Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Daher Tbm 960 vs Gulfstream G700
The Airbus H225 is a heavy twin‑engine helicopter, best suited to short‑ to medium‑range missions such as offshore transport and SAR; its practical range is roughly 450–700 nm depending on payload and reserves, and it typically carries about 16–19 passengers in an oil‑and‑gas style configuration (more in high‑density layouts). The Boeing BBJ MAX 9 is a long‑range VIP airliner in the large‑cabin/head‑of‑state category; with auxiliary tanks it is commonly marketed around 6,000–6,600 nm, and while it can seat well over 150 in airline layout, VIP configurations often carry roughly 25–60 with bedrooms, lounges, and conference space. The Daher TBM 960 is a single‑engine turboprop in the owner‑pilot/business utility class; it offers about 1,400–1,700 nm range and seats typically 4–6 passengers plus a pilot. The Gulfstream G700 is an ultra‑long‑range business jet; range is about 7,500 nm, and it usually accommodates around 10–19 passengers in high‑comfort cabin layouts.
| Spec | AIRBUS H225 | Boeing BBJ MAX 9 | Daher TBM 960 | Gulfstream G700 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 3 |
| DOC / nm | $ 20.87 | $ 15.74 | $ 2.25 | — |
| Min Crew | 2 | 4 | 1 | 4 |
| Total Seats | 21 | 12 | 6 | 16 |
| Flight Rules | IFR | — | IFR | — |
| Manufacturer | Airbus Helicopters | Boeing | Daher TBM | Gulfstream |
| Aircraft Name | H225 | BBJ MAX 9 | TBM 960 | G700 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | In Development |
| Max Range (nm) | 454 | 6376 | 1730 | 7500 |
| DOC / nm / Seat | $ 0.99 | $ 1.97 | $ 0.56 | — |
| Max Cabin Seats | 28 | 35 | — | 19 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | 77120 | 2908 | — |
| Standard Cabin Seats | 19 | 8 | 4 | 12 |
| Direct Operating Cost | $ 2,963 | $ 7,396 | $ 744 | — |
| Flight Deck (Base Spec) | EFIS | Honeywell | Garmin G3000 | Gulfstream Symmetry Flight Deck |
| Max Cruise Speed (ktas) | 142 | 470 | 330 | 516 |
| Base Aircraft Price (USD) | $ 29,500,000 | $107,700,000 | $4,450,000 | $78,000,000 |
| Aircraft Type | — | — | Turbo Prop | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 1 | 4 |
| Total Seats | 21 | 10 | 6 | 16 |
| Max Cabin Seats | 28 | 35 | — | 19 |
| Standard Cabin Seats | 19 | 8 | 4 | 12 |
| Configuration | — | Green Interior | — | — |
| Cabin Pressure (psi) | — | 9 | 6.2 | — |
| SL Cabin Altitude (ft) | — | 24000 | 14390 | — |
| Lavatory | — | — | No | — |
| Galley Location | — | — | MID | FWD |
| Crew Rest | — | — | — | Optional |
| Jump Seat | — | — | — | Yes |
| Lavatory Location | — | — | — | FWD / AFT |
| Engine | ||||
| FADEC | Yes | Yes | Yes | — |
| Model | Makila 2A1 | LEAP-1B | TBM 960 | Pearl 700 |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | On-Condition | 3500 | On Condition |
| Horsepower | 2100 | — | 850 | — |
| No. of Engines | 2 | 2 | — | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 15 | ISA + 49 | — |
| Thrust (lbs) | — | 28000 | — | 18250 |
| Dimensions | ||||
| Length (ft) | 63.4 | 138.4 | 35.3 | 109.9 |
| Overall Height (ft) | 16.3 | 40.3 | — | 25.4 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | 123 | — |
| Wingspan (ft) | — | 117.9 | 42.1 | 103 |
| Aisle Step (ft) | — | Flat Floor | — | Flat Floor |
| Cabin Width (ft) | — | 11.6 | 4 | 8.2 |
| Cabin Height (ft) | — | 7.1 | 4.1 | 6.25 |
| Cabin Length (ft) | — | 107.2 | 13.4 | 56.9 |
| Cabin Width - Floor (ft) | — | 10.7 | — | — |
| Cabin Length - Seating (ft) | — | 100.6 | — | — |
| Baggage Volume Ext. (cu. ft) | — | 1485 | — | — |
| Baggage Volume Int. (cu. ft) | — | — | — | 195 |