Bell 525 Relentless vs Boeing Bbj Max 9 vs Cessna Citation Xls vs Gulfstream G700
The Bell 525 Relentless is a fly-by-wire helicopter best suited to short-to-medium missions where vertical access matters more than nonstop distance. Its typical range is roughly 500–600 nautical miles, and it generally carries about 12–16 passengers depending on interior and payload choices. The Cessna Citation XLS+ is a midsize business jet aimed at efficient regional travel. It commonly offers around 1,800–2,100 nautical miles of range and typically seats about 7–9 passengers in an executive layout. The Boeing BBJ MAX 9 is a VIP airliner based on a narrowbody transport, optimized for long-range, high-comfort group travel. It can reach roughly 6,000–6,600 nautical miles with auxiliary tanks, and cabin configurations vary widely, often accommodating a few dozen passengers, with maximum VIP-style layouts commonly in the tens rather than hundreds. The Gulfstream G700 is an ultra-long-range purpose-built business jet, offering about 7,500 nautical miles of range and typically seating around 13–19 passengers, emphasizing speed, cabin volume, and nonstop intercontinental capability.
| Spec | Bell 525 Relentless | Boeing BBJ MAX 9 | Cessna Citation XLS+ | Gulfstream G700 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 3 |
| Min Crew | 2 | 4 | 2 | 4 |
| Total Seats | 18 | 12 | 10 | 16 |
| Flight Rules | IFR | — | — | — |
| Manufacturer | Bell | Boeing | Cessna Citation | Gulfstream |
| Aircraft Name | 525 Relentless | BBJ MAX 9 | XLS+ | G700 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | In Development |
| Max Range (nm) | 580 | 6376 | 1906 | 7500 |
| Max Cabin Seats | 16 | 35 | 9 | 19 |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 6675 | 77120 | 7540 | — |
| Standard Cabin Seats | 16 | 8 | 8 | 12 |
| Flight Deck (Base Spec) | Garmin G5000H | Honeywell | Rockwell Collins Pro Line 21 | Gulfstream Symmetry Flight Deck |
| Max Cruise Speed (ktas) | 160 | 470 | 430 | 516 |
| Base Aircraft Price (USD) | $15,000,000 | $107,700,000 | $15,500,000 | $78,000,000 |
| DOC / nm | — | $ 15.74 | $ 5.34 | — |
| DOC / nm / Seat | — | $ 1.97 | $ 0.67 | — |
| Direct Operating Cost | — | $ 7,396 | $ 2,303 | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 2 | 4 |
| Total Seats | 18 | 10 | 10 | 16 |
| Max Cabin Seats | 16 | 35 | 9 | 19 |
| Standard Cabin Seats | 16 | 8 | 8 | 12 |
| Configuration | — | Green Interior | — | — |
| Cabin Pressure (psi) | — | 9 | 9.3 | — |
| SL Cabin Altitude (ft) | — | 24000 | 25230 | — |
| Lavatory | — | — | 1 Enclosed Belted Flushing | — |
| Crew Rest | — | — | No | Optional |
| Jump Seat | — | — | No | Yes |
| Galley Location | — | — | FWD | FWD |
| Lavatory Location | — | — | AFT | FWD / AFT |
| Galley / Refreshment | — | — | Galley | — |
| Engine | ||||
| FADEC | Dual-Channel | Yes | Yes | — |
| Model | CT7-2F1 | LEAP-1B | PW545C | Pearl 700 |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 4000 | On-Condition | 5000 | On Condition |
| Horsepower | 1800 | — | — | — |
| No. of Engines | 2 | 2 | 2 | 2 |
| Fuel Capacity (gal) | 641 | — | — | — |
| Flat Rating | — | ISA + 15 | ISA + 10 | — |
| Thrust (lbs) | — | 28000 | 4119 | 18250 |
| Dimensions | ||||
| Width (ft) | 25.77 | — | — | — |
| Length (ft) | 61.58 | 138.4 | 52.5 | 109.9 |
| Cabin Width (ft) | 7.58 | 11.6 | 5.5 | 8.2 |
| Cabin Height (ft) | 4.5 | 7.1 | 5.7 | 6.25 |
| Cabin Length (ft) | 15.5 | 107.2 | 18.5 | 56.9 |
| Overall Height (ft) | 18.18 | 40.3 | 17.2 | 25.4 |
| Rotor Diameter (ft) | 54.5 | — | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | 1485 | 80 | — |
| Wingspan (ft) | — | 117.9 | 56.3 | 103 |
| Aisle Step (ft) | — | Flat Floor | 0.7 | Flat Floor |
| Cabin Width - Floor (ft) | — | 10.7 | 3.9 | — |
| Cabin Length - Seating (ft) | — | 100.6 | 14.3 | — |
| Baggage Volume Int. (cu. ft) | — | — | 10 | 195 |