Bell 525 Relentless vs Cessna Citation Xls vs Md Helicopters (mcdonnell Douglas) 902 Explorer
The Bell 525 Relentless is a fly-by-wire, super‑medium helicopter aimed at fast point-to-point regional travel with vertical takeoff and landing. It typically carries around 16 passengers in an executive configuration (with layouts varying by operator) and has an approximate range on the order of 500–600 nautical miles. The Cessna Citation XLS+ is a super‑light business jet designed for higher cruise speeds and longer nonstop legs between airports. It commonly seats about 7–9 passengers in a business layout and offers roughly 1,800–2,100 nautical miles of range, depending on payload, reserves, and conditions. The MD Helicopters (McDonnell Douglas) 902 Explorer is a light twin helicopter optimized for utility, law enforcement, EMS, and corporate shuttle missions. It generally accommodates about 8–10 passengers (or fewer with mission equipment) and has a shorter typical range, roughly 250–350 nautical miles. Overall, the XLS+ leads on range and speed but needs runways, while the Bell 525 carries more people farther than the MD 902 and benefits from helicopter access to tight landing sites.
| Spec | Bell 525 Relentless | Cessna Citation XLS+ |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 2 |
| Total Seats | 18 | 10 |
| Flight Rules | IFR | — |
| Manufacturer | Bell | Cessna Citation |
| Aircraft Name | 525 Relentless | XLS+ |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 1906 |
| Max Cabin Seats | 16 | 9 |
| OEM Verification | VERIFIED | VERIFIED |
| Useful Load (lbs) | 6675 | 7540 |
| Standard Cabin Seats | 16 | 8 |
| Flight Deck (Base Spec) | Garmin G5000H | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 160 | 430 |
| Base Aircraft Price (USD) | $15,000,000 | $15,500,000 |
| DOC / nm | — | $ 5.34 |
| DOC / nm / Seat | — | $ 0.67 |
| Direct Operating Cost | — | $ 2,303 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 2 |
| Total Seats | 18 | 10 |
| Max Cabin Seats | 16 | 9 |
| Standard Cabin Seats | 16 | 8 |
| 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 |
| Model | CT7-2F1 | PW545C |
| Fuel Type | JetFuel | — |
| TBO (hrs) | 4000 | 5000 |
| Horsepower | 1800 | — |
| No. of Engines | 2 | 2 |
| Fuel Capacity (gal) | 641 | — |
| Flat Rating | — | ISA + 10 |
| Thrust (lbs) | — | 4119 |
| Dimensions | ||
| Width (ft) | 25.77 | — |
| Length (ft) | 61.58 | 52.5 |
| 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 |
| Rotor Diameter (ft) | 54.5 | — |
| Baggage Volume Ext. (cu. ft) | 128 | 80 |
| 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 |