Airbus Helicopters H225 vs Bell 525 Relentless vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Pilatus Pc 24
The Airbus H225, Bell 525 Relentless, and MD Helicopters 902 Explorer are all rotorcraft, typically used for offshore transport, utility, and VIP missions, while the Pilatus PC-24 is a fixed‑wing light jet aimed at fast business and mixed passenger/cargo operations. In category terms, the H225 is a heavy twin‑engine helicopter, the Bell 525 is a super‑medium twin, and the MD 902 is a light twin (with a NOTAR anti‑torque system), whereas the PC‑24 is a twin‑engine jet. For range, the PC‑24 generally offers the longest legs (on the order of roughly 2,000 nautical miles), the H225 and Bell 525 are mid‑range helicopters (commonly around the 500–600+ nautical mile class depending on fit and reserves), and the MD 902 is shorter‑range (often roughly 300–400 nautical miles). Passenger capacity typically scales similarly: the H225 can carry the most (often up to about 19 passengers in high‑density layouts), the Bell 525 is next (commonly up to around 16–20 depending on configuration), the MD 902 is smaller (typically 7–8), and the PC‑24 usually seats about 8–10 passengers in executive layouts.
| Spec | AIRBUS H225 | Bell 525 Relentless | Pilatus PC-24 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | — | $ 3.71 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 21 | 18 | 6 |
| Flight Rules | IFR | IFR | — |
| Manufacturer | Airbus Helicopters | Bell | Pilatus |
| Aircraft Name | H225 | 525 Relentless | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 580 | 2076 |
| DOC / nm / Seat | $ 0.99 | — | $ 0.62 |
| Max Cabin Seats | 28 | 16 | 10 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 6675 | 6680 |
| Standard Cabin Seats | 19 | 16 | 6 |
| Direct Operating Cost | $ 2,963 | — | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Garmin G5000H | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 160 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,000,000 | $11,800,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 21 | 18 | 6 |
| Max Cabin Seats | 28 | 16 | 10 |
| Standard Cabin Seats | 19 | 16 | 6 |
| Lavatory | — | — | 1 Enclosed Flushing |
| Crew Rest | — | — | No |
| Jump Seat | — | — | No |
| Cargo Door | — | — | Yes |
| Galley Location | — | — | FWD |
| Lavatory Location | — | — | FWD |
| Cabin Pressure (psi) | — | — | 9.3 |
| Galley / Refreshment | — | — | Optional Refreshment Center |
| SL Cabin Altitude (ft) | — | — | 23500 |
| Engine | |||
| FADEC | Yes | Dual-Channel | Yes |
| Model | Makila 2A1 | CT7-2F1 | FJ44-4A-QPM |
| Fuel Type | JetFuel | JetFuel | — |
| TBO (hrs) | 3500 | 4000 | 5000 |
| Horsepower | 2100 | 1800 | — |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | 641 | — |
| Flat Rating | — | — | ISA + 23 |
| Thrust (lbs) | — | — | 3435 |
| Dimensions | |||
| Length (ft) | 63.4 | 61.58 | 52.2 |
| Overall Height (ft) | 16.3 | 18.18 | 17.4 |
| Rotor Diameter (ft) | 53.2 | 54.5 | — |
| Cabin Volume (cu. ft) | 547 | — | — |
| Width (ft) | — | 25.77 | — |
| Cabin Width (ft) | — | 7.58 | 5.6 |
| Cabin Height (ft) | — | 4.5 | 5.1 |
| Cabin Length (ft) | — | 15.5 | 23 |
| Baggage Volume Ext. (cu. ft) | — | 128 | — |
| Wingspan (ft) | — | — | 55.8 |
| Aisle Step (ft) | — | — | Flat Floor |
| Cabin Width - Floor (ft) | — | — | 3.8 |
| Cabin Length - Seating (ft) | — | — | 17 |
| Baggage Volume Int. (cu. ft) | — | — | 90 |