Bell 525 Relentless vs Daher Tbm 960 vs Leonardo Aw189 vs Pilatus Pc 24
The Bell 525 Relentless and Leonardo AW189 are medium helicopters, while the Daher TBM 960 is a single‑engine turboprop airplane and the Pilatus PC‑24 is a light twin‑jet. For range, the PC‑24 generally leads among these four, suited to longer point‑to‑point trips with jet speeds; the TBM 960 also offers long range for its class, typically comparable to or slightly behind the PC‑24 depending on reserves and payload. The two helicopters trade outright range for vertical lift and access: the AW189 and Bell 525 deliver shorter ranges than the fixed‑wing aircraft but can serve helipads, offshore platforms, and confined sites; between them, the Bell 525 is often positioned toward the longer‑range end of its helicopter segment. For passenger capacity, the PC‑24 typically seats around 6–10 in executive layouts, the TBM 960 commonly carries 4–6 passengers plus a pilot, while the AW189 and Bell 525 can be configured for higher cabin loads, often around 12–16 passengers depending on mission and seating density.
| Spec | Bell 525 Relentless | Daher TBM 960 | AGUSTA / LEONARDO AW189 | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 | 1 |
| Total Seats | 18 | 6 | 21 | 6 |
| Flight Rules | IFR | IFR | IFR | — |
| Manufacturer | Bell | Daher TBM | Leonardo | Pilatus |
| Aircraft Name | 525 Relentless | TBM 960 | AW189 | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 1730 | 651 | 2076 |
| Max Cabin Seats | 16 | — | 19 | 10 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 6675 | 2908 | — | 6680 |
| Standard Cabin Seats | 16 | 4 | 19 | 6 |
| Flight Deck (Base Spec) | Garmin G5000H | Garmin G3000 | EFIS | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 160 | 330 | 155 | 440 |
| Base Aircraft Price (USD) | $15,000,000 | $4,450,000 | $2,413,000 | $11,800,000 |
| DOC / nm | — | $ 2.25 | $ 15.57 | $ 3.71 |
| Aircraft Type | — | Turbo Prop | — | — |
| DOC / nm / Seat | — | $ 0.56 | $ 0.74 | $ 0.62 |
| Direct Operating Cost | — | $ 744 | $ 2,413 | $ 1,619 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 | 1 |
| Total Seats | 18 | 6 | 21 | 6 |
| Max Cabin Seats | 16 | — | 19 | 10 |
| Standard Cabin Seats | 16 | 4 | 19 | 6 |
| Lavatory | — | No | — | 1 Enclosed Flushing |
| Galley Location | — | MID | — | FWD |
| Cabin Pressure (psi) | — | 6.2 | — | 9.3 |
| SL Cabin Altitude (ft) | — | 14390 | — | 23500 |
| Crew Rest | — | — | — | No |
| Jump Seat | — | — | — | No |
| Cargo Door | — | — | — | Yes |
| Lavatory Location | — | — | — | FWD |
| Galley / Refreshment | — | — | — | Optional Refreshment Center |
| Engine | ||||
| FADEC | Dual-Channel | Yes | Yes | Yes |
| Model | CT7-2F1 | TBM 960 | CT7-2E1 | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | JetFuel | — |
| TBO (hrs) | 4000 | 3500 | 4000 | 5000 |
| Horsepower | 1800 | 850 | 1983 | — |
| No. of Engines | 2 | — | 2 | 2 |
| Fuel Capacity (gal) | 641 | — | — | — |
| Flat Rating | — | ISA + 49 | — | ISA + 23 |
| Thrust (lbs) | — | — | — | 3435 |
| Dimensions | ||||
| Width (ft) | 25.77 | — | — | — |
| Length (ft) | 61.58 | 35.3 | 57.8 | 52.2 |
| Cabin Width (ft) | 7.58 | 4 | — | 5.6 |
| Cabin Height (ft) | 4.5 | 4.1 | — | 5.1 |
| Cabin Length (ft) | 15.5 | 13.4 | — | 23 |
| Overall Height (ft) | 18.18 | — | 16.6 | 17.4 |
| Rotor Diameter (ft) | 54.5 | — | 48 | — |
| Baggage Volume Ext. (cu. ft) | 128 | — | 85 | — |
| Wingspan (ft) | — | 42.1 | — | 55.8 |
| Cabin Volume (cu. ft) | — | 123 | 395 | — |
| Aisle Step (ft) | — | — | — | Flat Floor |
| Cabin Width - Floor (ft) | — | — | — | 3.8 |
| Cabin Length - Seating (ft) | — | — | — | 17 |
| Baggage Volume Int. (cu. ft) | — | — | — | 90 |