Bell 525 Relentless vs Daher Tbm 960 vs Pilatus Pc 24 vs Sikorsky S 92
The Bell 525 Relentless and Sikorsky S-92 are twin‑engine helicopters aimed at offshore, corporate, and utility missions, while the Daher TBM 960 and Pilatus PC‑24 are fixed‑wing business aircraft (a high‑performance single‑engine turboprop and a light jet, respectively). In category terms, the TBM 960 is best seen as an owner‑flown or small‑team business turboprop; the PC‑24 is a light business jet designed to carry more people and operate from shorter or less‑prepared runways; the Bell 525 is a modern super‑medium helicopter; and the S‑92 is a larger medium helicopter commonly used for offshore transport and VIP configurations. For range, the fixed‑wing aircraft generally travel farther and faster on a trip profile: the TBM 960 is typically around the 1,400–1,700 nm class, and the PC‑24 is roughly around 1,800–2,000 nm depending on load. Helicopter ranges are shorter, with the Bell 525 and S‑92 commonly in the several‑hundred‑nautical‑mile class (often roughly 500–600+ nm, mission dependent). Passenger capacity is usually highest in the S‑92 (often configured around 12–19), followed by the Bell 525 (around 12–16), while the PC‑24 typically seats about 6–10 and the TBM 960 about 4–6.
| Spec | Bell 525 Relentless | Daher TBM 960 | Pilatus PC-24 | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 | 2 |
| Total Seats | 18 | 6 | 6 | 21 |
| Flight Rules | IFR | IFR | — | IFR |
| Manufacturer | Bell | Daher TBM | Pilatus | Sikorsky |
| Aircraft Name | 525 Relentless | TBM 960 | PC-24 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 1730 | 2076 | 439 |
| Max Cabin Seats | 16 | — | 10 | 19 |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 6675 | 2908 | 6680 | 7417 |
| Standard Cabin Seats | 16 | 4 | 6 | 19 |
| Flight Deck (Base Spec) | Garmin G5000H | Garmin G3000 | Pilatus ACE (Primus Apex) | EFIS |
| Max Cruise Speed (ktas) | 160 | 330 | 440 | 155 |
| Base Aircraft Price (USD) | $15,000,000 | $4,450,000 | $11,800,000 | $30,650,000 |
| DOC / nm | — | $ 2.25 | $ 3.71 | $ 19.79 |
| Aircraft Type | — | Turbo Prop | — | — |
| DOC / nm / Seat | — | $ 0.56 | $ 0.62 | $ 0.94 |
| Direct Operating Cost | — | $ 744 | $ 1,619 | $ 3,068 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 | 2 |
| Total Seats | 18 | 6 | 6 | 21 |
| Max Cabin Seats | 16 | — | 10 | 19 |
| Standard Cabin Seats | 16 | 4 | 6 | 19 |
| 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 | FJ44-4A-QPM | CT7-8A |
| Fuel Type | JetFuel | — | — | JetFuel |
| TBO (hrs) | 4000 | 3500 | 5000 | 4000 |
| Horsepower | 1800 | 850 | — | 2520 |
| No. of Engines | 2 | — | 2 | 1 |
| Fuel Capacity (gal) | 641 | — | — | 760 |
| Flat Rating | — | ISA + 49 | ISA + 23 | — |
| Thrust (lbs) | — | — | 3435 | — |
| Dimensions | ||||
| Width (ft) | 25.77 | — | — | — |
| Length (ft) | 61.58 | 35.3 | 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 | — | 17.4 | 17.8 |
| Rotor Diameter (ft) | 54.5 | — | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | — | — | 140 |
| Wingspan (ft) | — | 42.1 | 55.8 | — |
| Cabin Volume (cu. ft) | — | 123 | — | 775 |
| Aisle Step (ft) | — | — | Flat Floor | — |
| Cabin Width - Floor (ft) | — | — | 3.8 | — |
| Cabin Length - Seating (ft) | — | — | 17 | — |
| Baggage Volume Int. (cu. ft) | — | — | 90 | — |