Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Bombardier Global 7500 vs Daher Tbm 960
The Airbus H225 is a twin‑engine helicopter, optimized for vertical lift and short‑range missions rather than intercity air travel; typical range is roughly 450–650 nm depending on load and reserves, with passenger capacity commonly around 16–19 in an offshore/transport layout. The Boeing BBJ MAX 9 is a VIP-configured airliner based on the 737 MAX 9, offering true long-range airline performance; range is typically about 3,200–3,600 nm, and capacity varies widely by interior but is often set around 25–50 passengers for executive use (far more in airline seating). The Bombardier Global 7500 is an ultra‑long‑range business jet built for nonstop intercontinental legs, around 7,700 nm range, usually carrying about 8–19 passengers in high-comfort layouts. The Daher TBM 960 is a single‑engine turboprop in the owner‑pilot/short business trip category; range is about 1,400–1,700 nm and seating is typically 4–6 passengers plus a pilot, trading speed and flexibility for lower operating costs.
| Spec | AIRBUS H225 | Boeing BBJ MAX 9 | Bombardier Global 7500 | Daher TBM 960 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.74 | $ 9.50 | $ 2.25 |
| Min Crew | 2 | 4 | 2 | 1 |
| Total Seats | 21 | 12 | 14 | 6 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Airbus Helicopters | Boeing | Bombardier | Daher TBM |
| Aircraft Name | H225 | BBJ MAX 9 | Global 7500 | TBM 960 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6376 | 7700 | 1730 |
| DOC / nm / Seat | $ 0.99 | $ 1.97 | $ 0.79 | $ 0.56 |
| Max Cabin Seats | 28 | 35 | 19 | — |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 77120 | — | 2908 |
| Standard Cabin Seats | 19 | 8 | 12 | 4 |
| Direct Operating Cost | $ 2,963 | $ 7,396 | $ 4,900 | $ 744 |
| Flight Deck (Base Spec) | EFIS | Honeywell | Bombardier Vision (Pro Line Fusion) | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 470 | 516 | 330 |
| Base Aircraft Price (USD) | $ 29,500,000 | $107,700,000 | $75,000,000 | $4,450,000 |
| Aircraft Type | — | — | Business Jet | Turbo Prop |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 2 | 1 |
| Total Seats | 21 | 10 | 14 | 6 |
| Max Cabin Seats | 28 | 35 | 19 | — |
| Standard Cabin Seats | 19 | 8 | 12 | 4 |
| Configuration | — | Green Interior | — | — |
| Cabin Pressure (psi) | — | 9 | — | 6.2 |
| SL Cabin Altitude (ft) | — | 24000 | — | 14390 |
| 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 | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | LEAP-1B | Passport | TBM 960 |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | On-Condition | On-Condition | 3500 |
| Horsepower | 2100 | — | — | 850 |
| No. of Engines | 2 | 2 | 2 | — |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 15 | ISA + 15 | ISA + 49 |
| Thrust (lbs) | — | 28000 | 18920 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 138.4 | 111 | 35.3 |
| Overall Height (ft) | 16.3 | 40.3 | 27 | — |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | 123 |
| Wingspan (ft) | — | 117.9 | 104 | 42.1 |
| Aisle Step (ft) | — | Flat Floor | — | — |
| Cabin Width (ft) | — | 11.6 | 8 | 4 |
| Cabin Height (ft) | — | 7.1 | 6.2 | 4.1 |
| Cabin Length (ft) | — | 107.2 | 54.5 | 13.4 |
| Cabin Width - Floor (ft) | — | 10.7 | — | — |
| Cabin Length - Seating (ft) | — | 100.6 | — | — |
| Baggage Volume Ext. (cu. ft) | — | 1485 | — | — |