Airbus Helicopters H225 vs Cessna Citation Xls vs Piper M600 Sls vs Robinson R66
The Airbus H225 is a heavy, twin‑engine helicopter optimized for offshore, SAR, and utility work. It carries the most people of the group, typically around 16–19 passengers (depending on layout), and offers medium-to-long helicopter range, roughly 450–600 nautical miles in many mission profiles. The Cessna Citation XLS+ is a midsize business jet focused on fast point‑to‑point travel. It typically seats about 7–9 passengers and has the longest practical range here, around 1,700–2,100 nautical miles depending on payload and conditions. The Piper M600 SLS is a single‑engine turboprop personal aircraft emphasizing owner-operator simplicity and efficiency. It usually carries 5–6 passengers and offers solid regional range, roughly 1,000–1,500 nautical miles depending on configuration. The Robinson R66 is a light, single‑engine turbine helicopter aimed at short‑range utility and private missions. It typically seats 4–5 occupants and has the shortest range of the set, commonly around 300–400 nautical miles.
| Spec | AIRBUS H225 | Cessna Citation XLS+ | Piper M600 SLS |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 5.34 | $ 2.19 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 21 | 10 | 6 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Cessna Citation | Piper |
| Aircraft Name | H225 | XLS+ | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1906 | 1406 |
| DOC / nm / Seat | $ 0.99 | $ 0.67 | $ 0.55 |
| Max Cabin Seats | 28 | 9 | — |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 7540 | 2200 |
| Standard Cabin Seats | 19 | 8 | 4 |
| Direct Operating Cost | $ 2,963 | $ 2,303 | $ 603 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 430 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,500,000 | $3,081,400 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 21 | 10 | 5 |
| Max Cabin Seats | 28 | 9 | — |
| Standard Cabin Seats | 19 | 8 | 4 |
| Lavatory | — | 1 Enclosed Belted Flushing | No |
| Crew Rest | — | No | — |
| Jump Seat | — | No | — |
| Galley Location | — | FWD | MID |
| Lavatory Location | — | AFT | — |
| Cabin Pressure (psi) | — | 9.3 | 5.6 |
| Galley / Refreshment | — | Galley | Refreshment Centre |
| SL Cabin Altitude (ft) | — | 25230 | 12600 |
| Max Cabin Altitude (ft) | — | — | 8644 |
| Engine | |||
| FADEC | Yes | Yes | No |
| Model | Makila 2A1 | PW545C | 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 + 10 | ISA + 55 |
| Thrust (lbs) | — | 4119 | — |
| Dimensions | |||
| Length (ft) | 63.4 | 52.5 | 29.7 |
| Overall Height (ft) | 16.3 | 17.2 | 11.3 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | 165 |
| Wingspan (ft) | — | 56.3 | 43.2 |
| Aisle Step (ft) | — | 0.7 | — |
| Cabin Width (ft) | — | 5.5 | 4.1 |
| Cabin Height (ft) | — | 5.7 | 4 |
| Cabin Length (ft) | — | 18.5 | 12.3 |
| Cabin Width - Floor (ft) | — | 3.9 | — |
| Cabin Length - Seating (ft) | — | 14.3 | — |
| Baggage Volume Ext. (cu. ft) | — | 80 | — |
| Baggage Volume Int. (cu. ft) | — | 10 | 20 |