Bell 525 Relentless vs Boeing Bbj Max 9 vs Cessna Citation Xls vs Piper M600 Sls
The Bell 525 Relentless is a fly-by-wire, twin‑engine helicopter aimed at offshore and corporate transport. It typically carries about 16 passengers in an airliner-style configuration (fewer in VIP layouts) and offers roughly a 500–600 nautical mile class range, trading speed and cabin size for vertical lift and point-to-point access. The Boeing BBJ MAX 9 is a long‑range VIP airliner in the large-cabin “bizliner” category. It can be configured for a few dozen passengers in executive comfort (often around 25–50) and, in airline service, seats far more. Its range is in the roughly 3,200–3,500 nautical mile class, making it the clear leader for capacity and long-haul missions. The Cessna Citation XLS+ is a midsize business jet, typically seating about 8–12 passengers with a range around 2,000–2,100 nautical miles, balancing efficiency, runway flexibility, and comfort. The Piper M600 SLS is a single‑engine turboprop in the personal/light business category, generally carrying 4–6 passengers with about 1,400–1,500 nautical miles of range, prioritizing simplicity and operating cost over cabin size and speed.
| Spec | Bell 525 Relentless | Boeing BBJ MAX 9 | Cessna Citation XLS+ | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 2 | 1 |
| Total Seats | 18 | 12 | 10 | 6 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Bell | Boeing | Cessna Citation | Piper |
| Aircraft Name | 525 Relentless | BBJ MAX 9 | XLS+ | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 6376 | 1906 | 1406 |
| Max Cabin Seats | 16 | 35 | 9 | — |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 6675 | 77120 | 7540 | 2200 |
| Standard Cabin Seats | 16 | 8 | 8 | 4 |
| Flight Deck (Base Spec) | Garmin G5000H | Honeywell | Rockwell Collins Pro Line 21 | Garmin G3000 |
| Max Cruise Speed (ktas) | 160 | 470 | 430 | 274 |
| Base Aircraft Price (USD) | $15,000,000 | $107,700,000 | $15,500,000 | $3,081,400 |
| DOC / nm | — | $ 15.74 | $ 5.34 | $ 2.19 |
| DOC / nm / Seat | — | $ 1.97 | $ 0.67 | $ 0.55 |
| Direct Operating Cost | — | $ 7,396 | $ 2,303 | $ 603 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 2 | 1 |
| Total Seats | 18 | 10 | 10 | 5 |
| Max Cabin Seats | 16 | 35 | 9 | — |
| Standard Cabin Seats | 16 | 8 | 8 | 4 |
| Configuration | — | Green Interior | — | — |
| Cabin Pressure (psi) | — | 9 | 9.3 | 5.6 |
| SL Cabin Altitude (ft) | — | 24000 | 25230 | 12600 |
| Lavatory | — | — | 1 Enclosed Belted Flushing | No |
| Crew Rest | — | — | No | — |
| Jump Seat | — | — | No | — |
| Galley Location | — | — | FWD | MID |
| Lavatory Location | — | — | AFT | — |
| Galley / Refreshment | — | — | Galley | Refreshment Centre |
| Max Cabin Altitude (ft) | — | — | — | 8644 |
| Engine | ||||
| FADEC | Dual-Channel | Yes | Yes | No |
| Model | CT7-2F1 | LEAP-1B | PW545C | PT6A-42A |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 4000 | On-Condition | 5000 | 3600 |
| Horsepower | 1800 | — | — | 600 |
| No. of Engines | 2 | 2 | 2 | 1 |
| Fuel Capacity (gal) | 641 | — | — | 260 |
| Flat Rating | — | ISA + 15 | ISA + 10 | ISA + 55 |
| Thrust (lbs) | — | 28000 | 4119 | — |
| Dimensions | ||||
| Width (ft) | 25.77 | — | — | — |
| Length (ft) | 61.58 | 138.4 | 52.5 | 29.7 |
| Cabin Width (ft) | 7.58 | 11.6 | 5.5 | 4.1 |
| Cabin Height (ft) | 4.5 | 7.1 | 5.7 | 4 |
| Cabin Length (ft) | 15.5 | 107.2 | 18.5 | 12.3 |
| Overall Height (ft) | 18.18 | 40.3 | 17.2 | 11.3 |
| Rotor Diameter (ft) | 54.5 | — | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | 1485 | 80 | — |
| Wingspan (ft) | — | 117.9 | 56.3 | 43.2 |
| Aisle Step (ft) | — | Flat Floor | 0.7 | — |
| Cabin Width - Floor (ft) | — | 10.7 | 3.9 | — |
| Cabin Length - Seating (ft) | — | 100.6 | 14.3 | — |
| Baggage Volume Int. (cu. ft) | — | — | 10 | 20 |
| Cabin Volume (cu. ft) | — | — | — | 165 |