Airbus Helicopters H135 vs Embraer Phenom 100ev vs Embraer Phenom 300e vs Piper M600 Sls
The Airbus Helicopters H135 is a light twin-engine helicopter, best suited to short to medium missions such as EMS, police, offshore support, and VIP lift. It typically carries about 5–7 passengers (depending on interior and mission fit) and has an effective range on the order of roughly 300–350 nautical miles, varying with payload and reserves. The Embraer Phenom 100EV is a very light jet for short-haul business travel, generally seating 4–7 passengers in typical configurations, with a range around 1,100–1,200 nautical miles. The Embraer Phenom 300E is a light jet with more cabin space and performance, commonly arranged for 6–9 passengers, and offers substantially longer reach at about 1,900–2,000 nautical miles. The Piper M600 SLS is a single-engine turboprop that bridges personal and business use, typically accommodating about 4–6 passengers, with a range around 1,400 nautical miles.
| Spec | AIRBUS H135 | Embraer Phenom 100EV | Embraer Phenom 300E | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 6.33 | $ 2.84 | $ 3.88 | $ 2.19 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 9 | 7 | 10 | 6 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Airbus Helicopters | Embraer | Embraer | Piper |
| Aircraft Name | H135 | Phenom 100EV | Phenom 300E | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 342 | 1,178 | 2,010 | 1406 |
| DOC / nm / Seat | $ 0.79 | $ 0.71 | $ 0.55 | $ 0.55 |
| Max Cabin Seats | 7 | 7 | 10 | — |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 3124 | 3451 | 6914 | 2200 |
| Standard Cabin Seats | 7 | 5 | 6 | 4 |
| Direct Operating Cost | $ 861 | $ 1,152 | $ 1,758 | $ 603 |
| Flight Deck (Base Spec) | Helionix | Prodigy Touch (G3000) | Prodigy Touch (G3000) | Garmin G3000 |
| Max Cruise Speed (ktas) | 136 | 406 | 464 | 274 |
| Base Aircraft Price (USD) | $6,150,000 | $4,250,000 | $9,650,000 | $3,081,400 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 9 | 6 | 9 | 5 |
| Configuration | Green Interior | — | — | — |
| Max Cabin Seats | 7 | 6 | 9 | — |
| Standard Cabin Seats | 7 | 4 | 7 | 4 |
| Lavatory | — | 1 Flushing | 1 Enclosed Flushing | No |
| Crew Rest | — | No | No | — |
| Jump Seat | — | No | No | — |
| Lavatory Location | — | AFT | AFT | — |
| Cabin Pressure (psi) | — | 8.3 | 9.4 | 5.6 |
| Galley / Refreshment | — | No | Galley | Refreshment Centre |
| SL Cabin Altitude (ft) | — | 21280 | 25560 | 12600 |
| Galley Location | — | — | FWD | MID |
| Max Cabin Altitude (ft) | — | — | — | 8644 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | Arrius 2B2+ | PW617F1-E | Canada PW535E1 | PT6A-42A |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 4000 | 3500 | 5000 | 3600 |
| Horsepower | 660 | — | — | 600 |
| No. of Engines | 2 | 2 | 2 | 1 |
| Flat Rating | — | ISA + 8 | ISA + 15 | ISA + 55 |
| Thrust (lbs) | — | 1730 | 3360 | — |
| Fuel Burn (lbph) | — | 543 | 757 | — |
| Fuel Capacity (gal) | — | — | — | 260 |
| Dimensions | ||||
| Length (ft) | 33.5 | 42.1 | 51.2 | 29.7 |
| Overall Height (ft) | 12.6 | 14.3 | 16.75 | 11.3 |
| Rotor Diameter (ft) | 34 | — | — | — |
| Cabin Volume (cu. ft) | 173 | — | — | 165 |
| Wingspan (ft) | — | 40.4 | 52.16 | 43.2 |
| Aisle Step (ft) | — | 0.3 | 0.3 | — |
| Cabin Width (ft) | — | 5.1 | 5.1 | 4.1 |
| Cabin Height (ft) | — | 4.9 | 4.9 | 4 |
| Cabin Length (ft) | — | 11 | 17.2 | 12.3 |
| Cabin Width - Floor (ft) | — | 3.6 | 3.6 | — |
| Cabin Length - Seating (ft) | — | 9 | 14.8 | — |
| Baggage Volume Ext. (cu. ft) | — | 60 | 74 | — |
| Baggage Volume Int. (cu. ft) | — | 10 | 10 | 20 |