Airbus Helicopters H225 vs Bell 525 Relentless vs Pilatus Pc 24 vs Piper M600 Sls
The Airbus H225 and Bell 525 Relentless are large, twin‑engine helicopters aimed at offshore, SAR, and utility missions. The H225 is the heavier, higher‑capacity option, typically carrying roughly 16–19 passengers in transport layouts, with range commonly in the ~450–550 nm class depending on fuel and mission equipment. The Bell 525 is a slightly smaller, newer‑generation super‑medium, usually configured around 12–16 passengers, with range often cited around ~500–560 nm. The Pilatus PC‑24 is a twin‑engine light jet built for flexible operations, including short and semi‑prepared runways, and typically seats 6–10 passengers depending on interior and crew. Its range is in the ~1,900–2,000 nm class, making it a step up from helicopters for point‑to‑point travel. The Piper M600 SLS is a single‑engine turboprop for owner‑operators, generally seating about 4–6 passengers, with range around ~1,400–1,500 nm. In short, H225/525 emphasize vertical lift and access, while PC‑24 and M600 prioritize speed and longer stage lengths.
| Spec | AIRBUS H225 | Bell 525 Relentless | Pilatus PC-24 | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | — | $ 3.71 | $ 2.19 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 18 | 6 | 6 |
| Flight Rules | IFR | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Bell | Pilatus | Piper |
| Aircraft Name | H225 | 525 Relentless | PC-24 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 580 | 2076 | 1406 |
| DOC / nm / Seat | $ 0.99 | — | $ 0.62 | $ 0.55 |
| Max Cabin Seats | 28 | 16 | 10 | — |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 6675 | 6680 | 2200 |
| Standard Cabin Seats | 19 | 16 | 6 | 4 |
| Direct Operating Cost | $ 2,963 | — | $ 1,619 | $ 603 |
| Flight Deck (Base Spec) | EFIS | Garmin G5000H | Pilatus ACE (Primus Apex) | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 160 | 440 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,000,000 | $11,800,000 | $3,081,400 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 18 | 6 | 5 |
| Max Cabin Seats | 28 | 16 | 10 | — |
| Standard Cabin Seats | 19 | 16 | 6 | 4 |
| Lavatory | — | — | 1 Enclosed Flushing | No |
| Crew Rest | — | — | No | — |
| Jump Seat | — | — | No | — |
| Cargo Door | — | — | Yes | — |
| Galley Location | — | — | FWD | MID |
| Lavatory Location | — | — | FWD | — |
| Cabin Pressure (psi) | — | — | 9.3 | 5.6 |
| Galley / Refreshment | — | — | Optional Refreshment Center | Refreshment Centre |
| SL Cabin Altitude (ft) | — | — | 23500 | 12600 |
| Max Cabin Altitude (ft) | — | — | — | 8644 |
| Engine | ||||
| FADEC | Yes | Dual-Channel | Yes | No |
| Model | Makila 2A1 | CT7-2F1 | FJ44-4A-QPM | 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 + 23 | ISA + 55 |
| Thrust (lbs) | — | — | 3435 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 61.58 | 52.2 | 29.7 |
| Overall Height (ft) | 16.3 | 18.18 | 17.4 | 11.3 |
| Rotor Diameter (ft) | 53.2 | 54.5 | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | 165 |
| Width (ft) | — | 25.77 | — | — |
| Cabin Width (ft) | — | 7.58 | 5.6 | 4.1 |
| Cabin Height (ft) | — | 4.5 | 5.1 | 4 |
| Cabin Length (ft) | — | 15.5 | 23 | 12.3 |
| Baggage Volume Ext. (cu. ft) | — | 128 | — | — |
| Wingspan (ft) | — | — | 55.8 | 43.2 |
| Aisle Step (ft) | — | — | Flat Floor | — |
| Cabin Width - Floor (ft) | — | — | 3.8 | — |
| Cabin Length - Seating (ft) | — | — | 17 | — |
| Baggage Volume Int. (cu. ft) | — | — | 90 | 20 |