Bell 525 Relentless vs Daher Tbm 960 vs Gulfstream G700 vs Md Helicopters (mcdonnell Douglas) 902 Explorer
The Gulfstream G700 is a long‑range, large‑cabin business jet designed for intercontinental travel, carrying roughly 13 to 19 passengers depending on configuration and offering about 7,500 nautical miles of range. The Daher TBM 960 is a high‑performance single‑engine turboprop airplane in the owner‑pilot/short business trip category; it typically seats about 4 to 6 passengers (up to around 6–7 including pilot, depending on layout) and has roughly 1,700 nautical miles of range. The Bell 525 Relentless is a super‑medium helicopter aimed at offshore, corporate, and utility missions; it commonly accommodates around 16 passengers (with layouts varying by mission) and has on the order of 560 nautical miles of range. The MD Helicopters (McDonnell Douglas) 902 Explorer is a light helicopter used for public safety, EMS, and utility work; it typically carries about 4 to 6 passengers and has roughly 300 nautical miles of range. Overall, the G700 dominates range and cabin size, the TBM 960 offers efficient point‑to‑point airplane travel, and the helicopters trade range for vertical access and landing flexibility.
| Spec | Bell 525 Relentless | Daher TBM 960 | Gulfstream G700 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 3 |
| Min Crew | 2 | 1 | 4 |
| Total Seats | 18 | 6 | 16 |
| Flight Rules | IFR | IFR | — |
| Manufacturer | Bell | Daher TBM | Gulfstream |
| Aircraft Name | 525 Relentless | TBM 960 | G700 |
| Certification | FAA / EASA | FAA / EASA | In Development |
| Max Range (nm) | 580 | 1730 | 7500 |
| Max Cabin Seats | 16 | — | 19 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 6675 | 2908 | — |
| Standard Cabin Seats | 16 | 4 | 12 |
| Flight Deck (Base Spec) | Garmin G5000H | Garmin G3000 | Gulfstream Symmetry Flight Deck |
| Max Cruise Speed (ktas) | 160 | 330 | 516 |
| Base Aircraft Price (USD) | $15,000,000 | $4,450,000 | $78,000,000 |
| 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 | 4 |
| Total Seats | 18 | 6 | 16 |
| Max Cabin Seats | 16 | — | 19 |
| Standard Cabin Seats | 16 | 4 | 12 |
| Lavatory | — | No | — |
| Galley Location | — | MID | FWD |
| Cabin Pressure (psi) | — | 6.2 | — |
| SL Cabin Altitude (ft) | — | 14390 | — |
| Crew Rest | — | — | Optional |
| Jump Seat | — | — | Yes |
| Lavatory Location | — | — | FWD / AFT |
| Engine | |||
| FADEC | Dual-Channel | Yes | — |
| Model | CT7-2F1 | TBM 960 | Pearl 700 |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 4000 | 3500 | On Condition |
| Horsepower | 1800 | 850 | — |
| No. of Engines | 2 | — | 2 |
| Fuel Capacity (gal) | 641 | — | — |
| Flat Rating | — | ISA + 49 | — |
| Thrust (lbs) | — | — | 18250 |
| Dimensions | |||
| Width (ft) | 25.77 | — | — |
| Length (ft) | 61.58 | 35.3 | 109.9 |
| Cabin Width (ft) | 7.58 | 4 | 8.2 |
| Cabin Height (ft) | 4.5 | 4.1 | 6.25 |
| Cabin Length (ft) | 15.5 | 13.4 | 56.9 |
| Overall Height (ft) | 18.18 | — | 25.4 |
| Rotor Diameter (ft) | 54.5 | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | — | — |
| Wingspan (ft) | — | 42.1 | 103 |
| Cabin Volume (cu. ft) | — | 123 | — |
| Aisle Step (ft) | — | — | Flat Floor |
| Baggage Volume Int. (cu. ft) | — | — | 195 |