Bell 525 Relentless vs Cessna Citation Xls vs Gulfstream G700
The Bell 525 Relentless is a twin‑engine civil helicopter aimed at offshore, corporate, and utility missions. Compared with the jets, it operates at much lower speed and altitude but can land in tight or unimproved areas and offer point‑to‑point access without runways. Its typical passenger capacity is around 16 (depending on configuration), and its range is roughly in the 500–600 nautical mile class. The Cessna Citation XLS+ is a super‑midsize business jet designed for short to medium trips with strong runway flexibility. It generally seats about 8–9 passengers in a standard corporate layout (more in high‑density), with a range around 2,000–2,100 nautical miles, making it suitable for many regional and some transcontinental missions. The Gulfstream G700 is an ultra‑long‑range, large‑cabin business jet focused on intercontinental travel and maximum cabin space. It typically accommodates about 13–19 passengers (and can be configured higher), with range on the order of 7,500 nautical miles, enabling many nonstop long‑haul city pairs.
| Spec | Bell 525 Relentless | Cessna Citation XLS+ | Gulfstream G700 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 3 |
| Min Crew | 2 | 2 | 4 |
| Total Seats | 18 | 10 | 16 |
| Flight Rules | IFR | — | — |
| Manufacturer | Bell | Cessna Citation | Gulfstream |
| Aircraft Name | 525 Relentless | XLS+ | G700 |
| Certification | FAA / EASA | FAA / EASA | In Development |
| Max Range (nm) | 580 | 1906 | 7500 |
| Max Cabin Seats | 16 | 9 | 19 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 6675 | 7540 | — |
| Standard Cabin Seats | 16 | 8 | 12 |
| Flight Deck (Base Spec) | Garmin G5000H | Rockwell Collins Pro Line 21 | Gulfstream Symmetry Flight Deck |
| Max Cruise Speed (ktas) | 160 | 430 | 516 |
| Base Aircraft Price (USD) | $15,000,000 | $15,500,000 | $78,000,000 |
| DOC / nm | — | $ 5.34 | — |
| DOC / nm / Seat | — | $ 0.67 | — |
| Direct Operating Cost | — | $ 2,303 | — |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 4 |
| Total Seats | 18 | 10 | 16 |
| Max Cabin Seats | 16 | 9 | 19 |
| Standard Cabin Seats | 16 | 8 | 12 |
| Lavatory | — | 1 Enclosed Belted Flushing | — |
| Crew Rest | — | No | Optional |
| Jump Seat | — | No | Yes |
| Galley Location | — | FWD | FWD |
| Lavatory Location | — | AFT | FWD / AFT |
| Cabin Pressure (psi) | — | 9.3 | — |
| Galley / Refreshment | — | Galley | — |
| SL Cabin Altitude (ft) | — | 25230 | — |
| Engine | |||
| FADEC | Dual-Channel | Yes | — |
| Model | CT7-2F1 | PW545C | Pearl 700 |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 4000 | 5000 | On Condition |
| Horsepower | 1800 | — | — |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 641 | — | — |
| Flat Rating | — | ISA + 10 | — |
| Thrust (lbs) | — | 4119 | 18250 |
| Dimensions | |||
| Width (ft) | 25.77 | — | — |
| Length (ft) | 61.58 | 52.5 | 109.9 |
| Cabin Width (ft) | 7.58 | 5.5 | 8.2 |
| Cabin Height (ft) | 4.5 | 5.7 | 6.25 |
| Cabin Length (ft) | 15.5 | 18.5 | 56.9 |
| Overall Height (ft) | 18.18 | 17.2 | 25.4 |
| Rotor Diameter (ft) | 54.5 | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | 80 | — |
| Wingspan (ft) | — | 56.3 | 103 |
| Aisle Step (ft) | — | 0.7 | Flat Floor |
| Cabin Width - Floor (ft) | — | 3.9 | — |
| Cabin Length - Seating (ft) | — | 14.3 | — |
| Baggage Volume Int. (cu. ft) | — | 10 | 195 |