Bell 525 Relentless vs Daher Tbm 960 vs Gulfstream G700 vs Leonardo Aw189
The Gulfstream G700 is a long‑range, large‑cabin business jet designed for intercontinental missions. It offers by far the greatest range, typically around 7,500 nautical miles, and the highest passenger capacity of the group, commonly configured for roughly 10–19 passengers depending on interior layout. The Daher TBM 960 is a high‑performance single‑engine turboprop airplane aimed at fast, efficient owner‑pilot or small‑team travel. It has a much shorter range than the G700 but remains strong for its class at about 1,700 nautical miles, with seating generally for up to 6 passengers. The Bell 525 Relentless is a super‑medium helicopter focused on offshore, corporate, and utility roles, trading speed and range for vertical lift and access. Its range is roughly in the 500–600 nautical mile class, with typical capacity around 16–20 occupants depending on configuration. The Leonardo AW189 is a larger medium helicopter optimized for offshore transport and search‑and‑rescue, with similar mission flexibility. Its range is commonly around 450–500 nautical miles, and it typically carries about 16–19 passengers in an offshore layout.
| Spec | Bell 525 Relentless | Daher TBM 960 | Gulfstream G700 | AGUSTA / LEONARDO AW189 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| Min Crew | 2 | 1 | 4 | 1 |
| Total Seats | 18 | 6 | 16 | 21 |
| Flight Rules | IFR | IFR | — | IFR |
| Manufacturer | Bell | Daher TBM | Gulfstream | Leonardo |
| Aircraft Name | 525 Relentless | TBM 960 | G700 | AW189 |
| Certification | FAA / EASA | FAA / EASA | In Development | FAA / EASA |
| Max Range (nm) | 580 | 1730 | 7500 | 651 |
| Max Cabin Seats | 16 | — | 19 | 19 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 6675 | 2908 | — | — |
| Standard Cabin Seats | 16 | 4 | 12 | 19 |
| Flight Deck (Base Spec) | Garmin G5000H | Garmin G3000 | Gulfstream Symmetry Flight Deck | EFIS |
| Max Cruise Speed (ktas) | 160 | 330 | 516 | 155 |
| Base Aircraft Price (USD) | $15,000,000 | $4,450,000 | $78,000,000 | $2,413,000 |
| DOC / nm | — | $ 2.25 | — | $ 15.57 |
| Aircraft Type | — | Turbo Prop | — | — |
| DOC / nm / Seat | — | $ 0.56 | — | $ 0.74 |
| Direct Operating Cost | — | $ 744 | — | $ 2,413 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 4 | 1 |
| Total Seats | 18 | 6 | 16 | 21 |
| Max Cabin Seats | 16 | — | 19 | 19 |
| Standard Cabin Seats | 16 | 4 | 12 | 19 |
| Lavatory | — | No | — | — |
| Galley Location | — | MID | FWD | — |
| Cabin Pressure (psi) | — | 6.2 | — | — |
| SL Cabin Altitude (ft) | — | 14390 | — | — |
| Crew Rest | — | — | Optional | — |
| Jump Seat | — | — | Yes | — |
| Lavatory Location | — | — | FWD / AFT | — |
| Engine | ||||
| FADEC | Dual-Channel | Yes | — | Yes |
| Model | CT7-2F1 | TBM 960 | Pearl 700 | CT7-2E1 |
| Fuel Type | JetFuel | — | — | JetFuel |
| TBO (hrs) | 4000 | 3500 | On Condition | 4000 |
| Horsepower | 1800 | 850 | — | 1983 |
| No. of Engines | 2 | — | 2 | 2 |
| Fuel Capacity (gal) | 641 | — | — | — |
| Flat Rating | — | ISA + 49 | — | — |
| Thrust (lbs) | — | — | 18250 | — |
| Dimensions | ||||
| Width (ft) | 25.77 | — | — | — |
| Length (ft) | 61.58 | 35.3 | 109.9 | 57.8 |
| Cabin Width (ft) | 7.58 | 4 | 8.2 | — |
| Cabin Height (ft) | 4.5 | 4.1 | 6.25 | — |
| Cabin Length (ft) | 15.5 | 13.4 | 56.9 | — |
| Overall Height (ft) | 18.18 | — | 25.4 | 16.6 |
| Rotor Diameter (ft) | 54.5 | — | — | 48 |
| Baggage Volume Ext. (cu. ft) | 128 | — | — | 85 |
| Wingspan (ft) | — | 42.1 | 103 | — |
| Cabin Volume (cu. ft) | — | 123 | — | 395 |
| Aisle Step (ft) | — | — | Flat Floor | — |
| Baggage Volume Int. (cu. ft) | — | — | 195 | — |