Bell 525 Relentless vs Daher Tbm 960 vs Gulfstream G700 vs Pilatus Pc 24
The Bell 525 Relentless is a long-range commercial helicopter, suited to offshore and executive point-to-point missions where vertical access matters. It typically carries around a dozen passengers in a high-density configuration (fewer in executive layouts) and offers roughly a few-hundred–nautical-mile class range, commonly cited around 500–600 nm depending on reserves and payload. The Daher TBM 960 is a single‑engine turboprop business aircraft focused on speed and efficiency for small parties. It is generally flown with 1–2 pilots and about 4–6 passengers, with range on the order of about 1,400–1,700 nm depending on conditions and reserves. The Gulfstream G700 is an ultra‑long‑range large‑cabin business jet designed for intercontinental travel. Typical passenger loads are about 12–16 (with higher certified maxima), and its range is roughly 7,500 nm class. The Pilatus PC‑24 is a light jet optimized for versatility, including operating from shorter and rougher runways than many jets. It commonly seats 6–10 passengers (higher maximums available) with range around 2,000 nm class.
| Spec | Bell 525 Relentless | Daher TBM 960 | Gulfstream G700 | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| Min Crew | 2 | 1 | 4 | 1 |
| Total Seats | 18 | 6 | 16 | 6 |
| Flight Rules | IFR | IFR | — | — |
| Manufacturer | Bell | Daher TBM | Gulfstream | Pilatus |
| Aircraft Name | 525 Relentless | TBM 960 | G700 | PC-24 |
| Certification | FAA / EASA | FAA / EASA | In Development | FAA / EASA |
| Max Range (nm) | 580 | 1730 | 7500 | 2076 |
| Max Cabin Seats | 16 | — | 19 | 10 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 6675 | 2908 | — | 6680 |
| Standard Cabin Seats | 16 | 4 | 12 | 6 |
| Flight Deck (Base Spec) | Garmin G5000H | Garmin G3000 | Gulfstream Symmetry Flight Deck | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 160 | 330 | 516 | 440 |
| Base Aircraft Price (USD) | $15,000,000 | $4,450,000 | $78,000,000 | $11,800,000 |
| DOC / nm | — | $ 2.25 | — | $ 3.71 |
| Aircraft Type | — | Turbo Prop | — | — |
| DOC / nm / Seat | — | $ 0.56 | — | $ 0.62 |
| Direct Operating Cost | — | $ 744 | — | $ 1,619 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 4 | 1 |
| Total Seats | 18 | 6 | 16 | 6 |
| Max Cabin Seats | 16 | — | 19 | 10 |
| Standard Cabin Seats | 16 | 4 | 12 | 6 |
| Lavatory | — | No | — | 1 Enclosed Flushing |
| Galley Location | — | MID | FWD | FWD |
| Cabin Pressure (psi) | — | 6.2 | — | 9.3 |
| SL Cabin Altitude (ft) | — | 14390 | — | 23500 |
| Crew Rest | — | — | Optional | No |
| Jump Seat | — | — | Yes | No |
| Lavatory Location | — | — | FWD / AFT | FWD |
| Cargo Door | — | — | — | Yes |
| Galley / Refreshment | — | — | — | Optional Refreshment Center |
| Engine | ||||
| FADEC | Dual-Channel | Yes | — | Yes |
| Model | CT7-2F1 | TBM 960 | Pearl 700 | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 4000 | 3500 | On Condition | 5000 |
| Horsepower | 1800 | 850 | — | — |
| No. of Engines | 2 | — | 2 | 2 |
| Fuel Capacity (gal) | 641 | — | — | — |
| Flat Rating | — | ISA + 49 | — | ISA + 23 |
| Thrust (lbs) | — | — | 18250 | 3435 |
| Dimensions | ||||
| Width (ft) | 25.77 | — | — | — |
| Length (ft) | 61.58 | 35.3 | 109.9 | 52.2 |
| Cabin Width (ft) | 7.58 | 4 | 8.2 | 5.6 |
| Cabin Height (ft) | 4.5 | 4.1 | 6.25 | 5.1 |
| Cabin Length (ft) | 15.5 | 13.4 | 56.9 | 23 |
| Overall Height (ft) | 18.18 | — | 25.4 | 17.4 |
| Rotor Diameter (ft) | 54.5 | — | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | — | — | — |
| Wingspan (ft) | — | 42.1 | 103 | 55.8 |
| Cabin Volume (cu. ft) | — | 123 | — | — |
| Aisle Step (ft) | — | — | Flat Floor | Flat Floor |
| Baggage Volume Int. (cu. ft) | — | — | 195 | 90 |
| Cabin Width - Floor (ft) | — | — | — | 3.8 |
| Cabin Length - Seating (ft) | — | — | — | 17 |