Airbus Helicopters H225 vs Cessna 208b Grand Caravan Ex vs Daher Tbm 960
The Airbus H225 is a heavy, twin‑engine helicopter built for offshore transport, search and rescue, and utility missions. Compared with the two fixed‑wing turboprops, it typically has the shortest point‑to‑point range because helicopters trade cruise efficiency for vertical lift, but it can operate without runways and carry a relatively large cabin load, commonly up to about 19 passengers depending on configuration. The Cessna 208B Grand Caravan EX is a single‑engine utility turboprop airplane optimized for rugged, short‑field operations. It generally offers longer range than the H225 and is frequently configured for around 9 passengers (with higher‑density seating possible in some roles), making it a workhorse for regional transport and freight where simple infrastructure is the norm. The Daher TBM 960 is a high‑performance single‑engine turboprop in the personal/business aviation category. It typically provides the longest range and fastest cruise of the three, but with the smallest passenger capacity, usually seating about 4 to 6 occupants in a premium cabin focused on speed and efficiency rather than maximum headcount.
| Spec | AIRBUS H225 | Daher TBM 960 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 20.87 | $ 2.25 |
| Min Crew | 2 | 1 |
| Total Seats | 21 | 6 |
| Flight Rules | IFR | IFR |
| Manufacturer | Airbus Helicopters | Daher TBM |
| Aircraft Name | H225 | TBM 960 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1730 |
| DOC / nm / Seat | $ 0.99 | $ 0.56 |
| Max Cabin Seats | 28 | — |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | 2908 |
| Standard Cabin Seats | 19 | 4 |
| Direct Operating Cost | $ 2,963 | $ 744 |
| Flight Deck (Base Spec) | EFIS | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 330 |
| Base Aircraft Price (USD) | $ 29,500,000 | $4,450,000 |
| Aircraft Type | — | Turbo Prop |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 1 |
| Total Seats | 21 | 6 |
| Max Cabin Seats | 28 | — |
| Standard Cabin Seats | 19 | 4 |
| Lavatory | — | No |
| Galley Location | — | MID |
| Cabin Pressure (psi) | — | 6.2 |
| SL Cabin Altitude (ft) | — | 14390 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | Makila 2A1 | TBM 960 |
| Fuel Type | JetFuel | — |
| TBO (hrs) | 3500 | 3500 |
| Horsepower | 2100 | 850 |
| No. of Engines | 2 | — |
| Fuel Capacity (gal) | 684 | — |
| Flat Rating | — | ISA + 49 |
| Dimensions | ||
| Length (ft) | 63.4 | 35.3 |
| Overall Height (ft) | 16.3 | — |
| Rotor Diameter (ft) | 53.2 | — |
| Cabin Volume (cu. ft) | 547 | 123 |
| Wingspan (ft) | — | 42.1 |
| Cabin Width (ft) | — | 4 |
| Cabin Height (ft) | — | 4.1 |
| Cabin Length (ft) | — | 13.4 |