Airbus Helicopters H225 vs Bell 525 Relentless vs Cessna Citation Xls vs Daher Tbm 960
The Airbus H225 and Bell 525 Relentless are large, long‑range helicopters aimed at offshore, SAR, and executive transport; both typically carry around 12–19 passengers depending on configuration. The H225 generally offers roughly 450–500 nm class range, while the Bell 525 is in a similar ballpark, commonly cited around the 500–600 nm class, with higher cruise speed than many legacy heavy helicopters. The Cessna Citation XLS+ is a midsize business jet designed for short to medium missions, typically seating about 7–9 passengers in executive layouts (up to around 12 with additional seating options). Its range is in the neighborhood of about 2,000–2,100 nm, enabling routine city‑pair travel beyond the reach of helicopters. The Daher TBM 960 is a high‑performance single‑engine turboprop, usually configured for 4–6 passengers plus a pilot. It typically offers about 1,500–1,700 nm range, trading jet speed and cabin volume for lower operating costs and access to shorter runways.
| Spec | AIRBUS H225 | Bell 525 Relentless | Cessna Citation XLS+ | Daher TBM 960 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | — | $ 5.34 | $ 2.25 |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 21 | 18 | 10 | 6 |
| Flight Rules | IFR | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Bell | Cessna Citation | Daher TBM |
| Aircraft Name | H225 | 525 Relentless | XLS+ | TBM 960 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 580 | 1906 | 1730 |
| DOC / nm / Seat | $ 0.99 | — | $ 0.67 | $ 0.56 |
| Max Cabin Seats | 28 | 16 | 9 | — |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 6675 | 7540 | 2908 |
| Standard Cabin Seats | 19 | 16 | 8 | 4 |
| Direct Operating Cost | $ 2,963 | — | $ 2,303 | $ 744 |
| Flight Deck (Base Spec) | EFIS | Garmin G5000H | Rockwell Collins Pro Line 21 | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 160 | 430 | 330 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,000,000 | $15,500,000 | $4,450,000 |
| Aircraft Type | — | — | — | Turbo Prop |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 21 | 18 | 10 | 6 |
| Max Cabin Seats | 28 | 16 | 9 | — |
| Standard Cabin Seats | 19 | 16 | 8 | 4 |
| Lavatory | — | — | 1 Enclosed Belted Flushing | No |
| Crew Rest | — | — | No | — |
| Jump Seat | — | — | No | — |
| Galley Location | — | — | FWD | MID |
| Lavatory Location | — | — | AFT | — |
| Cabin Pressure (psi) | — | — | 9.3 | 6.2 |
| Galley / Refreshment | — | — | Galley | — |
| SL Cabin Altitude (ft) | — | — | 25230 | 14390 |
| Engine | ||||
| FADEC | Yes | Dual-Channel | Yes | Yes |
| Model | Makila 2A1 | CT7-2F1 | PW545C | TBM 960 |
| Fuel Type | JetFuel | JetFuel | — | — |
| TBO (hrs) | 3500 | 4000 | 5000 | 3500 |
| Horsepower | 2100 | 1800 | — | 850 |
| No. of Engines | 2 | 2 | 2 | — |
| Fuel Capacity (gal) | 684 | 641 | — | — |
| Flat Rating | — | — | ISA + 10 | ISA + 49 |
| Thrust (lbs) | — | — | 4119 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 61.58 | 52.5 | 35.3 |
| Overall Height (ft) | 16.3 | 18.18 | 17.2 | — |
| Rotor Diameter (ft) | 53.2 | 54.5 | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | 123 |
| Width (ft) | — | 25.77 | — | — |
| Cabin Width (ft) | — | 7.58 | 5.5 | 4 |
| Cabin Height (ft) | — | 4.5 | 5.7 | 4.1 |
| Cabin Length (ft) | — | 15.5 | 18.5 | 13.4 |
| Baggage Volume Ext. (cu. ft) | — | 128 | 80 | — |
| Wingspan (ft) | — | — | 56.3 | 42.1 |
| Aisle Step (ft) | — | — | 0.7 | — |
| Cabin Width - Floor (ft) | — | — | 3.9 | — |
| Cabin Length - Seating (ft) | — | — | 14.3 | — |
| Baggage Volume Int. (cu. ft) | — | — | 10 | — |