Airbus Helicopters H225 vs Bell 525 Relentless vs Leonardo Aw189 vs Piper M600 Sls
The Airbus H225, Bell 525 Relentless, and Leonardo AW189 are super‑medium, twin‑engine helicopters aimed at offshore transport, SAR, and utility work, while the Piper M600 SLS is a single‑engine turboprop fixed‑wing aircraft primarily for personal and business travel. In range, the M600 SLS typically offers the longest point‑to‑point capability (roughly 1,000+ nm, depending on reserves and conditions). The three helicopters generally fall into a similar class, commonly around the 450–550 nm range with typical passenger payloads, varying by configuration, fuel, and mission equipment. For passenger capacity, the helicopters are designed for multi‑passenger cabin layouts: the H225 is usually the largest of the three, often configured around the high‑teens to near twenty seats for offshore roles; the AW189 and Bell 525 are commonly in the mid‑teens in typical transport layouts. The Piper M600 SLS seats up to six (including the pilot), trading cabin volume for speed, efficiency, and longer range on runways rather than vertical lift.
| Spec | AIRBUS H225 | Bell 525 Relentless | AGUSTA / LEONARDO AW189 | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | — | $ 15.57 | $ 2.19 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 18 | 21 | 6 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Bell | Leonardo | Piper |
| Aircraft Name | H225 | 525 Relentless | AW189 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 580 | 651 | 1406 |
| DOC / nm / Seat | $ 0.99 | — | $ 0.74 | $ 0.55 |
| Max Cabin Seats | 28 | 16 | 19 | — |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 6675 | — | 2200 |
| Standard Cabin Seats | 19 | 16 | 19 | 4 |
| Direct Operating Cost | $ 2,963 | — | $ 2,413 | $ 603 |
| Flight Deck (Base Spec) | EFIS | Garmin G5000H | EFIS | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 160 | 155 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,000,000 | $2,413,000 | $3,081,400 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 18 | 21 | 5 |
| Max Cabin Seats | 28 | 16 | 19 | — |
| Standard Cabin Seats | 19 | 16 | 19 | 4 |
| Lavatory | — | — | — | No |
| Galley Location | — | — | — | MID |
| Cabin Pressure (psi) | — | — | — | 5.6 |
| Galley / Refreshment | — | — | — | Refreshment Centre |
| SL Cabin Altitude (ft) | — | — | — | 12600 |
| Max Cabin Altitude (ft) | — | — | — | 8644 |
| Engine | ||||
| FADEC | Yes | Dual-Channel | Yes | No |
| Model | Makila 2A1 | CT7-2F1 | CT7-2E1 | PT6A-42A |
| Fuel Type | JetFuel | JetFuel | JetFuel | — |
| TBO (hrs) | 3500 | 4000 | 4000 | 3600 |
| Horsepower | 2100 | 1800 | 1983 | 600 |
| No. of Engines | 2 | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | 641 | — | 260 |
| Flat Rating | — | — | — | ISA + 55 |
| Dimensions | ||||
| Length (ft) | 63.4 | 61.58 | 57.8 | 29.7 |
| Overall Height (ft) | 16.3 | 18.18 | 16.6 | 11.3 |
| Rotor Diameter (ft) | 53.2 | 54.5 | 48 | — |
| Cabin Volume (cu. ft) | 547 | — | 395 | 165 |
| Width (ft) | — | 25.77 | — | — |
| Cabin Width (ft) | — | 7.58 | — | 4.1 |
| Cabin Height (ft) | — | 4.5 | — | 4 |
| Cabin Length (ft) | — | 15.5 | — | 12.3 |
| Baggage Volume Ext. (cu. ft) | — | 128 | 85 | — |
| Wingspan (ft) | — | — | — | 43.2 |
| Baggage Volume Int. (cu. ft) | — | — | — | 20 |