Airbus Helicopters H225 vs Cessna 208b Grand Caravan Ex vs Cessna Citation Xls vs Pilatus Pc 24
The Airbus H225 is a heavy twin‑engine helicopter, best suited to offshore, search‑and‑rescue, and utility missions. Compared with the fixed‑wing aircraft here, it typically has shorter range (roughly 450–650 nm depending on fit) but strong vertical‑lift capability and a higher people‑moving capacity for its class, commonly around 16–19 passengers in transport layouts. The Cessna 208B Grand Caravan EX is a single‑engine turboprop utility aircraft optimized for short, rugged runways and simple operations. It carries about 9–14 passengers depending on configuration, with typical ranges around 900–1,200 nm. The Cessna Citation XLS+ is a midsize business jet focused on speed and comfort. It usually seats about 8–9 passengers in executive layout, and commonly ranges about 1,900–2,100 nm. The Pilatus PC‑24 is a light business jet designed for versatility, including operation from shorter or semi‑prepared strips. It generally carries around 6–10 passengers, with range typically about 1,800–2,000 nm.
| Spec | AIRBUS H225 | Cessna Citation XLS+ | Pilatus PC-24 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 5.34 | $ 3.71 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 21 | 10 | 6 |
| Flight Rules | IFR | — | — |
| Manufacturer | Airbus Helicopters | Cessna Citation | Pilatus |
| Aircraft Name | H225 | XLS+ | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1906 | 2076 |
| DOC / nm / Seat | $ 0.99 | $ 0.67 | $ 0.62 |
| Max Cabin Seats | 28 | 9 | 10 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 7540 | 6680 |
| Standard Cabin Seats | 19 | 8 | 6 |
| Direct Operating Cost | $ 2,963 | $ 2,303 | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 430 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,500,000 | $11,800,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 21 | 10 | 6 |
| Max Cabin Seats | 28 | 9 | 10 |
| Standard Cabin Seats | 19 | 8 | 6 |
| Lavatory | — | 1 Enclosed Belted Flushing | 1 Enclosed Flushing |
| Crew Rest | — | No | No |
| Jump Seat | — | No | No |
| Galley Location | — | FWD | FWD |
| Lavatory Location | — | AFT | FWD |
| Cabin Pressure (psi) | — | 9.3 | 9.3 |
| Galley / Refreshment | — | Galley | Optional Refreshment Center |
| SL Cabin Altitude (ft) | — | 25230 | 23500 |
| Cargo Door | — | — | Yes |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Makila 2A1 | PW545C | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | 5000 | 5000 |
| Horsepower | 2100 | — | — |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — |
| Flat Rating | — | ISA + 10 | ISA + 23 |
| Thrust (lbs) | — | 4119 | 3435 |
| Dimensions | |||
| Length (ft) | 63.4 | 52.5 | 52.2 |
| Overall Height (ft) | 16.3 | 17.2 | 17.4 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | — |
| Wingspan (ft) | — | 56.3 | 55.8 |
| Aisle Step (ft) | — | 0.7 | Flat Floor |
| Cabin Width (ft) | — | 5.5 | 5.6 |
| Cabin Height (ft) | — | 5.7 | 5.1 |
| Cabin Length (ft) | — | 18.5 | 23 |
| Cabin Width - Floor (ft) | — | 3.9 | 3.8 |
| Cabin Length - Seating (ft) | — | 14.3 | 17 |
| Baggage Volume Ext. (cu. ft) | — | 80 | — |
| Baggage Volume Int. (cu. ft) | — | 10 | 90 |