Leonardo Aw189 vs Pilatus Pc 24 vs Sikorsky S 92
The Agusta/Leonardo AW189 is a medium twin‑engine helicopter typically used for offshore transport, SAR, and utility missions. It generally offers a practical range on the order of about 450–500 nautical miles (with reserves depending on fit) and is commonly configured for roughly 12–16 passengers in a transport cabin, trading speed and altitude for vertical access and hover capability. The Pilatus PC‑24 is a twin‑engine light business jet aimed at regional corporate and special-mission flying. It cruises much faster than either helicopter and typically reaches around 2,000 nautical miles of range, usually seating about 6–10 passengers in an executive layout (more in high‑density or medevac configurations), but it requires runways rather than helipads. The Sikorsky S‑92 is a larger, heavy twin‑engine helicopter optimized for offshore and high-utilization roles. It typically carries more people than the AW189, often around 16–19 passengers, with a broadly similar ballpark range (roughly 500+ nautical miles depending on configuration), emphasizing payload and cabin volume over the AW189 while remaining slower than the PC‑24.
| Spec | AGUSTA / LEONARDO AW189 | Pilatus PC-24 | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 15.57 | $ 3.71 | $ 19.79 |
| Min Crew | 1 | 1 | 2 |
| Total Seats | 21 | 6 | 21 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Leonardo | Pilatus | Sikorsky |
| Aircraft Name | AW189 | PC-24 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 651 | 2076 | 439 |
| DOC / nm / Seat | $ 0.74 | $ 0.62 | $ 0.94 |
| Max Cabin Seats | 19 | 10 | 19 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified |
| Standard Cabin Seats | 19 | 6 | 19 |
| Direct Operating Cost | $ 2,413 | $ 1,619 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Pilatus ACE (Primus Apex) | EFIS |
| Max Cruise Speed (ktas) | 155 | 440 | 155 |
| Base Aircraft Price (USD) | $2,413,000 | $11,800,000 | $30,650,000 |
| Useful Load (lbs) | — | 6680 | 7417 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 2 |
| Total Seats | 21 | 6 | 21 |
| Max Cabin Seats | 19 | 10 | 19 |
| Standard Cabin Seats | 19 | 6 | 19 |
| Lavatory | — | 1 Enclosed Flushing | — |
| Crew Rest | — | No | — |
| Jump Seat | — | No | — |
| Cargo Door | — | Yes | — |
| Galley Location | — | FWD | — |
| Lavatory Location | — | FWD | — |
| Cabin Pressure (psi) | — | 9.3 | — |
| Galley / Refreshment | — | Optional Refreshment Center | — |
| SL Cabin Altitude (ft) | — | 23500 | — |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | CT7-2E1 | FJ44-4A-QPM | CT7-8A |
| Fuel Type | JetFuel | — | JetFuel |
| TBO (hrs) | 4000 | 5000 | 4000 |
| Horsepower | 1983 | — | 2520 |
| No. of Engines | 2 | 2 | 1 |
| Flat Rating | — | ISA + 23 | — |
| Thrust (lbs) | — | 3435 | — |
| Fuel Capacity (gal) | — | — | 760 |
| Dimensions | |||
| Length (ft) | 57.8 | 52.2 | — |
| Overall Height (ft) | 16.6 | 17.4 | 17.8 |
| Rotor Diameter (ft) | 48 | — | — |
| Cabin Volume (cu. ft) | 395 | — | 775 |
| Baggage Volume Ext. (cu. ft) | 85 | — | 140 |
| Wingspan (ft) | — | 55.8 | — |
| Aisle Step (ft) | — | Flat Floor | — |
| Cabin Width (ft) | — | 5.6 | — |
| Cabin Height (ft) | — | 5.1 | — |
| Cabin Length (ft) | — | 23 | — |
| Cabin Width - Floor (ft) | — | 3.8 | — |
| Cabin Length - Seating (ft) | — | 17 | — |
| Baggage Volume Int. (cu. ft) | — | 90 | — |