Airbus Helicopters H225 vs Cessna Citation Xls vs Enstrom 480b vs Piper M600 Sls
The Airbus H225 is a heavy twin‑engine helicopter built for offshore and utility missions. It carries roughly 16–24 passengers depending on configuration and typically offers a few hundred nautical miles of practical range, with longer legs possible under favorable conditions. The Enstrom 480B is a light single‑engine helicopter aimed at training, patrol, and personal use; it generally seats up to 5 (including the pilot) and has a shorter range, roughly a couple hundred nautical miles. The Cessna Citation XLS+ is a super‑midsize business jet optimized for fast point‑to‑point travel. It typically seats about 8–9 passengers in executive layout and has an approximate range around 2,000 nautical miles. The Piper M600 SLS is a single‑engine turboprop, positioned between piston aircraft and jets for owner‑pilots; it commonly carries 4–6 passengers plus a pilot and offers roughly 1,400–1,600 nautical miles of range. Overall, the XLS+ leads for speed and long-range travel, the M600 SLS balances range with lower operating complexity, while the H225 and 480B trade speed and range for vertical lift and access to remote landing sites.
| 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 |