Bell 525 Relentless vs Cessna Citation Xls vs Daher Tbm 960 vs Leonardo Aw189
The Bell 525 Relentless and Leonardo AW189 are twin‑engine helicopters suited to vertical access and offshore or utility-style missions, while the Cessna Citation XLS+ is a midsize business jet optimized for fast city‑pair travel, and the Daher TBM 960 is a high‑performance single‑engine turboprop aimed at efficient owner‑operation. For range, the Citation XLS+ is typically the longest‑leg option in this group, commonly around the ~2,000‑nautical‑mile class depending on reserves and loading. The TBM 960 is also long‑range for its category, generally in the ~1,400–1,700‑nautical‑mile class. Helicopter ranges are shorter: the AW189 and Bell 525 are often in the several‑hundred‑nautical‑mile range, with typical missions commonly under ~500 nautical miles, though exact figures vary by fuel, payload, and reserve requirements. For passenger capacity, the Citation XLS+ usually seats about 8–9 in a typical executive layout. The TBM 960 generally carries 4–6 passengers plus a pilot. The AW189 is commonly configured for roughly 12–16 passengers (or more in high-density layouts). The Bell 525 is typically in the ~10–16 passenger range depending on configuration.
| Spec | Bell 525 Relentless | Cessna Citation XLS+ | Daher TBM 960 | AGUSTA / LEONARDO AW189 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 18 | 10 | 6 | 21 |
| Flight Rules | IFR | — | IFR | IFR |
| Manufacturer | Bell | Cessna Citation | Daher TBM | Leonardo |
| Aircraft Name | 525 Relentless | XLS+ | TBM 960 | AW189 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 1906 | 1730 | 651 |
| Max Cabin Seats | 16 | 9 | — | 19 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 6675 | 7540 | 2908 | — |
| Standard Cabin Seats | 16 | 8 | 4 | 19 |
| Flight Deck (Base Spec) | Garmin G5000H | Rockwell Collins Pro Line 21 | Garmin G3000 | EFIS |
| Max Cruise Speed (ktas) | 160 | 430 | 330 | 155 |
| Base Aircraft Price (USD) | $15,000,000 | $15,500,000 | $4,450,000 | $2,413,000 |
| DOC / nm | — | $ 5.34 | $ 2.25 | $ 15.57 |
| DOC / nm / Seat | — | $ 0.67 | $ 0.56 | $ 0.74 |
| Direct Operating Cost | — | $ 2,303 | $ 744 | $ 2,413 |
| Aircraft Type | — | — | Turbo Prop | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 18 | 10 | 6 | 21 |
| Max Cabin Seats | 16 | 9 | — | 19 |
| Standard Cabin Seats | 16 | 8 | 4 | 19 |
| 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 | Dual-Channel | Yes | Yes | Yes |
| Model | CT7-2F1 | PW545C | TBM 960 | CT7-2E1 |
| Fuel Type | JetFuel | — | — | JetFuel |
| TBO (hrs) | 4000 | 5000 | 3500 | 4000 |
| Horsepower | 1800 | — | 850 | 1983 |
| No. of Engines | 2 | 2 | — | 2 |
| Fuel Capacity (gal) | 641 | — | — | — |
| Flat Rating | — | ISA + 10 | ISA + 49 | — |
| Thrust (lbs) | — | 4119 | — | — |
| Dimensions | ||||
| Width (ft) | 25.77 | — | — | — |
| Length (ft) | 61.58 | 52.5 | 35.3 | 57.8 |
| 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 | — |
| Overall Height (ft) | 18.18 | 17.2 | — | 16.6 |
| Rotor Diameter (ft) | 54.5 | — | — | 48 |
| Baggage Volume Ext. (cu. ft) | 128 | 80 | — | 85 |
| 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 | — | — |
| Cabin Volume (cu. ft) | — | — | 123 | 395 |