Airbus Helicopters H225 vs Bell 525 Relentless vs Bombardier Global 7500 vs Piper M600 Sls
The Airbus H225 and Bell 525 Relentless are large, twin‑engine helicopters suited to offshore transport, SAR, and high‑utilization utility missions. The H225 typically offers longer real‑world endurance and a higher maximum seating density, commonly carrying around 16–19 passengers, with range roughly in the 450–500+ nautical mile class depending on fit and reserves. The Bell 525 is a newer‑generation super‑medium with modern avionics and fly‑by‑wire, generally configured around 12–16 passengers, with range commonly quoted around the mid‑500 nautical mile class. The Bombardier Global 7500 is an ultra‑long‑range business jet in a different category entirely, optimized for intercontinental travel at high speed and altitude. It can fly about 7,700 nautical miles and typically carries 8–19 passengers depending on cabin layout. The Piper M600 SLS is a single‑engine turboprop personal/light business aircraft, aimed at owner‑pilots. It typically seats 4–6 passengers and offers roughly 1,200–1,600 nautical miles of range depending on power settings and payload.
| Spec | AIRBUS H225 | Bell 525 Relentless | Bombardier Global 7500 | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | — | $ 9.50 | $ 2.19 |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 21 | 18 | 14 | 6 |
| Flight Rules | IFR | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Bell | Bombardier | Piper |
| Aircraft Name | H225 | 525 Relentless | Global 7500 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 580 | 7700 | 1406 |
| DOC / nm / Seat | $ 0.99 | — | $ 0.79 | $ 0.55 |
| Max Cabin Seats | 28 | 16 | 19 | — |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 6675 | — | 2200 |
| Standard Cabin Seats | 19 | 16 | 12 | 4 |
| Direct Operating Cost | $ 2,963 | — | $ 4,900 | $ 603 |
| Flight Deck (Base Spec) | EFIS | Garmin G5000H | Bombardier Vision (Pro Line Fusion) | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 160 | 516 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,000,000 | $75,000,000 | $3,081,400 |
| Aircraft Type | — | — | Business Jet | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 21 | 18 | 14 | 5 |
| Max Cabin Seats | 28 | 16 | 19 | — |
| Standard Cabin Seats | 19 | 16 | 12 | 4 |
| Lavatory | — | — | 2 Enclosed Flushing | No |
| Crew Rest | — | — | Yes | — |
| Jump Seat | — | — | Yes | — |
| Galley Location | — | — | FWD | MID |
| Lavatory Location | — | — | FWD / AFT | — |
| Galley / Refreshment | — | — | Galley | Refreshment Centre |
| Max Cabin Altitude (ft) | — | — | 4500 | 8644 |
| Cabin Pressure (psi) | — | — | — | 5.6 |
| SL Cabin Altitude (ft) | — | — | — | 12600 |
| Engine | ||||
| FADEC | Yes | Dual-Channel | Yes | No |
| Model | Makila 2A1 | CT7-2F1 | Passport | PT6A-42A |
| Fuel Type | JetFuel | JetFuel | — | — |
| TBO (hrs) | 3500 | 4000 | On-Condition | 3600 |
| Horsepower | 2100 | 1800 | — | 600 |
| No. of Engines | 2 | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | 641 | — | 260 |
| Flat Rating | — | — | ISA + 15 | ISA + 55 |
| Thrust (lbs) | — | — | 18920 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 61.58 | 111 | 29.7 |
| Overall Height (ft) | 16.3 | 18.18 | 27 | 11.3 |
| Rotor Diameter (ft) | 53.2 | 54.5 | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | 165 |
| Width (ft) | — | 25.77 | — | — |
| Cabin Width (ft) | — | 7.58 | 8 | 4.1 |
| Cabin Height (ft) | — | 4.5 | 6.2 | 4 |
| Cabin Length (ft) | — | 15.5 | 54.5 | 12.3 |
| Baggage Volume Ext. (cu. ft) | — | 128 | — | — |
| Wingspan (ft) | — | — | 104 | 43.2 |
| Baggage Volume Int. (cu. ft) | — | — | — | 20 |