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 |