Airbus Helicopters H225 vs Cessna 208b Grand Caravan Ex vs Daher Tbm 960 vs Piaggio Avanti Evo
The Airbus H225 is a large twin‑engine helicopter suited to offshore, SAR, and heavy utility work. It typically carries around 16–19 passengers in an airliner‑style cabin and has a practical range on the order of about 450–600 nautical miles depending on configuration, payload, and reserves. The Cessna 208B Grand Caravan EX is a rugged single‑engine turboprop utility airplane optimized for short/rough strips and regional feeder missions. It generally seats 9–14 passengers and offers roughly 800–900 nautical miles of range, varying with load and conditions. The Daher TBM 960 is a high‑performance single‑engine turboprop executive aircraft. It is usually configured for 4–6 passengers (up to about 6–7 seats depending on layout) and delivers approximately 1,000–1,700 nautical miles of range depending on speed/altitude choices and reserves. The Piaggio Avanti EVO is a fast twin‑turboprop business aircraft with a stand‑up cabin feel for its class. It commonly seats 6–8 passengers and typically reaches about 1,300–1,700 nautical miles of range, mission‑dependent.
| Spec | AIRBUS H225 | Daher TBM 960 | Piaggio Avanti EVO |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 2.25 | — |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 21 | 6 | 8 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Daher TBM | Piaggio |
| Aircraft Name | H225 | TBM 960 | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1730 | 1530 |
| DOC / nm / Seat | $ 0.99 | $ 0.56 | — |
| Max Cabin Seats | 28 | — | 7 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | 2908 | 3775 |
| Standard Cabin Seats | 19 | 4 | 6 |
| Direct Operating Cost | $ 2,963 | $ 744 | — |
| Flight Deck (Base Spec) | EFIS | Garmin G3000 | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 142 | 330 | 400 |
| Base Aircraft Price (USD) | $ 29,500,000 | $4,450,000 | $ 7,695,000 |
| Aircraft Type | — | Turbo Prop | — |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 21 | 6 | 8 |
| Max Cabin Seats | 28 | — | 7 |
| Standard Cabin Seats | 19 | 4 | 6 |
| Lavatory | — | No | No |
| Galley Location | — | MID | — |
| Cabin Pressure (psi) | — | 6.2 | 9 |
| SL Cabin Altitude (ft) | — | 14390 | 24000 |
| Galley / Refreshment | — | — | No |
| Max Cabin Altitude (ft) | — | — | 6600 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Makila 2A1 | TBM 960 | PT6A–66B |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | 3500 | 3600 |
| Horsepower | 2100 | 850 | 850 |
| No. of Engines | 2 | — | 2 |
| Fuel Capacity (gal) | 684 | — | — |
| Flat Rating | — | ISA + 49 | ISA + 28 |
| Fuel Burn (gph) | — | — | 100 |
| Dimensions | |||
| Length (ft) | 63.4 | 35.3 | 47.3 |
| Overall Height (ft) | 16.3 | — | 13.1 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | 123 | — |
| Wingspan (ft) | — | 42.1 | 47.1 |
| Cabin Width (ft) | — | 4 | 6.1 |
| Cabin Height (ft) | — | 4.1 | 5.8 |
| Cabin Length (ft) | — | 13.4 | 14.9 |
| Cabin Width - Floor (ft) | — | — | 3.5 |
| Baggage Volume Int. (cu. ft) | — | — | 35.2 |