Airbus Helicopters H225 vs Bell 525 Relentless vs Dassault Falcon 8x vs Piper M600 Sls
The Airbus H225 and Bell 525 Relentless are large, long-range helicopters designed for missions like offshore transport, SAR, and government/VIP lift. The H225 typically offers very high cabin volume and can carry roughly 19 passengers in high-density layouts, with practical ranges commonly in the 450–700 nm class depending on reserves and payload. The Bell 525 is a newer super‑medium class helicopter, generally configured for about 16 passengers, with a similar order-of-magnitude range (often cited around 500–600 nm) and a focus on cruise speed and modern avionics. The Dassault Falcon 8X is a long-range tri-jet business aircraft, in a different category entirely: it trades vertical lift for much higher speed, altitude, and intercontinental reach. Typical passenger loads are about 12–16 in executive configuration, with published range around 6,450 nm. The Piper M600 SLS is a single‑engine turboprop, optimized for owner-operators and short-to-medium trips. It seats up to six, with range roughly 1,000–1,400 nm depending on power settings and payload.
| Spec | AIRBUS H225 | Bell 525 Relentless | Dassault Falcon 8X | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | — | $ 7.66 | $ 2.19 |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 21 | 18 | 17 | 6 |
| Flight Rules | IFR | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Bell | Dassault Falcon | Piper |
| Aircraft Name | H225 | 525 Relentless | 8X | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 580 | 6450 | 1406 |
| DOC / nm / Seat | $ 0.99 | — | $ 0.64 | $ 0.55 |
| Max Cabin Seats | 28 | 16 | 16 | — |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 6675 | 36900 | 2200 |
| Standard Cabin Seats | 19 | 16 | 14 | 4 |
| Direct Operating Cost | $ 2,963 | — | $ 3,805 | $ 603 |
| Flight Deck (Base Spec) | EFIS | Garmin G5000H | Honeywell Primus EASy II | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 160 | 516 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,000,000 | $ 62,500,000 | $3,081,400 |
| Cabin | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 21 | 18 | 17 | 5 |
| Max Cabin Seats | 28 | 16 | 16 | — |
| Standard Cabin Seats | 19 | 16 | 14 | 4 |
| Lavatory | — | — | 2 Enclosed Flushing | No |
| Crew Rest | — | — | No | — |
| Jump Seat | — | — | Yes | — |
| Galley Location | — | — | FWD | MID |
| Lavatory Location | — | — | FWD / AFT | — |
| Cabin Pressure (psi) | — | — | 10.2 | 5.6 |
| Galley / Refreshment | — | — | Galley | Refreshment Centre |
| SL Cabin Altitude (ft) | — | — | 29200 | 12600 |
| Max Cabin Altitude (ft) | — | — | 3900 | 8644 |
| Engine | ||||
| FADEC | Yes | Dual-Channel | Yes | No |
| Model | Makila 2A1 | CT7-2F1 | PW307D | PT6A-42A |
| Fuel Type | JetFuel | JetFuel | — | — |
| TBO (hrs) | 3500 | 4000 | On-Condition | 3600 |
| Horsepower | 2100 | 1800 | — | 600 |
| No. of Engines | 2 | 2 | 3 | 1 |
| Fuel Capacity (gal) | 684 | 641 | — | 260 |
| Flat Rating | — | — | ISA + 17 | ISA + 55 |
| Thrust (lbs) | — | — | 6722 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 61.58 | 80.2 | 29.7 |
| Overall Height (ft) | 16.3 | 18.18 | 26.1 | 11.3 |
| Rotor Diameter (ft) | 53.2 | 54.5 | — | — |
| Cabin Volume (cu. ft) | 547 | — | 1695 | 165 |
| Width (ft) | — | 25.77 | — | — |
| Cabin Width (ft) | — | 7.58 | 7.7 | 4.1 |
| Cabin Height (ft) | — | 4.5 | 6.2 | 4 |
| Cabin Length (ft) | — | 15.5 | 42.7 | 12.3 |
| Baggage Volume Ext. (cu. ft) | — | 128 | — | — |
| Wingspan (ft) | — | — | 86.3 | 43.2 |
| Cabin Width - Floor (ft) | — | — | 6.3 | — |
| Cabin Length - Seating (ft) | — | — | 29.2 | — |
| Baggage Volume Int. (cu. ft) | — | — | 140 | 20 |