Daher Tbm 960 vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Piaggio Avanti Evo vs Piper M600 Sls
The Daher TBM 960 and Piper M600 SLS are single‑engine turboprop airplanes in the high‑performance personal/corporate category. Both typically seat a pilot plus five passengers (up to six seats total). Range is broadly similar, with the TBM 960 generally around 1,400–1,700 nm depending on power settings and reserves, and the M600 SLS commonly around 1,400–1,600 nm. The Piaggio Avanti EVO is a twin‑turboprop business aircraft in a higher cabin‑class than the TBM/M600, usually configured for seven to nine passengers (plus crew). Its range is typically in the roughly 1,400–1,700 nm class, varying with load and speed. The MD Helicopters (McDonnell Douglas) 902 Explorer is a twin‑engine light helicopter oriented to utility, law enforcement, EMS, and corporate shuttle roles. Passenger capacity is typically about five to six plus a pilot (configuration dependent). Its range is much shorter than the fixed‑wing turboprops, commonly on the order of roughly 300–400 nm, reflecting rotorcraft efficiency and mission profiles.
| Spec | Daher TBM 960 | Piaggio Avanti EVO | Piper M600 SLS |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 2.25 | — | $ 2.19 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 6 | 8 | 6 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Daher TBM | Piaggio | Piper |
| Aircraft Name | TBM 960 | Avanti EVO | M600 |
| Aircraft Type | Turbo Prop | — | — |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1730 | 1530 | 1406 |
| DOC / nm / Seat | $ 0.56 | — | $ 0.55 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 2908 | 3775 | 2200 |
| Standard Cabin Seats | 4 | 6 | 4 |
| Direct Operating Cost | $ 744 | — | $ 603 |
| Flight Deck (Base Spec) | Garmin G3000 | Rockwell Collins Pro Line 21 | Garmin G3000 |
| Max Cruise Speed (ktas) | 330 | 400 | 274 |
| Base Aircraft Price (USD) | $4,450,000 | $ 7,695,000 | $3,081,400 |
| Max Cabin Seats | — | 7 | — |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Lavatory | No | No | No |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 6 | 8 | 5 |
| Galley Location | MID | — | MID |
| Cabin Pressure (psi) | 6.2 | 9 | 5.6 |
| Standard Cabin Seats | 4 | 6 | 4 |
| SL Cabin Altitude (ft) | 14390 | 24000 | 12600 |
| Max Cabin Seats | — | 7 | — |
| Galley / Refreshment | — | No | Refreshment Centre |
| Max Cabin Altitude (ft) | — | 6600 | 8644 |
| Engine | |||
| FADEC | Yes | Yes | No |
| Model | TBM 960 | PT6A–66B | PT6A-42A |
| TBO (hrs) | 3500 | 3600 | 3600 |
| Horsepower | 850 | 850 | 600 |
| Flat Rating | ISA + 49 | ISA + 28 | ISA + 55 |
| No. of Engines | — | 2 | 1 |
| Fuel Burn (gph) | — | 100 | — |
| Fuel Capacity (gal) | — | — | 260 |
| Dimensions | |||
| Length (ft) | 35.3 | 47.3 | 29.7 |
| Wingspan (ft) | 42.1 | 47.1 | 43.2 |
| Cabin Width (ft) | 4 | 6.1 | 4.1 |
| Cabin Height (ft) | 4.1 | 5.8 | 4 |
| Cabin Length (ft) | 13.4 | 14.9 | 12.3 |
| Cabin Volume (cu. ft) | 123 | — | 165 |
| Overall Height (ft) | — | 13.1 | 11.3 |
| Cabin Width - Floor (ft) | — | 3.5 | — |
| Baggage Volume Int. (cu. ft) | — | 35.2 | 20 |