Rockwell Aero Commander 100 / Darter & Lark Commander
Touring Aircraft
The Aero Commander 100 is a single-engine three- or four-seat light touring aircraft developed by the US-American manufacturer Volaircraft Inc and produced by the Aero Commander Division of the Rockwell-Standard Corp., later North American Rockwell.
| Propulsion | 1 Piston Engine |
| Engine Model | Lycoming O-320-A1A |
| Engine Power | 112 kW | 150 hp |
| max. Cruise Speed | 217 km/h | 117 kts 135 mph |
| max. Speed (vne) | 274 km/h | 148 kts 170 mph |
| Service Ceiling | 2.972 m | 9.750 ft |
| Rate of climb | 239 m/min | 785 ft/min |
| Range | 820 km | 443 NM 510 mi. |
| Empty Weight | 580 kg | 1.279 lbs |
| max. Takeoff Weight | 1.020 kg | 2.249 lbs |
| Wing Span | 10,67 m | 35 ft 0 in |
| Wing Area | 16,8 m² | 181 ft² |
| Length | 6,86 m | 22 ft 6 in |
| Height | 2,84 m | 9 ft 4 in |
| First Flight | 1960 |
| Production Status | out of production |
| Production Range | 1964-1969 |
| Total Production | 570 |
| ICAO Code | LARK VO10 |
| FAA TCDS | 1A21 |
| Data for (Version) | Rockwell Darter Commander |
| Variants | Volaire Model 10 / Volaire 1035 / Aero Commander Model 100A, Volaire Model 10A / Volair 1050 / Aero Commander Model 100 / Darter Commander, Aero Commander Model 100-180 Lark Comman |