Bell 525 Relentless vs Cessna Citation Xls vs Leonardo Aw189 vs Sikorsky S 92
The Bell 525 Relentless and Leonardo AW189 are super-medium helicopters, while the Sikorsky S-92 is a larger, heavy helicopter; the Cessna Citation XLS+ is a midsize business jet. In range terms, the Citation XLS+ generally offers the longest typical trip capability for point-to-point travel, commonly around 2,000+ nautical miles depending on payload and conditions, because it cruises faster and more efficiently than rotorcraft. Among the helicopters, the S-92 and AW189 are broadly comparable in practical mission range, often on the order of roughly 450–550 nautical miles with reserves (mission dependent), while the Bell 525 is in a similar super-medium bracket and is often cited around the ~500-nautical-mile class for typical offshore-style missions. For passenger capacity, the Citation XLS+ is usually configured for about 8–9 passengers in executive layout. The Bell 525 and AW189 commonly seat roughly 12–16 passengers depending on configuration, while the larger S-92 typically carries the most, often around 16–19 passengers in high-density seating (with fewer in VIP layouts).
| Spec | Bell 525 Relentless | Cessna Citation XLS+ | AGUSTA / LEONARDO AW189 | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 2 |
| Total Seats | 18 | 10 | 21 | 21 |
| Flight Rules | IFR | — | IFR | IFR |
| Manufacturer | Bell | Cessna Citation | Leonardo | Sikorsky |
| Aircraft Name | 525 Relentless | XLS+ | AW189 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 1906 | 651 | 439 |
| Max Cabin Seats | 16 | 9 | 19 | 19 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 6675 | 7540 | — | 7417 |
| Standard Cabin Seats | 16 | 8 | 19 | 19 |
| Flight Deck (Base Spec) | Garmin G5000H | Rockwell Collins Pro Line 21 | EFIS | EFIS |
| Max Cruise Speed (ktas) | 160 | 430 | 155 | 155 |
| Base Aircraft Price (USD) | $15,000,000 | $15,500,000 | $2,413,000 | $30,650,000 |
| DOC / nm | — | $ 5.34 | $ 15.57 | $ 19.79 |
| DOC / nm / Seat | — | $ 0.67 | $ 0.74 | $ 0.94 |
| Direct Operating Cost | — | $ 2,303 | $ 2,413 | $ 3,068 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 2 |
| Total Seats | 18 | 10 | 21 | 21 |
| Max Cabin Seats | 16 | 9 | 19 | 19 |
| Standard Cabin Seats | 16 | 8 | 19 | 19 |
| Lavatory | — | 1 Enclosed Belted Flushing | — | — |
| Crew Rest | — | No | — | — |
| Jump Seat | — | No | — | — |
| Galley Location | — | FWD | — | — |
| Lavatory Location | — | AFT | — | — |
| Cabin Pressure (psi) | — | 9.3 | — | — |
| Galley / Refreshment | — | Galley | — | — |
| SL Cabin Altitude (ft) | — | 25230 | — | — |
| Engine | ||||
| FADEC | Dual-Channel | Yes | Yes | Yes |
| Model | CT7-2F1 | PW545C | CT7-2E1 | CT7-8A |
| Fuel Type | JetFuel | — | JetFuel | JetFuel |
| TBO (hrs) | 4000 | 5000 | 4000 | 4000 |
| Horsepower | 1800 | — | 1983 | 2520 |
| No. of Engines | 2 | 2 | 2 | 1 |
| Fuel Capacity (gal) | 641 | — | — | 760 |
| Flat Rating | — | ISA + 10 | — | — |
| Thrust (lbs) | — | 4119 | — | — |
| Dimensions | ||||
| Width (ft) | 25.77 | — | — | — |
| Length (ft) | 61.58 | 52.5 | 57.8 | — |
| Cabin Width (ft) | 7.58 | 5.5 | — | — |
| Cabin Height (ft) | 4.5 | 5.7 | — | — |
| Cabin Length (ft) | 15.5 | 18.5 | — | — |
| Overall Height (ft) | 18.18 | 17.2 | 16.6 | 17.8 |
| Rotor Diameter (ft) | 54.5 | — | 48 | — |
| Baggage Volume Ext. (cu. ft) | 128 | 80 | 85 | 140 |
| Wingspan (ft) | — | 56.3 | — | — |
| 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) | — | — | 395 | 775 |