Airbus Helicopters H225 vs Cessna 208b Grand Caravan Ex vs Daher Tbm 960 vs Gulfstream G700
The Airbus H225 is a large twin‑engine helicopter suited to offshore, SAR, and utility roles; it trades speed and range for vertical lift, typically carrying around 19 passengers in a high‑density configuration and offering roughly 500–700 nm of range depending on payload and reserves. The Cessna 208B Grand Caravan EX is a single‑engine turboprop utility aircraft optimized for short, rough fields and regional hauling; it commonly seats 9–14 passengers and can manage about 800–900 nm with typical loads. The Daher TBM 960 is a high‑performance single‑engine turboprop business aircraft focused on fast point‑to‑point travel; it usually carries 4–6 passengers (up to about 8 seats installed) and offers about 1,400–1,700 nm range depending on cruise and reserves. The Gulfstream G700 is an ultra‑long‑range business jet designed for intercontinental missions and high cabin comfort; it typically carries 12–16 passengers (certified for more) with range around 7,000–7,500 nm. Overall, capacity peaks with the H225, range with the G700, and the Caravan/TBM sit between as utility and speed‑oriented turboprops.
| Spec | AIRBUS H225 | Daher TBM 960 | Gulfstream G700 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 3 |
| DOC / nm | $ 20.87 | $ 2.25 | — |
| Min Crew | 2 | 1 | 4 |
| Total Seats | 21 | 6 | 16 |
| Flight Rules | IFR | IFR | — |
| Manufacturer | Airbus Helicopters | Daher TBM | Gulfstream |
| Aircraft Name | H225 | TBM 960 | G700 |
| Certification | FAA / EASA | FAA / EASA | In Development |
| Max Range (nm) | 454 | 1730 | 7500 |
| DOC / nm / Seat | $ 0.99 | $ 0.56 | — |
| Max Cabin Seats | 28 | — | 19 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | 2908 | — |
| Standard Cabin Seats | 19 | 4 | 12 |
| Direct Operating Cost | $ 2,963 | $ 744 | — |
| Flight Deck (Base Spec) | EFIS | Garmin G3000 | Gulfstream Symmetry Flight Deck |
| Max Cruise Speed (ktas) | 142 | 330 | 516 |
| Base Aircraft Price (USD) | $ 29,500,000 | $4,450,000 | $78,000,000 |
| Aircraft Type | — | Turbo Prop | — |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 4 |
| Total Seats | 21 | 6 | 16 |
| Max Cabin Seats | 28 | — | 19 |
| Standard Cabin Seats | 19 | 4 | 12 |
| Lavatory | — | No | — |
| Galley Location | — | MID | FWD |
| Cabin Pressure (psi) | — | 6.2 | — |
| SL Cabin Altitude (ft) | — | 14390 | — |
| Crew Rest | — | — | Optional |
| Jump Seat | — | — | Yes |
| Lavatory Location | — | — | FWD / AFT |
| Engine | |||
| FADEC | Yes | Yes | — |
| Model | Makila 2A1 | TBM 960 | Pearl 700 |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | 3500 | On Condition |
| Horsepower | 2100 | 850 | — |
| No. of Engines | 2 | — | 2 |
| Fuel Capacity (gal) | 684 | — | — |
| Flat Rating | — | ISA + 49 | — |
| Thrust (lbs) | — | — | 18250 |
| Dimensions | |||
| Length (ft) | 63.4 | 35.3 | 109.9 |
| Overall Height (ft) | 16.3 | — | 25.4 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | 123 | — |
| Wingspan (ft) | — | 42.1 | 103 |
| Cabin Width (ft) | — | 4 | 8.2 |
| Cabin Height (ft) | — | 4.1 | 6.25 |
| Cabin Length (ft) | — | 13.4 | 56.9 |
| Aisle Step (ft) | — | — | Flat Floor |
| Baggage Volume Int. (cu. ft) | — | — | 195 |