Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Daher Tbm 960 vs Pilatus Pc 24
The Airbus H225 is a large twin‑engine helicopter used for offshore transport, SAR, and utility missions. It typically carries around 19 passengers in a high‑density layout (fewer in VIP) and offers a practical range on the order of roughly 500–600 nautical miles, trading speed and altitude for vertical lift and access to remote sites. The Boeing BBJ MAX 9 is a long‑range VIP airliner based on the 737 MAX 9, positioned for head‑of‑state and corporate shuttle missions. In BBJ configuration it commonly seats a few dozen up to roughly 50 passengers (far fewer than airline layouts) and provides intercontinental capability, typically about 3,200–3,600 nautical miles depending on fit and reserves. The Daher TBM 960 is a single‑engine turboprop in the high‑performance personal/corporate category. It carries up to 6 occupants (pilot plus up to 5) and delivers roughly 1,500–1,700 nautical miles of range. The Pilatus PC‑24 is a light jet aimed at business travel and mixed passenger/cargo use, often seating about 6–10 passengers, with a typical range around 2,000 nautical miles and the flexibility to use shorter or less‑prepared runways than many jets.
| Spec | AIRBUS H225 | Boeing BBJ MAX 9 | Daher TBM 960 | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.74 | $ 2.25 | $ 3.71 |
| Min Crew | 2 | 4 | 1 | 1 |
| Total Seats | 21 | 12 | 6 | 6 |
| Flight Rules | IFR | — | IFR | — |
| Manufacturer | Airbus Helicopters | Boeing | Daher TBM | Pilatus |
| Aircraft Name | H225 | BBJ MAX 9 | TBM 960 | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6376 | 1730 | 2076 |
| DOC / nm / Seat | $ 0.99 | $ 1.97 | $ 0.56 | $ 0.62 |
| Max Cabin Seats | 28 | 35 | — | 10 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 77120 | 2908 | 6680 |
| Standard Cabin Seats | 19 | 8 | 4 | 6 |
| Direct Operating Cost | $ 2,963 | $ 7,396 | $ 744 | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Honeywell | Garmin G3000 | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 470 | 330 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $107,700,000 | $4,450,000 | $11,800,000 |
| Aircraft Type | — | — | Turbo Prop | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 1 | 1 |
| Total Seats | 21 | 10 | 6 | 6 |
| Max Cabin Seats | 28 | 35 | — | 10 |
| Standard Cabin Seats | 19 | 8 | 4 | 6 |
| Configuration | — | Green Interior | — | — |
| Cabin Pressure (psi) | — | 9 | 6.2 | 9.3 |
| SL Cabin Altitude (ft) | — | 24000 | 14390 | 23500 |
| Lavatory | — | — | No | 1 Enclosed Flushing |
| Galley Location | — | — | MID | FWD |
| Crew Rest | — | — | — | No |
| Jump Seat | — | — | — | No |
| Cargo Door | — | — | — | Yes |
| Lavatory Location | — | — | — | FWD |
| Galley / Refreshment | — | — | — | Optional Refreshment Center |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | LEAP-1B | TBM 960 | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | On-Condition | 3500 | 5000 |
| Horsepower | 2100 | — | 850 | — |
| No. of Engines | 2 | 2 | — | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 15 | ISA + 49 | ISA + 23 |
| Thrust (lbs) | — | 28000 | — | 3435 |
| Dimensions | ||||
| Length (ft) | 63.4 | 138.4 | 35.3 | 52.2 |
| Overall Height (ft) | 16.3 | 40.3 | — | 17.4 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | 123 | — |
| Wingspan (ft) | — | 117.9 | 42.1 | 55.8 |
| Aisle Step (ft) | — | Flat Floor | — | Flat Floor |
| Cabin Width (ft) | — | 11.6 | 4 | 5.6 |
| Cabin Height (ft) | — | 7.1 | 4.1 | 5.1 |
| Cabin Length (ft) | — | 107.2 | 13.4 | 23 |
| Cabin Width - Floor (ft) | — | 10.7 | — | 3.8 |
| Cabin Length - Seating (ft) | — | 100.6 | — | 17 |
| Baggage Volume Ext. (cu. ft) | — | 1485 | — | — |
| Baggage Volume Int. (cu. ft) | — | — | — | 90 |