Airbus Helicopters H225 vs Cessna 208b Grand Caravan Ex vs Pilatus Pc 24 vs Sikorsky S 92
The Airbus H225 and Sikorsky S-92 are large, twin‑engine helicopters typically used for offshore transport, search and rescue, and utility missions. They trade speed and range for vertical lift, with typical practical ranges in the roughly 450–550 nautical mile class, depending on payload and reserves. Passenger capacity is generally high for helicopters: the H225 is commonly configured around 16–19 passengers, while the S-92 is often around 19, with layouts varying by operator and role. The Cessna 208B Grand Caravan EX is a single‑engine turboprop fixed‑wing aircraft aimed at short‑haul utility, commuter, and cargo work. It generally offers longer range than the helicopters (about 900+ nautical miles in typical conditions) and seats up to about 9 passengers in commuter configuration (or more in specialized high‑density layouts). The Pilatus PC‑24 is a twin‑engine light business jet optimized for fast regional travel and flexible runway performance. It typically ranges around 1,800–2,000 nautical miles and carries about 6–10 passengers, depending on cabin layout.
| Spec | AIRBUS H225 | Pilatus PC-24 | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 3.71 | $ 19.79 |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 21 | 6 | 21 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Pilatus | Sikorsky |
| Aircraft Name | H225 | PC-24 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 2076 | 439 |
| DOC / nm / Seat | $ 0.99 | $ 0.62 | $ 0.94 |
| Max Cabin Seats | 28 | 10 | 19 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 6680 | 7417 |
| Standard Cabin Seats | 19 | 6 | 19 |
| Direct Operating Cost | $ 2,963 | $ 1,619 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Pilatus ACE (Primus Apex) | EFIS |
| Max Cruise Speed (ktas) | 142 | 440 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $11,800,000 | $30,650,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 21 | 6 | 21 |
| Max Cabin Seats | 28 | 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 | Makila 2A1 | FJ44-4A-QPM | CT7-8A |
| Fuel Type | JetFuel | — | JetFuel |
| TBO (hrs) | 3500 | 5000 | 4000 |
| Horsepower | 2100 | — | 2520 |
| No. of Engines | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | 760 |
| Flat Rating | — | ISA + 23 | — |
| Thrust (lbs) | — | 3435 | — |
| Dimensions | |||
| Length (ft) | 63.4 | 52.2 | — |
| Overall Height (ft) | 16.3 | 17.4 | 17.8 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | 775 |
| 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 | — |
| Baggage Volume Ext. (cu. ft) | — | — | 140 |