Bell 525 Relentless vs Daher Tbm 960 vs Leonardo Aw189 vs Piaggio Avanti Evo
The Bell 525 Relentless and Leonardo AW189 are medium twin‑engine helicopters, while the Daher TBM 960 and Piaggio Avanti EVO are pressurized fixed‑wing turboprop airplanes (the TBM is single‑engine; the Avanti is twin‑engine). In range terms, the TBM 960 and Avanti EVO generally lead among these four because airplanes cruise more efficiently; the TBM 960 is typically around the 1,000+ nautical mile class depending on reserves and payload, and the Avanti EVO is in a similar ballpark. The Bell 525 and AW189 usually offer shorter overall range (often in the several‑hundred‑nautical‑mile class), though they excel at point‑to‑point access without runways and can operate to helipads and confined areas. For passenger capacity, the TBM 960 is commonly configured for about 4–6 passengers plus pilot, while the Avanti EVO is typically around 6–8 passengers. The AW189 and Bell 525 can seat more in high‑density layouts (often up to the mid‑teens), but typical executive configurations are lower to prioritize comfort, baggage, and mission equipment.
| Spec | Bell 525 Relentless | Daher TBM 960 | AGUSTA / LEONARDO AW189 | Piaggio Avanti EVO |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 | 1 |
| Total Seats | 18 | 6 | 21 | 8 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Bell | Daher TBM | Leonardo | Piaggio |
| Aircraft Name | 525 Relentless | TBM 960 | AW189 | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 1730 | 651 | 1530 |
| Max Cabin Seats | 16 | — | 19 | 7 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 6675 | 2908 | — | 3775 |
| Standard Cabin Seats | 16 | 4 | 19 | 6 |
| Flight Deck (Base Spec) | Garmin G5000H | Garmin G3000 | EFIS | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 160 | 330 | 155 | 400 |
| Base Aircraft Price (USD) | $15,000,000 | $4,450,000 | $2,413,000 | $ 7,695,000 |
| 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 | 1 | 1 |
| Total Seats | 18 | 6 | 21 | 8 |
| Max Cabin Seats | 16 | — | 19 | 7 |
| Standard Cabin Seats | 16 | 4 | 19 | 6 |
| Lavatory | — | No | — | No |
| Galley Location | — | MID | — | — |
| Cabin Pressure (psi) | — | 6.2 | — | 9 |
| SL Cabin Altitude (ft) | — | 14390 | — | 24000 |
| Galley / Refreshment | — | — | — | No |
| Max Cabin Altitude (ft) | — | — | — | 6600 |
| Engine | ||||
| FADEC | Dual-Channel | Yes | Yes | Yes |
| Model | CT7-2F1 | TBM 960 | CT7-2E1 | PT6A–66B |
| Fuel Type | JetFuel | — | JetFuel | — |
| TBO (hrs) | 4000 | 3500 | 4000 | 3600 |
| Horsepower | 1800 | 850 | 1983 | 850 |
| No. of Engines | 2 | — | 2 | 2 |
| Fuel Capacity (gal) | 641 | — | — | — |
| Flat Rating | — | ISA + 49 | — | ISA + 28 |
| Fuel Burn (gph) | — | — | — | 100 |
| Dimensions | ||||
| Width (ft) | 25.77 | — | — | — |
| Length (ft) | 61.58 | 35.3 | 57.8 | 47.3 |
| Cabin Width (ft) | 7.58 | 4 | — | 6.1 |
| Cabin Height (ft) | 4.5 | 4.1 | — | 5.8 |
| Cabin Length (ft) | 15.5 | 13.4 | — | 14.9 |
| Overall Height (ft) | 18.18 | — | 16.6 | 13.1 |
| Rotor Diameter (ft) | 54.5 | — | 48 | — |
| Baggage Volume Ext. (cu. ft) | 128 | — | 85 | — |
| Wingspan (ft) | — | 42.1 | — | 47.1 |
| Cabin Volume (cu. ft) | — | 123 | 395 | — |
| Cabin Width - Floor (ft) | — | — | — | 3.5 |
| Baggage Volume Int. (cu. ft) | — | — | — | 35.2 |