFR | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Leonardo | Pilatus | Piper |
| Aircraft Name | H225 | AW189 | PC-24 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 651 | 2076 | 1406 |
| DOC / nm / Seat | $ 0.99 | $ 0.74 | $ 0.62 | $ 0.55 |
| Max Cabin Seats | 28 | 19 | 10 | — |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | — | 6680 | 2200 |
| Standard Cabin Seats | 19 | 19 | 6 | 4 |
| Direct Operating Cost | $ 2,963 | $ 2,413 | $ 1,619 | $ 603 |
| Flight Deck (Base Spec) | EFIS | EFIS | Pilatus ACE (Primus Apex) | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 155 | 440 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $2,413,000 | $11,800,000 | $3,081,400 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 | 1 |
| Total Seats | 21 | 21 | 6 | 5 |
| Max Cabin Seats | 28 | 19 | 10 | — |
| Standard Cabin Seats | 19 | 19 | 6 | 4 |
| Lavatory | — | — | 1 Enclosed Flushing | No |
| Crew Rest | — | — | No | — |
| Jump Seat | — | — | No | — |
| Cargo Door | — | — | Yes | — |
| Galley Location | — | — | FWD | MID |
| Lavatory Location | — | — | FWD | — |
| Cabin Pressure (psi) | — | — | 9.3 | 5.6 |
| Galley / Refreshment | — | — | Optional Refreshment Center | Refreshment Centre |
| SL Cabin Altitude (ft) | — | — | 23500 | 12600 |
| Max Cabin Altitude (ft) | — | — | — | 8644 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | Makila 2A1 | CT7-2E1 | FJ44-4A-QPM | PT6A-42A |
| Fuel Type | JetFuel | JetFuel | — | — |
| TBO (hrs) | 3500 | 4000 | 5000 | 3600 |
| Horsepower | 2100 | 1983 | — | 600 |
| No. of Engines | 2 | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | — | 260 |
| Flat Rating | — | — | ISA + 23 | ISA + 55 |
| Thrust (lbs) | — | — | 3435 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 57.8 | 52.2 | 29.7 |
| Overall Height (ft) | 16.3 | 16.6 | 17.4 | 11.3 |
| Rotor Diameter (ft) | 53.2 | 48 | — | — |
| Cabin Volume (cu. ft) | 547 | 395 | — | 165 |
| Baggage Volume Ext. (cu. ft) | — | 85 | — | — |
| Wingspan (ft) | — | — | 55.8 | 43.2 |
| Aisle Step (ft) | — | — | Flat Floor | — |
| Cabin Width (ft) | — | — | 5.6 | 4.1 |
| Cabin Height (ft) | — | — | 5.1 | 4 |
| Cabin Length (ft) | — | — | 23 | 12.3 |
| Cabin Width - Floor (ft) | — | — | 3.8 | — |
| Cabin Length - Seating (ft) | — | — | 17 | — |
| Baggage Volume Int. (cu. ft) | — | — | 90 | 20 |