Bell 407gxi vs Leonardo Aw169 vs Leonardo Aw189
The Bell 407GXi is a light single‑engine helicopter, best suited to shorter regional missions and operations where low operating cost and simple logistics matter most. Its typical range is in the few‑hundred‑nautical‑mile class (often around the mid‑300 nm range depending on configuration), and passenger capacity is generally about five to six passengers plus one or two pilots, depending on seating and mission fit. The Leonardo AW169 sits in the light‑to‑intermediate twin‑engine category, offering more redundancy, cabin volume, and payload than the 407GXi while remaining compact for rooftop and confined-area work. Its range is broadly similar to or somewhat higher than the Bell in many layouts (commonly around the mid‑300 to 400+ nm bracket), with typical passenger seating around six to eight, and higher-density layouts possible. The Leonardo AW189 is a larger, super‑medium twin‑engine helicopter aimed at longer, heavier missions such as offshore transport and SAR. It generally offers the longest range of the three (often roughly 450–500+ nm with appropriate tanks and reserves) and the highest passenger capacity, commonly around 16–19 passengers in transport configurations.
| Spec | Bell 407GXi | AGUSTA / LEONARDO AW169 | AGUSTA / LEONARDO AW189 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 4.43 | $ 11.84 | $ 15.57 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 6 | 12 | 21 |
| Flight Rules | VFR | IFR | IFR |
| Manufacturer | Bell | Leonardo | Leonardo |
| Aircraft Name | 407GXi | AW169 | AW189 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 337 | 440 | 651 |
| DOC / nm / Seat | $ 0.74 | $ 0.99 | $ 0.74 |
| Max Cabin Seats | 5 | 10 | 19 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2300 | — | — |
| Standard Cabin Seats | 5 | 10 | 19 |
| Direct Operating Cost | $ 589 | $ 1,658 | $ 2,413 |
| Flight Deck (Base Spec) | Garmin G1000H NXI | EFIS | EFIS |
| Max Cruise Speed (ktas) | 133 | 140 | 155 |
| Base Aircraft Price (USD) | $3,225,000 | $9,450,000 | $2,413,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 6 | 12 | 21 |
| Max Cabin Seats | 5 | 10 | 19 |
| Standard Cabin Seats | 5 | 10 | 19 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | M250-C47E/4 | PW210A | CT7-2E1 |
| Fuel Type | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 3500 | 4000 | 4000 |
| Horsepower | 862 | 1000 | 1983 |
| No. of Engines | 1 | 2 | 2 |
| Fuel Burn (gph) | 46 | — | — |
| Fuel Capacity (gal) | 127.8 | — | — |
| Dimensions | |||
| Width (ft) | 25.4 | — | — |
| Length (ft) | 41.4 | 48.1 | 57.8 |
| Cabin Width (ft) | 5 | — | — |
| Cabin Height (ft) | 3.9 | — | — |
| Overall Height (ft) | 10.2 | 14.8 | 16.6 |
| Rotor Diameter (ft) | 35 | — | 48 |
| Cabin Volume (cu. ft) | 125 | 222.5 | 395 |
| Baggage Volume Ext. (cu. ft) | 16 | 49.5 | 85 |