Airbus Helicopters H225 vs Cessna Citation Xls vs Daher Tbm 960 vs Piper M600 Sls
The Airbus H225 is a heavy twin‑engine helicopter built for offshore, SAR, and utility work rather than point‑to‑point business travel. It typically carries around 16–19 passengers in high‑density seating (fewer in VIP layouts) and has an operational range on the order of roughly 500–700 nautical miles depending on tanks, payload, and mission profile. The Cessna Citation XLS+ is a light business jet optimized for fast, comfortable regional travel. It generally seats 7–9 passengers and offers about 1,700–2,100 nautical miles of range depending on reserves and operating conditions. The Daher TBM 960 is a high‑performance single‑engine turboprop aimed at owner‑pilots needing jet‑like efficiency. It usually carries 4–6 passengers (up to 6 seats) and can reach roughly 1,400–1,700 nautical miles. The Piper M600 SLS is a more entry‑level single‑engine turboprop, typically seating 4–6, with range commonly around 1,000–1,200 nautical miles.
| Spec | AIRBUS H225 | Cessna Citation XLS+ | Daher TBM 960 | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 5.34 | $ 2.25 | $ 2.19 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 10 | 6 | 6 |
| Flight Rules | IFR | — | IFR | IFR |
| Manufacturer | Airbus Helicopters | Cessna Citation | Daher TBM | Piper |
| Aircraft Name | H225 | XLS+ | TBM 960 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1906 | 1730 | 1406 |
| DOC / nm / Seat | $ 0.99 | $ 0.67 | $ 0.56 | $ 0.55 |
| Max Cabin Seats | 28 | 9 | — | — |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 7540 | 2908 | 2200 |
| Standard Cabin Seats | 19 | 8 | 4 | 4 |
| Direct Operating Cost | $ 2,963 | $ 2,303 | $ 744 | $ 603 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Garmin G3000 | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 430 | 330 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,500,000 | $4,450,000 | $3,081,400 |
| Aircraft Type | — | — | Turbo Prop | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 10 | 6 | 5 |
| Max Cabin Seats | 28 | 9 | — | — |
| Standard Cabin Seats | 19 | 8 | 4 | 4 |
| Lavatory | — | 1 Enclosed Belted Flushing | No | No |
| Crew Rest | — | No | — | — |
| Jump Seat | — | No | — | — |
| Galley Location | — | FWD | MID | MID |
| Lavatory Location | — | AFT | — | — |
| Cabin Pressure (psi) | — | 9.3 | 6.2 | 5.6 |
| Galley / Refreshment | — | Galley | — | Refreshment Centre |
| SL Cabin Altitude (ft) | — | 25230 | 14390 | 12600 |
| Max Cabin Altitude (ft) | — | — | — | 8644 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | Makila 2A1 | PW545C | TBM 960 | PT6A-42A |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | 5000 | 3500 | 3600 |
| Horsepower | 2100 | — | 850 | 600 |
| No. of Engines | 2 | 2 | — | 1 |
| Fuel Capacity (gal) | 684 | — | — | 260 |
| Flat Rating | — | ISA + 10 | ISA + 49 | ISA + 55 |
| Thrust (lbs) | — | 4119 | — | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 52.5 | 35.3 | 29.7 |
| Overall Height (ft) | 16.3 | 17.2 | — | 11.3 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | 123 | 165 |
| Wingspan (ft) | — | 56.3 | 42.1 | 43.2 |
| Aisle Step (ft) | — | 0.7 | — | — |
| Cabin Width (ft) | — | 5.5 | 4 | 4.1 |
| Cabin Height (ft) | — | 5.7 | 4.1 | 4 |
| Cabin Length (ft) | — | 18.5 | 13.4 | 12.3 |
| Cabin Width - Floor (ft) | — | 3.9 | — | — |
| Cabin Length - Seating (ft) | — | 14.3 | — | — |
| Baggage Volume Ext. (cu. ft) | — | 80 | — | — |
| Baggage Volume Int. (cu. ft) | — | 10 | — | 20 |