Bell 525 Relentless vs Piaggio Avanti Evo vs Piper M600 Sls vs Sikorsky S 92
The Bell 525 Relentless and Sikorsky S-92 are helicopters, while the Piaggio Avanti EVO and Piper M600 SLS are fixed‑wing turboprops; that category split largely drives their differences. For range, the fixed‑wing aircraft generally lead: the Piper M600 SLS is oriented toward long, efficient owner-flown trips, while the Piaggio Avanti EVO typically offers similarly strong or greater point‑to‑point range with higher cruise efficiency and speed in the turboprop class. The Bell 525 targets medium-to-long helicopter missions, commonly offering longer legs than many medium twins but usually less point‑to‑point range than comparable fixed‑wing turboprops. The Sikorsky S-92 is a larger, heavy helicopter optimized for offshore and utility work, with solid range but again generally constrained versus fixed‑wing aircraft on pure distance. Passenger capacity separates them most: the Piper M600 SLS is a single‑pilot capable aircraft typically seating around six, the Avanti EVO usually carries more (often seven to nine). The Bell 525 commonly accommodates a larger cabin load (often up to the low teens depending on layout), while the S-92 is the clear high-capacity option, frequently configured for roughly 19 passengers.
| Spec | Bell 525 Relentless | Piaggio Avanti EVO | Piper M600 SLS | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 | 2 |
| Total Seats | 18 | 8 | 6 | 21 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Bell | Piaggio | Piper | Sikorsky |
| Aircraft Name | 525 Relentless | Avanti EVO | M600 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 1530 | 1406 | 439 |
| Max Cabin Seats | 16 | 7 | — | 19 |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 6675 | 3775 | 2200 | 7417 |
| Standard Cabin Seats | 16 | 6 | 4 | 19 |
| Flight Deck (Base Spec) | Garmin G5000H | Rockwell Collins Pro Line 21 | Garmin G3000 | EFIS |
| Max Cruise Speed (ktas) | 160 | 400 | 274 | 155 |
| Base Aircraft Price (USD) | $15,000,000 | $ 7,695,000 | $3,081,400 | $30,650,000 |
| DOC / nm | — | — | $ 2.19 | $ 19.79 |
| DOC / nm / Seat | — | — | $ 0.55 | $ 0.94 |
| Direct Operating Cost | — | — | $ 603 | $ 3,068 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 | 2 |
| Total Seats | 18 | 8 | 5 | 21 |
| Max Cabin Seats | 16 | 7 | — | 19 |
| Standard Cabin Seats | 16 | 6 | 4 | 19 |
| Lavatory | — | No | No | — |
| Cabin Pressure (psi) | — | 9 | 5.6 | — |
| Galley / Refreshment | — | No | Refreshment Centre | — |
| SL Cabin Altitude (ft) | — | 24000 | 12600 | — |
| Max Cabin Altitude (ft) | — | 6600 | 8644 | — |
| Galley Location | — | — | MID | — |
| Engine | ||||
| FADEC | Dual-Channel | Yes | No | Yes |
| Model | CT7-2F1 | PT6A–66B | PT6A-42A | CT7-8A |
| Fuel Type | JetFuel | — | — | JetFuel |
| TBO (hrs) | 4000 | 3600 | 3600 | 4000 |
| Horsepower | 1800 | 850 | 600 | 2520 |
| No. of Engines | 2 | 2 | 1 | 1 |
| Fuel Capacity (gal) | 641 | — | 260 | 760 |
| Flat Rating | — | ISA + 28 | ISA + 55 | — |
| Fuel Burn (gph) | — | 100 | — | — |
| Dimensions | ||||
| Width (ft) | 25.77 | — | — | — |
| Length (ft) | 61.58 | 47.3 | 29.7 | — |
| Cabin Width (ft) | 7.58 | 6.1 | 4.1 | — |
| Cabin Height (ft) | 4.5 | 5.8 | 4 | — |
| Cabin Length (ft) | 15.5 | 14.9 | 12.3 | — |
| Overall Height (ft) | 18.18 | 13.1 | 11.3 | 17.8 |
| Rotor Diameter (ft) | 54.5 | — | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | — | — | 140 |
| Wingspan (ft) | — | 47.1 | 43.2 | — |
| Cabin Width - Floor (ft) | — | 3.5 | — | — |
| Baggage Volume Int. (cu. ft) | — | 35.2 | 20 | — |
| Cabin Volume (cu. ft) | — | — | 165 | 775 |