Embraer Phenom 100ev vs Piper Seneca
The Embraer Phenom 100EV and the Piper Seneca sit in different aircraft categories and are used for different missions. The Phenom 100EV is a very light jet, optimized for fast, high-altitude business travel with jet performance and a pressurized cabin designed around premium comfort. The Piper Seneca is a piston-powered light twin, commonly used for personal travel, training, and utility missions, offering twin-engine redundancy but at lower speeds and altitudes than a jet. In range, the Phenom 100EV generally provides a longer, more efficient point-to-point capability for typical business trip profiles, roughly around 1,100–1,200 nautical miles depending on configuration and conditions. A Seneca’s range is typically shorter, commonly in the ballpark of about 700–900 nautical miles, again depending on model, payload, and power settings. For passenger capacity, both can often be configured to carry about four to six people, but the Phenom 100EV usually markets a 4–6 passenger cabin plus one or two pilots, while the Seneca is often arranged for up to six seats including the pilot, with less cabin volume and amenities than the jet.
| Spec | Embraer Phenom 100EV | Piper Seneca |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 2.84 | $ 1.69 |
| Min Crew | 1 | — |
| Total Seats | 7 | 6 |
| Manufacturer | Embraer | Piper |
| Aircraft Name | Phenom 100EV | Seneca |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1,178 | 828 |
| DOC / nm / Seat | $ 0.71 | $ 0.28 |
| Max Cabin Seats | 7 | — |
| OEM Verification | VERIFIED | Un-Verified |
| Useful Load (lbs) | 3451 | 1331 |
| Standard Cabin Seats | 5 | 4 |
| Direct Operating Cost | $ 1,152 | $ 337 |
| Flight Deck (Base Spec) | Prodigy Touch (G3000) | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 406 | 200 |
| Base Aircraft Price (USD) | $4,250,000 | $1,095,000 |
| Flight Rules | — | IFR |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | 1 Flushing | — |
| Min Crew | 1 | — |
| Crew Rest | No | — |
| Jump Seat | No | — |
| Total Seats | 6 | 6 |
| Max Cabin Seats | 6 | — |
| Lavatory Location | AFT | — |
| Cabin Pressure (psi) | 8.3 | — |
| Galley / Refreshment | No | — |
| Standard Cabin Seats | 4 | 4 |
| SL Cabin Altitude (ft) | 21280 | — |
| Engine | ||
| FADEC | Yes | No |
| Model | PW617F1-E | TSIO-360-RB |
| TBO (hrs) | 3500 | 1800 |
| Flat Rating | ISA + 8 | — |
| Thrust (lbs) | 1730 | — |
| No. of Engines | 2 | 2 |
| Fuel Burn (lbph) | 543 | — |
| Fuel Type | — | AvGas |
| Horsepower | — | 220 |
| Fuel Delivery | — | Fuel Injected |
| Fuel Capacity (gal) | — | 122 |
| Dimensions | ||
| Length (ft) | 42.1 | 28.6 |
| Wingspan (ft) | 40.4 | 39 |
| Aisle Step (ft) | 0.3 | — |
| Cabin Width (ft) | 5.1 | — |
| Cabin Height (ft) | 4.9 | — |
| Cabin Length (ft) | 11 | — |
| Overall Height (ft) | 14.3 | 10 |
| Cabin Width - Floor (ft) | 3.6 | — |
| Cabin Length - Seating (ft) | 9 | — |
| Baggage Volume Ext. (cu. ft) | 60 | — |
| Baggage Volume Int. (cu. ft) | 10 | — |