Bell 525 Relentless vs Daher Tbm 960 vs Piaggio Avanti Evo
The Bell 525 Relentless is a twin‑engine helicopter aimed at vertical-lift missions, trading runway independence for lower cruise efficiency than fixed‑wing aircraft. It typically carries up to about 16 passengers in high-density seating (fewer in executive layouts) and offers a practical mission range on the order of roughly 500–600 nautical miles, varying with payload and reserves. The Daher TBM 960 is a single‑engine turboprop airplane in the high‑performance personal/corporate category. It is optimized for speed and efficiency with runway access, usually seating 4–6 passengers (up to around 6–7 plus pilot depending on configuration). Its range is generally around 1,400–1,700 nautical miles, again depending on power settings, payload, and reserves. The Piaggio Avanti EVO is a twin‑engine turboprop airplane positioned as a fast, cabin-comfort business aircraft. It typically seats about 7–9 passengers and combines jet‑like cruise speeds with turboprop economics. Its range commonly falls around 1,400–1,700 nautical miles depending on configuration and mission profile.
| Spec | Bell 525 Relentless | Daher TBM 960 | Piaggio Avanti EVO |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 18 | 6 | 8 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Bell | Daher TBM | Piaggio |
| Aircraft Name | 525 Relentless | TBM 960 | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 1730 | 1530 |
| Max Cabin Seats | 16 | — | 7 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 6675 | 2908 | 3775 |
| Standard Cabin Seats | 16 | 4 | 6 |
| Flight Deck (Base Spec) | Garmin G5000H | Garmin G3000 | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 160 | 330 | 400 |
| Base Aircraft Price (USD) | $15,000,000 | $4,450,000 | $ 7,695,000 |
| DOC / nm | — | $ 2.25 | — |
| Aircraft Type | — | Turbo Prop | — |
| DOC / nm / Seat | — | $ 0.56 | — |
| Direct Operating Cost | — | $ 744 | — |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 18 | 6 | 8 |
| Max Cabin Seats | 16 | — | 7 |
| Standard Cabin Seats | 16 | 4 | 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 |
| Model | CT7-2F1 | TBM 960 | PT6A–66B |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 4000 | 3500 | 3600 |
| Horsepower | 1800 | 850 | 850 |
| No. of Engines | 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 | 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 | — | 13.1 |
| Rotor Diameter (ft) | 54.5 | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | — | — |
| Wingspan (ft) | — | 42.1 | 47.1 |
| Cabin Volume (cu. ft) | — | 123 | — |
| Cabin Width - Floor (ft) | — | — | 3.5 |
| Baggage Volume Int. (cu. ft) | — | — | 35.2 |