Airbus Helicopters H225 vs Cessna 208b Grand Caravan Ex vs Pilatus Pc 24 vs Robinson R66
The Airbus H225 is a heavy, twin‑engine helicopter suited to offshore, SAR, and utility missions. It typically carries around 16–19 passengers (higher in dense seating) and offers roughly 400–500 nautical miles of range depending on payload and reserves. The Robinson R66 is a light, single‑engine helicopter aimed at short‑range utility and private operations, usually seating 4–5 passengers with about 300–350 nautical miles of range. The Cessna 208B Grand Caravan EX is a single‑engine turboprop fixed‑wing aircraft optimized for rugged regional transport and cargo. It commonly seats 9–14 passengers and can reach about 900–1,000 nautical miles with typical loads. The Pilatus PC‑24 is a twin‑engine light business jet, positioned for fast point‑to‑point travel and short/rough‑field versatility, generally accommodating 6–10 passengers with approximately 1,800–2,000 nautical miles of range. Overall, the helicopters trade speed and range for vertical access, while the Caravan emphasizes simplicity and payload on short routes, and the PC‑24 delivers the longest range and highest cruise speed of the group.
| Spec | AIRBUS H225 | Pilatus PC-24 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 20.87 | $ 3.71 |
| Min Crew | 2 | 1 |
| Total Seats | 21 | 6 |
| Flight Rules | IFR | — |
| Manufacturer | Airbus Helicopters | Pilatus |
| Aircraft Name | H225 | PC-24 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 2076 |
| DOC / nm / Seat | $ 0.99 | $ 0.62 |
| Max Cabin Seats | 28 | 10 |
| OEM Verification | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 6680 |
| Standard Cabin Seats | 19 | 6 |
| Direct Operating Cost | $ 2,963 | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $11,800,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 1 |
| Total Seats | 21 | 6 |
| Max Cabin Seats | 28 | 10 |
| Standard Cabin Seats | 19 | 6 |
| 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 |
| Model | Makila 2A1 | FJ44-4A-QPM |
| Fuel Type | JetFuel | — |
| TBO (hrs) | 3500 | 5000 |
| Horsepower | 2100 | — |
| No. of Engines | 2 | 2 |
| Fuel Capacity (gal) | 684 | — |
| Flat Rating | — | ISA + 23 |
| Thrust (lbs) | — | 3435 |
| Dimensions | ||
| Length (ft) | 63.4 | 52.2 |
| Overall Height (ft) | 16.3 | 17.4 |
| Rotor Diameter (ft) | 53.2 | — |
| Cabin Volume (cu. ft) | 547 | — |
| 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 |