Bell 525 Relentless vs Daher Tbm 960 vs Sikorsky S 92
The Bell 525 Relentless and Sikorsky S-92 are both twin‑engine helicopters aimed at offshore, corporate, and utility missions, while the Daher TBM 960 is a single‑engine turboprop airplane optimized for fast, efficient point‑to‑point travel from runways. In range terms, the TBM 960 generally offers the longest legs for typical passenger transport, commonly around 1,000+ nautical miles depending on reserves and payload, whereas the Bell 525 is typically in the mid‑hundreds of nautical miles for mission profiles, and the S‑92 is also in the helicopter mid‑hundreds, often comparable but mission‑ and configuration‑dependent. Passenger capacity differs sharply: the TBM 960 is usually operated with about 4–6 passengers plus a pilot (up to roughly 6 passengers in many layouts), the Bell 525 is commonly configured for around a dozen to the high‑teens depending on seating and mission equipment, and the S‑92 is the larger people‑mover, often set up for roughly 19 passengers in offshore transport configurations (with other layouts possible).
| Spec | Bell 525 Relentless | Daher TBM 960 | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 18 | 6 | 21 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Bell | Daher TBM | Sikorsky |
| Aircraft Name | 525 Relentless | TBM 960 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 1730 | 439 |
| Max Cabin Seats | 16 | — | 19 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 6675 | 2908 | 7417 |
| Standard Cabin Seats | 16 | 4 | 19 |
| Flight Deck (Base Spec) | Garmin G5000H | Garmin G3000 | EFIS |
| Max Cruise Speed (ktas) | 160 | 330 | 155 |
| Base Aircraft Price (USD) | $15,000,000 | $4,450,000 | $30,650,000 |
| DOC / nm | — | $ 2.25 | $ 19.79 |
| Aircraft Type | — | Turbo Prop | — |
| DOC / nm / Seat | — | $ 0.56 | $ 0.94 |
| Direct Operating Cost | — | $ 744 | $ 3,068 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 18 | 6 | 21 |
| Max Cabin Seats | 16 | — | 19 |
| Standard Cabin Seats | 16 | 4 | 19 |
| Lavatory | — | No | — |
| Galley Location | — | MID | — |
| Cabin Pressure (psi) | — | 6.2 | — |
| SL Cabin Altitude (ft) | — | 14390 | — |
| Engine | |||
| FADEC | Dual-Channel | Yes | Yes |
| Model | CT7-2F1 | TBM 960 | CT7-8A |
| Fuel Type | JetFuel | — | JetFuel |
| TBO (hrs) | 4000 | 3500 | 4000 |
| Horsepower | 1800 | 850 | 2520 |
| No. of Engines | 2 | — | 1 |
| Fuel Capacity (gal) | 641 | — | 760 |
| Flat Rating | — | ISA + 49 | — |
| Dimensions | |||
| Width (ft) | 25.77 | — | — |
| Length (ft) | 61.58 | 35.3 | — |
| Cabin Width (ft) | 7.58 | 4 | — |
| Cabin Height (ft) | 4.5 | 4.1 | — |
| Cabin Length (ft) | 15.5 | 13.4 | — |
| Overall Height (ft) | 18.18 | — | 17.8 |
| Rotor Diameter (ft) | 54.5 | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | — | 140 |
| Wingspan (ft) | — | 42.1 | — |
| Cabin Volume (cu. ft) | — | 123 | 775 |