Airbus Helicopters H225 vs Beechcraft King Air 360 Er vs Cessna Citation Xls vs Piper M600 Sls
The Airbus H225 is a heavy twin‑engine helicopter, optimized for vertical lift missions rather than point‑to‑point speed, typically carrying about 16–19 passengers in a transport layout and offering roughly 450–500 nautical miles of range depending on configuration and reserves. The Beechcraft King Air 360ER is a twin‑turboprop business aircraft aimed at efficient regional travel, generally seating 8–11 passengers and delivering long legs of about 1,800–2,000 nautical miles. The Cessna Citation XLS+ is a super‑midsize business jet focused on faster city‑pair capability, usually accommodating 8–9 passengers with a range around 2,100 nautical miles. The Piper M600 SLS is a single‑engine turboprop, positioned for owner‑pilot and light business use, typically seating up to 5–6 passengers (including pilot) with a range near 1,400–1,500 nautical miles. Overall, the H225 leads on passenger lift in a helicopter role, the King Air 360ER and XLS+ lead on range with the XLS+ providing the highest cruise speed, and the M600 SLS emphasizes simplicity and lower operating scale.
| 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 |