Airbus Helicopters H225 vs Bell 525 Relentless vs Piaggio Avanti Evo 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 typically carries more passengers in high‑density configurations (often around 16–19) and delivers long helicopter legs on the order of roughly 450–600 nautical miles depending on payload and reserves. The Bell 525 is a newer heavy helicopter in a similar range class, generally configured for about 12–16 passengers, with comparable medium‑to‑long helicopter range (roughly 500–600 nautical miles, mission dependent). The Piaggio Avanti EVO is a twin‑turboprop, pressurized fixed‑wing aircraft positioned as a fast business aircraft; it typically seats 6–9 passengers and offers substantially longer range than the helicopters, commonly around 1,400–1,700 nautical miles. The Piper M600 SLS is a single‑engine, pressurized turboprop in the personal/business category, usually seating 4–6 passengers, with a typical range around 1,000–1,500 nautical miles. Overall, helicopters trade speed and range for vertical lift and access, while the Avanti EVO and M600 favor efficient point‑to‑point travel.
| Spec | AIRBUS H225 | Bell 525 Relentless | Piaggio Avanti EVO | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | — | — | $ 2.19 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 18 | 8 | 6 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Bell | Piaggio | Piper |
| Aircraft Name | H225 | 525 Relentless | Avanti EVO | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 580 | 1530 | 1406 |
| DOC / nm / Seat | $ 0.99 | — | — | $ 0.55 |
| Max Cabin Seats | 28 | 16 | 7 | — |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 6675 | 3775 | 2200 |
| Standard Cabin Seats | 19 | 16 | 6 | 4 |
| Direct Operating Cost | $ 2,963 | — | — | $ 603 |
| Flight Deck (Base Spec) | EFIS | Garmin G5000H | Rockwell Collins Pro Line 21 | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 160 | 400 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,000,000 | $ 7,695,000 | $3,081,400 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 18 | 8 | 5 |
| Max Cabin Seats | 28 | 16 | 7 | — |
| Standard Cabin Seats | 19 | 16 | 6 | 4 |
| Lavatory | — | — | No | No |
| Cabin Pressure (psi) | — | — | 9 | 5.6 |
| Galley / Refreshment | — | — | No | Refreshment Centre |
| SL Cabin Altitude (ft) | — | — | 24000 | 12600 |
| Max Cabin Altitude (ft) | — | — | 6600 | 8644 |
| Galley Location | — | — | — | MID |
| Engine | ||||
| FADEC | Yes | Dual-Channel | Yes | No |
| Model | Makila 2A1 | CT7-2F1 | PT6A–66B | PT6A-42A |
| Fuel Type | JetFuel | JetFuel | — | — |
| TBO (hrs) | 3500 | 4000 | 3600 | 3600 |
| Horsepower | 2100 | 1800 | 850 | 600 |
| No. of Engines | 2 | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | 641 | — | 260 |
| Flat Rating | — | — | ISA + 28 | ISA + 55 |
| Fuel Burn (gph) | — | — | 100 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 61.58 | 47.3 | 29.7 |
| Overall Height (ft) | 16.3 | 18.18 | 13.1 | 11.3 |
| Rotor Diameter (ft) | 53.2 | 54.5 | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | 165 |
| Width (ft) | — | 25.77 | — | — |
| Cabin Width (ft) | — | 7.58 | 6.1 | 4.1 |
| Cabin Height (ft) | — | 4.5 | 5.8 | 4 |
| Cabin Length (ft) | — | 15.5 | 14.9 | 12.3 |
| Baggage Volume Ext. (cu. ft) | — | 128 | — | — |
| Wingspan (ft) | — | — | 47.1 | 43.2 |
| Cabin Width - Floor (ft) | — | — | 3.5 | — |
| Baggage Volume Int. (cu. ft) | — | — | 35.2 | 20 |