Airbus Helicopters H225 vs Cessna Citation Xls vs Embraer Legacy 650 E vs Piper M600 Sls
The Airbus H225 is a heavy twin‑engine helicopter, optimized for vertical lift, offshore and utility missions rather than point‑to‑point speed. It typically carries around 16–19 passengers depending on configuration, with a practical range on the order of roughly 450–550 nautical miles. The Cessna Citation XLS+ is a midsize business jet aimed at efficient regional travel. It generally seats about 7–9 passengers in a typical executive layout and offers roughly 1,900–2,100 nautical miles of range, depending on payload and conditions. The Embraer Legacy 650E is a large‑cabin long‑range business jet, suited to transcontinental and some intercontinental missions. It commonly accommodates about 13 passengers (often up to 14) and reaches roughly 3,900 nautical miles. The Piper M600 SLS is a single‑engine turboprop, positioned for owner‑pilots and short to medium business trips. It typically seats 5–6 passengers and has a range around 1,400–1,700 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 |