Airbus Helicopters H225 vs Cessna Citation Xls vs Pilatus Pc 24 vs Piper M600 Sls
The Airbus H225 is a heavy twin‑engine helicopter, suited to offshore and utility missions rather than point‑to‑point jet travel. Its range is roughly 500–600 nautical miles depending on load and reserves, and it typically carries about 16–19 passengers in an airline-style cabin (higher in dense seating, less in VIP layouts). The Cessna Citation XLS+ is a midsize business jet optimized for short-to-medium trips, offering about 1,800–2,100 nautical miles of range and usually seating 8–9 passengers in typical corporate configurations. The Pilatus PC‑24 is a light jet known for versatility and the ability to operate from shorter or semi-prepared runways; it commonly seats 6–10 passengers and offers around 2,000 nautical miles of range. The Piper M600 SLS is a single‑engine turboprop, slower but efficient for regional flying, with about 1,200–1,500 nautical miles of range and typically 4–6 passengers plus a pilot. Overall, the jets prioritize speed and altitude, the H225 prioritizes vertical access, and the M600 prioritizes economy and simplicity.
| Spec | AIRBUS H225 | Cessna Citation XLS+ | Pilatus PC-24 | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 5.34 | $ 3.71 | $ 2.19 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 10 | 6 | 6 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Airbus Helicopters | Cessna Citation | Pilatus | Piper |
| Aircraft Name | H225 | XLS+ | PC-24 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1906 | 2076 | 1406 |
| DOC / nm / Seat | $ 0.99 | $ 0.67 | $ 0.62 | $ 0.55 |
| Max Cabin Seats | 28 | 9 | 10 | — |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 7540 | 6680 | 2200 |
| Standard Cabin Seats | 19 | 8 | 6 | 4 |
| Direct Operating Cost | $ 2,963 | $ 2,303 | $ 1,619 | $ 603 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 430 | 440 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,500,000 | $11,800,000 | $3,081,400 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 10 | 6 | 5 |
| Max Cabin Seats | 28 | 9 | 10 | — |
| Standard Cabin Seats | 19 | 8 | 6 | 4 |
| Lavatory | — | 1 Enclosed Belted Flushing | 1 Enclosed Flushing | No |
| Crew Rest | — | No | No | — |
| Jump Seat | — | No | No | — |
| Galley Location | — | FWD | FWD | MID |
| Lavatory Location | — | AFT | FWD | — |
| Cabin Pressure (psi) | — | 9.3 | 9.3 | 5.6 |
| Galley / Refreshment | — | Galley | Optional Refreshment Center | Refreshment Centre |
| SL Cabin Altitude (ft) | — | 25230 | 23500 | 12600 |
| Cargo Door | — | — | Yes | — |
| Max Cabin Altitude (ft) | — | — | — | 8644 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | Makila 2A1 | PW545C | FJ44-4A-QPM | PT6A-42A |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | 5000 | 5000 | 3600 |
| Horsepower | 2100 | — | — | 600 |
| No. of Engines | 2 | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | — | 260 |
| Flat Rating | — | ISA + 10 | ISA + 23 | ISA + 55 |
| Thrust (lbs) | — | 4119 | 3435 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 52.5 | 52.2 | 29.7 |
| Overall Height (ft) | 16.3 | 17.2 | 17.4 | 11.3 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | 165 |
| Wingspan (ft) | — | 56.3 | 55.8 | 43.2 |
| Aisle Step (ft) | — | 0.7 | Flat Floor | — |
| Cabin Width (ft) | — | 5.5 | 5.6 | 4.1 |
| Cabin Height (ft) | — | 5.7 | 5.1 | 4 |
| Cabin Length (ft) | — | 18.5 | 23 | 12.3 |
| 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 | 20 |