Airbus Helicopters H225 vs Bell 525 Relentless vs Boeing Bbj Max 9 vs Daher Tbm 960
The Airbus H225 and Bell 525 Relentless are large civil helicopters aimed at offshore, SAR, and utility missions. Both typically carry around 16–20 passengers in high-density layouts, but in more common passenger-transport configurations they’re often set up closer to the low-to-mid teens. Their range is measured in the few-hundred-nautical-mile class, with the H225 generally around 450–500 nm and the 525 roughly around 500–600 nm depending on equipment and reserves. The Boeing BBJ MAX 9 is a long-range VIP airliner (business jet based on the 737 MAX 9). It operates in a different category entirely, offering intercontinental capability with auxiliary tanks—on the order of roughly 3,200–3,600 nm—while seating is typically configured for about 25–50 VIP passengers (though the airframe can seat far more in airline layout). The Daher TBM 960 is a single-engine turboprop business aircraft, optimized for fast point-to-point trips with 1–6 passengers and a range around 1,500–1,700 nm, trading cabin size for efficiency and access to shorter runways.
| Spec | AIRBUS H225 | Bell 525 Relentless | Boeing BBJ MAX 9 | Daher TBM 960 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | — | $ 15.74 | $ 2.25 |
| Min Crew | 2 | 2 | 4 | 1 |
| Total Seats | 21 | 18 | 12 | 6 |
| Flight Rules | IFR | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Bell | Boeing | Daher TBM |
| Aircraft Name | H225 | 525 Relentless | BBJ MAX 9 | TBM 960 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 580 | 6376 | 1730 |
| DOC / nm / Seat | $ 0.99 | — | $ 1.97 | $ 0.56 |
| Max Cabin Seats | 28 | 16 | 35 | — |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 6675 | 77120 | 2908 |
| Standard Cabin Seats | 19 | 16 | 8 | 4 |
| Direct Operating Cost | $ 2,963 | — | $ 7,396 | $ 744 |
| Flight Deck (Base Spec) | EFIS | Garmin G5000H | Honeywell | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 160 | 470 | 330 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,000,000 | $107,700,000 | $4,450,000 |
| Aircraft Type | — | — | — | Turbo Prop |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 4 | 1 |
| Total Seats | 21 | 18 | 10 | 6 |
| Max Cabin Seats | 28 | 16 | 35 | — |
| Standard Cabin Seats | 19 | 16 | 8 | 4 |
| Configuration | — | — | Green Interior | — |
| Cabin Pressure (psi) | — | — | 9 | 6.2 |
| SL Cabin Altitude (ft) | — | — | 24000 | 14390 |
| Lavatory | — | — | — | No |
| Galley Location | — | — | — | MID |
| Engine | ||||
| FADEC | Yes | Dual-Channel | Yes | Yes |
| Model | Makila 2A1 | CT7-2F1 | LEAP-1B | 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) | — | — | 28000 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 61.58 | 138.4 | 35.3 |
| Overall Height (ft) | 16.3 | 18.18 | 40.3 | — |
| Rotor Diameter (ft) | 53.2 | 54.5 | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | 123 |
| Width (ft) | — | 25.77 | — | — |
| Cabin Width (ft) | — | 7.58 | 11.6 | 4 |
| Cabin Height (ft) | — | 4.5 | 7.1 | 4.1 |
| Cabin Length (ft) | — | 15.5 | 107.2 | 13.4 |
| Baggage Volume Ext. (cu. ft) | — | 128 | 1485 | — |
| Wingspan (ft) | — | — | 117.9 | 42.1 |
| Aisle Step (ft) | — | — | Flat Floor | — |
| Cabin Width - Floor (ft) | — | — | 10.7 | — |
| Cabin Length - Seating (ft) | — | — | 100.6 | — |