Airbus Helicopters H225 vs Bell 525 Relentless vs Cessna Citation Xls vs Piper M600 Sls
The Airbus H225 and Bell 525 Relentless are large, twin‑engine helicopters aimed at offshore, SAR, and VIP transport, while the Cessna Citation XLS+ and Piper M600 SLS are fixed‑wing business aircraft focused on point‑to‑point travel. In range terms, the H225 typically offers roughly 450–600 nautical miles depending on payload and reserves, whereas the Bell 525 is in a similar but often slightly longer class, commonly cited around 500–650 nautical miles. For capacity, the H225 is the biggest here, commonly configured for about 16–19 passengers (and can be higher in dense layouts), while the Bell 525 is generally in the 12–16 passenger range depending on configuration. The Citation XLS+ is a midsize business jet with a much longer range—about 2,000 nautical miles—and typically seats 8–9 passengers in standard corporate layouts. The Piper M600 SLS is a single‑engine turboprop, usually seating about 5–6 passengers, with a range around 1,400–1,500 nautical miles.
| Spec | AIRBUS H225 | Bell 525 Relentless | Cessna Citation XLS+ | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | — | $ 5.34 | $ 2.19 |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 21 | 18 | 10 | 6 |
| Flight Rules | IFR | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Bell | Cessna Citation | Piper |
| Aircraft Name | H225 | 525 Relentless | XLS+ | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 580 | 1906 | 1406 |
| DOC / nm / Seat | $ 0.99 | — | $ 0.67 | $ 0.55 |
| Max Cabin Seats | 28 | 16 | 9 | — |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 6675 | 7540 | 2200 |
| Standard Cabin Seats | 19 | 16 | 8 | 4 |
| Direct Operating Cost | $ 2,963 | — | $ 2,303 | $ 603 |
| Flight Deck (Base Spec) | EFIS | Garmin G5000H | Rockwell Collins Pro Line 21 | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 160 | 430 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,000,000 | $15,500,000 | $3,081,400 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 21 | 18 | 10 | 5 |
| Max Cabin Seats | 28 | 16 | 9 | — |
| Standard Cabin Seats | 19 | 16 | 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 | Dual-Channel | Yes | No |
| Model | Makila 2A1 | CT7-2F1 | PW545C | PT6A-42A |
| Fuel Type | JetFuel | JetFuel | — | — |
| TBO (hrs) | 3500 | 4000 | 5000 | 3600 |
| Horsepower | 2100 | 1800 | — | 600 |
| No. of Engines | 2 | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | 641 | — | 260 |
| Flat Rating | — | — | ISA + 10 | ISA + 55 |
| Thrust (lbs) | — | — | 4119 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 61.58 | 52.5 | 29.7 |
| Overall Height (ft) | 16.3 | 18.18 | 17.2 | 11.3 |
| Rotor Diameter (ft) | 53.2 | 54.5 | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | 165 |
| Width (ft) | — | 25.77 | — | — |
| Cabin Width (ft) | — | 7.58 | 5.5 | 4.1 |
| Cabin Height (ft) | — | 4.5 | 5.7 | 4 |
| Cabin Length (ft) | — | 15.5 | 18.5 | 12.3 |
| Baggage Volume Ext. (cu. ft) | — | 128 | 80 | — |
| Wingspan (ft) | — | — | 56.3 | 43.2 |
| Aisle Step (ft) | — | — | 0.7 | — |
| Cabin Width - Floor (ft) | — | — | 3.9 | — |
| Cabin Length - Seating (ft) | — | — | 14.3 | — |
| Baggage Volume Int. (cu. ft) | — | — | 10 | 20 |