Airbus Helicopters H225 vs Cessna 208b Grand Caravan Ex vs Pilatus Pc 24 vs Piper M600 Sls
The Airbus H225 is a large twin‑engine helicopter suited to offshore and utility missions. It typically offers the shortest range of the group (often a few hundred nautical miles depending on payload and reserves) but can carry the most people, commonly around 19 passengers in transport layouts, with strong vertical-lift flexibility. The Cessna 208B Grand Caravan EX is a single‑engine turboprop utility airplane. It generally provides moderate range (often roughly 800–1,000+ nautical miles with reserves, mission‑dependent) and carries up to about 9 passengers, trading speed for rugged, short‑field practicality. The Pilatus PC‑24 is a twin‑engine light business jet. It delivers the longest range here (typically around 1,800–2,000 nautical miles, configuration‑dependent) and carries about 6–10 passengers in typical executive seating, emphasizing speed and jet comfort while still accessing shorter runways than many jets. The Piper M600 SLS is a single‑engine turboprop business aircraft. Its range is usually around 1,000–1,400 nautical miles depending on load, and it seats about 4–6 passengers, optimized for owner‑pilot efficiency and modern avionics.
| Spec | AIRBUS H225 | Pilatus PC-24 | Piper M600 SLS |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 3.71 | $ 2.19 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 21 | 6 | 6 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Pilatus | Piper |
| Aircraft Name | H225 | PC-24 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 2076 | 1406 |
| DOC / nm / Seat | $ 0.99 | $ 0.62 | $ 0.55 |
| Max Cabin Seats | 28 | 10 | — |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 6680 | 2200 |
| Standard Cabin Seats | 19 | 6 | 4 |
| Direct Operating Cost | $ 2,963 | $ 1,619 | $ 603 |
| Flight Deck (Base Spec) | EFIS | Pilatus ACE (Primus Apex) | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 440 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $11,800,000 | $3,081,400 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 21 | 6 | 5 |
| Max Cabin Seats | 28 | 10 | — |
| Standard Cabin Seats | 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 | No |
| Model | Makila 2A1 | FJ44-4A-QPM | PT6A-42A |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | 5000 | 3600 |
| Horsepower | 2100 | — | 600 |
| No. of Engines | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | 260 |
| Flat Rating | — | ISA + 23 | ISA + 55 |
| Thrust (lbs) | — | 3435 | — |
| Dimensions | |||
| Length (ft) | 63.4 | 52.2 | 29.7 |
| Overall Height (ft) | 16.3 | 17.4 | 11.3 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | 165 |
| 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 |