Bell 525 Relentless vs Cessna Citation Xls vs Daher Tbm 960 vs Md Helicopters (mcdonnell Douglas) 902 Explorer
The Bell 525 Relentless and the MD Helicopters (McDonnell Douglas) 902 Explorer are both rotorcraft, best suited to point-to-point access into constrained sites, but they trade range and cruise efficiency for vertical lift. The Bell 525 is a larger, longer-range helicopter, typically offering roughly 500–600 nm class range with seating commonly arranged for about 12–16 passengers depending on cabin fit. The MD 902 is a lighter utility helicopter, usually configured around 6–8 passengers, with a shorter range commonly in the ~300–400 nm class. The Cessna Citation XLS+ is a twin‑engine business jet optimized for fast city‑pair travel between airports, with a typical range around 2,000 nm and seating commonly 7–9 passengers in executive layout (up to about 12 in higher-density configurations). The Daher TBM 960 is a single‑engine turboprop business aircraft aimed at efficient owner-operator travel; it generally carries about 4–6 passengers plus pilot (up to 6 seats), with range often around 1,400–1,700 nm depending on reserves and speed settings.
| Spec | Bell 525 Relentless | Cessna Citation XLS+ | Daher TBM 960 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 18 | 10 | 6 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Bell | Cessna Citation | Daher TBM |
| Aircraft Name | 525 Relentless | XLS+ | TBM 960 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 1906 | 1730 |
| Max Cabin Seats | 16 | 9 | — |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 6675 | 7540 | 2908 |
| Standard Cabin Seats | 16 | 8 | 4 |
| Flight Deck (Base Spec) | Garmin G5000H | Rockwell Collins Pro Line 21 | Garmin G3000 |
| Max Cruise Speed (ktas) | 160 | 430 | 330 |
| Base Aircraft Price (USD) | $15,000,000 | $15,500,000 | $4,450,000 |
| DOC / nm | — | $ 5.34 | $ 2.25 |
| DOC / nm / Seat | — | $ 0.67 | $ 0.56 |
| Direct Operating Cost | — | $ 2,303 | $ 744 |
| Aircraft Type | — | — | Turbo Prop |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 18 | 10 | 6 |
| Max Cabin Seats | 16 | 9 | — |
| Standard Cabin Seats | 16 | 8 | 4 |
| Lavatory | — | 1 Enclosed Belted Flushing | No |
| Crew Rest | — | No | — |
| Jump Seat | — | No | — |
| Galley Location | — | FWD | MID |
| Lavatory Location | — | AFT | — |
| Cabin Pressure (psi) | — | 9.3 | 6.2 |
| Galley / Refreshment | — | Galley | — |
| SL Cabin Altitude (ft) | — | 25230 | 14390 |
| Engine | |||
| FADEC | Dual-Channel | Yes | Yes |
| Model | CT7-2F1 | PW545C | TBM 960 |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 4000 | 5000 | 3500 |
| Horsepower | 1800 | — | 850 |
| No. of Engines | 2 | 2 | — |
| Fuel Capacity (gal) | 641 | — | — |
| Flat Rating | — | ISA + 10 | ISA + 49 |
| Thrust (lbs) | — | 4119 | — |
| Dimensions | |||
| Width (ft) | 25.77 | — | — |
| Length (ft) | 61.58 | 52.5 | 35.3 |
| Cabin Width (ft) | 7.58 | 5.5 | 4 |
| Cabin Height (ft) | 4.5 | 5.7 | 4.1 |
| Cabin Length (ft) | 15.5 | 18.5 | 13.4 |
| Overall Height (ft) | 18.18 | 17.2 | — |
| Rotor Diameter (ft) | 54.5 | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | 80 | — |
| Wingspan (ft) | — | 56.3 | 42.1 |
| Aisle Step (ft) | — | 0.7 | — |
| Cabin Width - Floor (ft) | — | 3.9 | — |
| Cabin Length - Seating (ft) | — | 14.3 | — |
| Baggage Volume Int. (cu. ft) | — | 10 | — |
| Cabin Volume (cu. ft) | — | — | 123 |