Bell 525 Relentless vs Bombardier Global 7500 vs Daher Tbm 960 vs Md Helicopters (mcdonnell Douglas) 902 Explorer
The Bell 525 Relentless and the MD Helicopters 902 Explorer are helicopters, while the Bombardier Global 7500 is a long‑range business jet and the Daher TBM 960 is a high‑performance single‑engine turboprop airplane. In category and mission, the Global 7500 is built for intercontinental corporate travel at high altitude and high speed; the TBM 960 targets fast owner‑pilot or small executive trips with lower operating complexity; the Bell 525 is a fly‑by‑wire super‑medium helicopter aimed at offshore, corporate, and utility roles; and the 902 Explorer is a lighter twin‑engine helicopter commonly used for EMS, law enforcement, and utility work. Range differs dramatically: the Global 7500 leads at roughly 7,700 nautical miles, enabling nonstop long‑haul flights. The TBM 960 is mid‑range at about 1,400–1,700 nautical miles depending on profile. The Bell 525 is typically around 500–600 nautical miles, and the 902 Explorer is shorter, roughly 300–400 nautical miles. Passenger capacity follows mission: the Global 7500 typically carries around 8–19, the TBM 960 up to 6, the Bell 525 commonly about 16–20 (layout‑dependent), and the 902 Explorer about 8–10.
| Spec | Bell 525 Relentless | Bombardier Global 7500 | Daher TBM 960 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 18 | 14 | 6 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Bell | Bombardier | Daher TBM |
| Aircraft Name | 525 Relentless | Global 7500 | TBM 960 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 7700 | 1730 |
| Max Cabin Seats | 16 | 19 | — |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 6675 | — | 2908 |
| Standard Cabin Seats | 16 | 12 | 4 |
| Flight Deck (Base Spec) | Garmin G5000H | Bombardier Vision (Pro Line Fusion) | Garmin G3000 |
| Max Cruise Speed (ktas) | 160 | 516 | 330 |
| Base Aircraft Price (USD) | $15,000,000 | $75,000,000 | $4,450,000 |
| DOC / nm | — | $ 9.50 | $ 2.25 |
| Aircraft Type | — | Business Jet | Turbo Prop |
| DOC / nm / Seat | — | $ 0.79 | $ 0.56 |
| Direct Operating Cost | — | $ 4,900 | $ 744 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 18 | 14 | 6 |
| Max Cabin Seats | 16 | 19 | — |
| Standard Cabin Seats | 16 | 12 | 4 |
| Lavatory | — | 2 Enclosed Flushing | No |
| Crew Rest | — | Yes | — |
| Jump Seat | — | Yes | — |
| Galley Location | — | FWD | MID |
| Lavatory Location | — | FWD / AFT | — |
| Galley / Refreshment | — | Galley | — |
| Max Cabin Altitude (ft) | — | 4500 | — |
| Cabin Pressure (psi) | — | — | 6.2 |
| SL Cabin Altitude (ft) | — | — | 14390 |
| Engine | |||
| FADEC | Dual-Channel | Yes | Yes |
| Model | CT7-2F1 | Passport | TBM 960 |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 4000 | On-Condition | 3500 |
| Horsepower | 1800 | — | 850 |
| No. of Engines | 2 | 2 | — |
| Fuel Capacity (gal) | 641 | — | — |
| Flat Rating | — | ISA + 15 | ISA + 49 |
| Thrust (lbs) | — | 18920 | — |
| Dimensions | |||
| Width (ft) | 25.77 | — | — |
| Length (ft) | 61.58 | 111 | 35.3 |
| Cabin Width (ft) | 7.58 | 8 | 4 |
| Cabin Height (ft) | 4.5 | 6.2 | 4.1 |
| Cabin Length (ft) | 15.5 | 54.5 | 13.4 |
| Overall Height (ft) | 18.18 | 27 | — |
| Rotor Diameter (ft) | 54.5 | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | — | — |
| Wingspan (ft) | — | 104 | 42.1 |
| Cabin Volume (cu. ft) | — | — | 123 |