Airbus Helicopters H225 vs Daher Tbm 960 vs Leonardo Aw189 vs Pilatus Pc 24
The Airbus H225 and Leonardo AW189 are twin‑engine helicopters suited to offshore, SAR, and utility roles, trading cruise speed for vertical lift and hover capability. The H225 is the larger category, typically carrying around 16–19 passengers in high‑density layouts, with practical mission ranges commonly in the roughly 450–700 nm class depending on payload, reserves, and fit. The AW189 is a slightly smaller super‑medium helicopter, often configured for about 12–16 passengers, with a broadly similar but usually somewhat shorter practical range, commonly around 400–650 nm depending on mission profile. The Daher TBM 960 is a high‑performance single‑engine turboprop airplane in the owner‑flown/business category, typically seating 4–6 passengers (up to 6–7 including pilot and optional configurations) and offering long IFR ranges around 1,500–1,700 nm. The Pilatus PC‑24 is a twin‑engine light jet, generally carrying 6–10 passengers, with typical ranges around 1,800–2,000 nm, optimized for faster point‑to‑point travel and short/rough‑field capability compared with most jets.
| Spec | AIRBUS H225 | Daher TBM 960 | AGUSTA / LEONARDO AW189 | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 2.25 | $ 15.57 | $ 3.71 |
| Min Crew | 2 | 1 | 1 | 1 |
| Total Seats | 21 | 6 | 21 | 6 |
| Flight Rules | IFR | IFR | IFR | — |
| Manufacturer | Airbus Helicopters | Daher TBM | Leonardo | Pilatus |
| Aircraft Name | H225 | TBM 960 | AW189 | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1730 | 651 | 2076 |
| DOC / nm / Seat | $ 0.99 | $ 0.56 | $ 0.74 | $ 0.62 |
| Max Cabin Seats | 28 | — | 19 | 10 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 2908 | — | 6680 |
| Standard Cabin Seats | 19 | 4 | 19 | 6 |
| Direct Operating Cost | $ 2,963 | $ 744 | $ 2,413 | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Garmin G3000 | EFIS | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 330 | 155 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $4,450,000 | $2,413,000 | $11,800,000 |
| Aircraft Type | — | Turbo Prop | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 | 1 |
| Total Seats | 21 | 6 | 21 | 6 |
| Max Cabin Seats | 28 | — | 19 | 10 |
| Standard Cabin Seats | 19 | 4 | 19 | 6 |
| Lavatory | — | No | — | 1 Enclosed Flushing |
| Galley Location | — | MID | — | FWD |
| Cabin Pressure (psi) | — | 6.2 | — | 9.3 |
| SL Cabin Altitude (ft) | — | 14390 | — | 23500 |
| Crew Rest | — | — | — | No |
| Jump Seat | — | — | — | No |
| Cargo Door | — | — | — | Yes |
| Lavatory Location | — | — | — | FWD |
| Galley / Refreshment | — | — | — | Optional Refreshment Center |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | TBM 960 | CT7-2E1 | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | JetFuel | — |
| TBO (hrs) | 3500 | 3500 | 4000 | 5000 |
| Horsepower | 2100 | 850 | 1983 | — |
| No. of Engines | 2 | — | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 49 | — | ISA + 23 |
| Thrust (lbs) | — | — | — | 3435 |
| Dimensions | ||||
| Length (ft) | 63.4 | 35.3 | 57.8 | 52.2 |
| Overall Height (ft) | 16.3 | — | 16.6 | 17.4 |
| Rotor Diameter (ft) | 53.2 | — | 48 | — |
| Cabin Volume (cu. ft) | 547 | 123 | 395 | — |
| Wingspan (ft) | — | 42.1 | — | 55.8 |
| Cabin Width (ft) | — | 4 | — | 5.6 |
| Cabin Height (ft) | — | 4.1 | — | 5.1 |
| Cabin Length (ft) | — | 13.4 | — | 23 |
| Baggage Volume Ext. (cu. ft) | — | — | 85 | — |
| Aisle Step (ft) | — | — | — | Flat Floor |
| Cabin Width - Floor (ft) | — | — | — | 3.8 |
| Cabin Length - Seating (ft) | — | — | — | 17 |
| Baggage Volume Int. (cu. ft) | — | — | — | 90 |