Airbus Helicopters H225 vs Bell 525 Relentless vs Bombardier Global 7500 vs Daher Tbm 960
The Airbus H225 and Bell 525 Relentless are large, twin‑engine helicopters aimed at offshore, SAR, and utility missions, while the Bombardier Global 7500 is an ultra‑long‑range business jet and the Daher TBM 960 is a high‑performance single‑engine turboprop. In range terms, the Global 7500 dominates with intercontinental capability of roughly 7,700 nautical miles, designed for nonstops like New York–Hong Kong. The TBM 960 is next, typically around 1,400–1,700 nautical miles depending on reserves and conditions, suited to regional-to-transcontinental trips with one stop. The Bell 525 and Airbus H225 have helicopter-class ranges generally in the several-hundred‑nautical‑mile band (often roughly 500–700 nautical miles, mission dependent), optimized for short-to-medium legs rather than long-haul. Passenger capacity also separates them: the Global 7500 commonly carries about 8–19 passengers in executive layouts; the TBM 960 typically seats 4–6 passengers plus a pilot; the Bell 525 is usually configured around 12–16 passengers; and the H225 commonly seats in the mid‑teens to around 19, with higher-density options depending on configuration.
| Spec | AIRBUS H225 | Bell 525 Relentless | Bombardier Global 7500 | Daher TBM 960 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | — | $ 9.50 | $ 2.25 |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 21 | 18 | 14 | 6 |
| Flight Rules | IFR | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Bell | Bombardier | Daher TBM |
| Aircraft Name | H225 | 525 Relentless | Global 7500 | TBM 960 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 580 | 7700 | 1730 |
| DOC / nm / Seat | $ 0.99 | — | $ 0.79 | $ 0.56 |
| Max Cabin Seats | 28 | 16 | 19 | — |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 6675 | — | 2908 |
| Standard Cabin Seats | 19 | 16 | 12 | 4 |
| Direct Operating Cost | $ 2,963 | — | $ 4,900 | $ 744 |
| Flight Deck (Base Spec) | EFIS | Garmin G5000H | Bombardier Vision (Pro Line Fusion) | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 160 | 516 | 330 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,000,000 | $75,000,000 | $4,450,000 |
| Aircraft Type | — | — | Business Jet | Turbo Prop |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 21 | 18 | 14 | 6 |
| 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 | — |
| Max Cabin Altitude (ft) | — | — | 4500 | — |
| Cabin Pressure (psi) | — | — | — | 6.2 |
| SL Cabin Altitude (ft) | — | — | — | 14390 |
| Engine | ||||
| FADEC | Yes | Dual-Channel | Yes | Yes |
| Model | Makila 2A1 | CT7-2F1 | Passport | TBM 960 |
| Fuel Type | JetFuel | JetFuel | — | — |
| TBO (hrs) | 3500 | 4000 | On-Condition | 3500 |
| Horsepower | 2100 | 1800 | — | 850 |
| No. of Engines | 2 | 2 | 2 | — |
| Fuel Capacity (gal) | 684 | 641 | — | — |
| Flat Rating | — | — | ISA + 15 | ISA + 49 |
| Thrust (lbs) | — | — | 18920 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 61.58 | 111 | 35.3 |
| Overall Height (ft) | 16.3 | 18.18 | 27 | — |
| Rotor Diameter (ft) | 53.2 | 54.5 | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | 123 |
| Width (ft) | — | 25.77 | — | — |
| Cabin Width (ft) | — | 7.58 | 8 | 4 |
| Cabin Height (ft) | — | 4.5 | 6.2 | 4.1 |
| Cabin Length (ft) | — | 15.5 | 54.5 | 13.4 |
| Baggage Volume Ext. (cu. ft) | — | 128 | — | — |
| Wingspan (ft) | — | — | 104 | 42.1 |