Airbus Helicopters H225 vs Bombardier Global 7500 vs Cessna Citation Xls vs Daher Tbm 960
The Airbus H225 is a heavy twin‑engine helicopter suited to offshore, SAR, and utility missions. Its category is rotorcraft rather than business aviation; typical range is roughly 450–600 nautical miles depending on payload and reserves, and it can carry a large cabin load, commonly around 16–19 passengers (higher-density configurations are possible but mission-dependent). The Bombardier Global 7500 is an ultra‑long‑range business jet designed for intercontinental travel. It offers about 7,700 nautical miles of range and typically seats 14–19 passengers in executive layouts. The Cessna Citation XLS+ is a midsize business jet aimed at efficient regional missions and short‑to‑medium stage lengths. Its range is about 2,100 nautical miles, with typical seating for 8–9 passengers (often up to 12 depending on configuration). The Daher TBM 960 is a high‑performance single‑engine turboprop, positioned below light jets in cabin size but strong on efficiency and runway flexibility. Range is roughly 1,700 nautical miles, and capacity is generally 4–6 passengers plus a pilot.
| Spec | AIRBUS H225 | Bombardier Global 7500 | Cessna Citation XLS+ | Daher TBM 960 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 9.50 | $ 5.34 | $ 2.25 |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 21 | 14 | 10 | 6 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Airbus Helicopters | Bombardier | Cessna Citation | Daher TBM |
| Aircraft Name | H225 | Global 7500 | XLS+ | TBM 960 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 7700 | 1906 | 1730 |
| DOC / nm / Seat | $ 0.99 | $ 0.79 | $ 0.67 | $ 0.56 |
| Max Cabin Seats | 28 | 19 | 9 | — |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | — | 7540 | 2908 |
| Standard Cabin Seats | 19 | 12 | 8 | 4 |
| Direct Operating Cost | $ 2,963 | $ 4,900 | $ 2,303 | $ 744 |
| Flight Deck (Base Spec) | EFIS | Bombardier Vision (Pro Line Fusion) | Rockwell Collins Pro Line 21 | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 516 | 430 | 330 |
| Base Aircraft Price (USD) | $ 29,500,000 | $75,000,000 | $15,500,000 | $4,450,000 |
| Aircraft Type | — | Business Jet | — | Turbo Prop |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 21 | 14 | 10 | 6 |
| Max Cabin Seats | 28 | 19 | 9 | — |
| Standard Cabin Seats | 19 | 12 | 8 | 4 |
| Lavatory | — | 2 Enclosed Flushing | 1 Enclosed Belted Flushing | No |
| Crew Rest | — | Yes | No | — |
| Jump Seat | — | Yes | No | — |
| Galley Location | — | FWD | FWD | MID |
| Lavatory Location | — | FWD / AFT | AFT | — |
| Galley / Refreshment | — | Galley | Galley | — |
| Max Cabin Altitude (ft) | — | 4500 | — | — |
| Cabin Pressure (psi) | — | — | 9.3 | 6.2 |
| SL Cabin Altitude (ft) | — | — | 25230 | 14390 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | Passport | PW545C | TBM 960 |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | On-Condition | 5000 | 3500 |
| Horsepower | 2100 | — | — | 850 |
| No. of Engines | 2 | 2 | 2 | — |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 15 | ISA + 10 | ISA + 49 |
| Thrust (lbs) | — | 18920 | 4119 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 111 | 52.5 | 35.3 |
| Overall Height (ft) | 16.3 | 27 | 17.2 | — |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | 123 |
| Wingspan (ft) | — | 104 | 56.3 | 42.1 |
| Cabin Width (ft) | — | 8 | 5.5 | 4 |
| Cabin Height (ft) | — | 6.2 | 5.7 | 4.1 |
| Cabin Length (ft) | — | 54.5 | 18.5 | 13.4 |
| Aisle Step (ft) | — | — | 0.7 | — |
| Cabin Width - Floor (ft) | — | — | 3.9 | — |
| Cabin Length - Seating (ft) | — | — | 14.3 | — |
| Baggage Volume Ext. (cu. ft) | — | — | 80 | — |
| Baggage Volume Int. (cu. ft) | — | — | 10 | — |