Maule Aircraft M 9 235i vs Diamond Aircraft Da40 Xlt vs Tecnam P2010 P
Commercial aircraft are commonly compared by category, typical range, and passenger capacity. Regional aircraft cover short routes and prioritize frequency over distance; turboprops and small regional jets usually fly roughly 200–1,500 nautical miles and carry about 30–100 passengers. Narrow-body airliners serve most domestic and short-to-medium international markets, balancing efficiency with flexibility; they typically range about 1,500–3,500 nautical miles and seat roughly 120–240 passengers depending on layout. Wide-body aircraft are built for high-demand long-haul flying, offering more cabin volume and cargo capacity; they often operate about 3,500–8,000+ nautical miles and carry around 250–400+ passengers. Very large wide-bodies, used on dense hub-to-hub routes, can push capacity higher, sometimes 450–600+ seats, though they are less common because they require consistently high demand and suitable airport infrastructure. In general, as you move from regional to narrow-body to wide-body categories, passenger capacity and range increase, while operating economics shift from frequency and airport access to unit cost per seat and long-range efficiency.
| Spec | Diamond Aircraft DA40 XLT | Maule Aircraft M-9 235i | Tecnam P2010 P |
|---|---|---|---|
| Summary | |||
| DOC / nm | $ 0.88 | — | — |
| Total Seats | 4 | 4 | 4 |
| Flight Rules | VFR | VFR | VFR |
| Manufacturer | Diamond Aircraft | Maule Aircraft | Tecnam |
| Aircraft Name | DA40 XLT | M-9 235i | P2010 P |
| Certification | FAA / EASA | FAA | EASA |
| Max Range (nm) | 790 | 876 | 600 |
| DOC / nm / Seat | $ 0.22 | — | — |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 900 | 1100 | 925 |
| Direct Operating Cost | $ 125 | — | — |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Garmin G5 | Gyro / Analog |
| Max Cruise Speed (ktas) | 142 | 137 | 137 |
| Base Aircraft Price (USD) | $485,000 | $355,000 | $430,360 |
| Cabin | |||
| Total Seats | 4 | 4 | 4 |
| Engine | |||
| FADEC | No | No | No |
| Model | IO-360 M1A | I0-540-W1A5 | IO 360 M1A |
| Fuel Type | AvGas | AvGas | AvGas / MoGas |
| TBO (hrs) | 2000 | 2000 | 2000 |
| TBO (yrs) | 12 | 12 | 12 |
| Horsepower | 180 | 235 | 180 |
| Fuel Delivery | Fuel Injected | Fuel Injected | Fuel Injected |
| No. of Engines | 1 | 1 | 1 |
| Usable Fuel (gal) | 48 | — | — |
| Fuel Capacity (gal) | 50 | 85 | 63.4 |
| Fuel Burn (gph) | — | — | 10.3 |
| Dimensions | |||
| Length (ft) | 26.5 | 23.7 | 26.15 |
| Wingspan (ft) | 38.2 | 33 | 33.8 |
| Overall Height (ft) | 6.5 | 6.4 | 8.7 |
| Baggage Volume Int. (cu. ft) | — | 42 | — |
| Cabin Width (ft) | — | — | 3.74 |
| Cabin Height (ft) | — | — | 3 |