Cessna 172 Skyhawk vs Diamond Aircraft Da42 Vi vs Diamond Aircraft Da62 vs Embraer Phenom 100ev vs Pilatus Pc 12 Ngx vs Piper M500 vs Robinson Helicopters R22 Beta Ii
The Cessna Skyhawk is a single‑engine piston, fixed‑gear trainer/light tourer, typically carrying 3–4 people with a range around 600–800 nm. The Diamond DA42 VI is a twin‑engine piston, efficient IFR-capable light aircraft, usually 4–5 seats usable, with roughly 1,000–1,200 nm range. The Diamond DA62 is a larger twin‑engine piston geared to family/business touring, typically 5–7 seats with about 1,000–1,200 nm range. The Embraer Phenom 100EV is a very light jet for short business legs, generally 4–7 passengers (often 4–6 in comfort) and about 1,100–1,200 nm range. The Pilatus PC‑12 NGX is a single‑engine turboprop utility/business aircraft, commonly 6–9 passengers with roughly 1,500–1,800 nm range. The Piper M500 is a single‑engine turboprop pressurized cruiser, typically 5–6 seats and about 1,000–1,300 nm range. The Robinson R22 Beta II is a light two‑seat piston helicopter with short range, commonly around 200–300 nm.
| Spec | Cessna Skyhawk | Diamond Aircraft DA42 VI | Diamond Aircraft DA62 | Embraer Phenom 100EV | Pilatus PC-12 NGX | Piper M500 | ROBINSON R22 Beta II |
|---|---|---|---|---|---|---|---|
| Summary | |||||||
| DOC / nm | $ 0.95 | $ 1.11 | $ 1.18 | $ 2.84 | $ 2.78 | $ 3.11 | $ 1.80 |
| Total Seats | 4 | 4 | 5 | 7 | 8 | 6 | 2 |
| Flight Rules | VFR | IFR | IFR | — | IFR | IFR | VFR |
| Manufacturer | Cessna | Diamond Aircraft | Diamond Aircraft | Embraer | Pilatus | Piper | Robinson Helicopters |
| Aircraft Name | 172 Skyhawk | DA42 VI | DA62 | Phenom 100EV | PC-12 NGX | M500 | R22 Beta II |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 640 | 1273 | 1283 | 1,178 | 1803 | 1000 | 250 |
| DOC / nm / Seat | $ 0.24 | $ 0.28 | $ 0.24 | $ 0.71 | $ 0.46 | $ 0.78 | $ 0.90 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified | VERIFIED | VERIFIED | VERIFIED | Un-Verified |
| Direct Operating Cost | $ 118 | $ 211 | $ 225 | $ 1,152 | $ 793 | $ 579 | $ 173 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Garmin G1000 NXi | Garmin G1000 NXi | Prodigy Touch (G3000) | Honeywell Primus Apex | Garmin G1000 NXi | Gyro / Analog |
| Max Cruise Speed (ktas) | 124 | 190 | 190 | 406 | 290 | 260 | 96 |
| Base Aircraft Price (USD) | $415,000 | $869,000 | $1,290,000 | $4,250,000 | $5,350,000 | $2,122,600 | $ 312,000 |
| Useful Load (lbs) | — | 1298 | 1565 | 3451 | — | 1698 | 490 |
| Cockpit | — | — | 2 | 2 | 2 | 2 | — |
| Max Cabin Seats | — | — | 5 | 7 | 9 | — | — |
| Standard Cabin Seats | — | — | 3 | 5 | 6 | 4 | — |
| Min Crew | — | — | — | 1 | 1 | 1 | — |
| Cabin | |||||||
| Total Seats | 4 | 4 | 5 | 6 | 8 | 5 | 2 |
| Cockpit | — | — | 2 | 2 | 2 | 2 | — |
| Max Cabin Seats | — | — | 5 | 6 | 9 | — | — |
| Standard Cabin Seats | — | — | 3 | 4 | 6 | 4 | — |
| Lavatory | — | — | — | 1 Flushing | Optional | No | — |
| Min Crew | — | — | — | 1 | 1 | 1 | — |
| Crew Rest | — | — | — | No | — | — | — |
| Jump Seat | — | — | — | No | — | — | — |
| Lavatory Location | — | — | — | AFT | FWD | — | — |
| Cabin Pressure (psi) | — | — | — | 8.3 | 5.8 | 5.5 | — |
| Galley / Refreshment | — | — | — | No | No | Refreshment Centre | — |
| SL Cabin Altitude (ft) | — | — | — | 21280 | 13100 | 12600 | — |
| Cargo Door | — | — | — | — | Yes | — | — |
| Galley Location | — | — | — | — | — | MID | — |
| Max Cabin Altitude (ft) | — | — | — | — | — | 8244 | — |
| Engine | |||||||
| FADEC | No | Yes | Yes | Yes | Yes | No | No |
| Model | IO-360-L2A | AE300 | AE330 | PW617F1-E | PT6E-67XP | PT6A-42A | O-360 |
| Fuel Type | AvGas | Diesel / Jet Fuel | Diesel / Jet Fuel | — | — | — | AvGas |
| TBO (hrs) | 2000 | 1800 | 1800 | 3500 | 5000 | 3600 | 2000 |
| TBO (yrs) | 12 | — | — | — | — | — | 12 |
| Horsepower | 200 | 168 | 180 | — | 1200 | 500 | 131 |
| Fuel Delivery | Fuel Injected | Fuel Injected | Fuel Injected | — | — | — | Carbureted |
| No. of Engines | 1 | 2 | 2 | 2 | 1 | 1 | 1 |
| Fuel Capacity (gal) | 42 | 79.4 | 89 | — | — | 170 | 115 |
| Usable Fuel (gal) | — | 76.4 | 86 | — | 402 | — | — |
| Flat Rating | — | — | — | ISA + 8 | ISA + 35 | ISA + 55 | — |
| Thrust (lbs) | — | — | — | 1730 | — | — | — |
| Fuel Burn (lbph) | — | — | — | 543 | — | — | — |
| Dimensions | |||||||
| Length (ft) | 27.2 | 28.1 | 30.1 | 42.1 | 47.25 | 29.6 | 28.5 |
| Wingspan (ft) | 36.1 | 44.5 | 47.8 | 40.4 | 53.33 | 43.2 | — |
| Cabin Width (ft) | 3.4 | — | — | 5.1 | 5 | 4.1 | — |
| Cabin Height (ft) | 4 | — | — | 4.9 | 4.9 | 4 | — |
| Cabin Length (ft) | 11.9 | — | — | 11 | 16.9 | 12.3 | — |
| Overall Height (ft) | 9 | 8.2 | 9.3 | 14.3 | 14 | 11.3 | 8.8 |
| Baggage Volume Int. (cu. ft) | 30 | — | — | 10 | 40 | 20 | 1.5 |
| Aisle Step (ft) | — | — | — | 0.3 | — | — | — |
| Cabin Width - Floor (ft) | — | — | — | 3.6 | 4.25 | — | — |
| Cabin Length - Seating (ft) | — | — | — | 9 | — | — | — |
| Baggage Volume Ext. (cu. ft) | — | — | — | 60 | — | — | — |
| Cabin Volume (cu. ft) | — | — | — | — | — | 165 | — |
| Rotor Diameter (ft) | — | — | — | — | — | — | 25.2 |