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Vmcg
Minimum Control Speed Ground
| Question | Answer |
|---|---|
| Ground minimum control speed, Vmcg (88 KIAS), is | is the minimum controllable speed during the take-off run, at which, when an engine is failed |
| it is possible to maintain directional control using only primary aerodynamic controls without deviating more than 25 feet laterally with all three wheels on the runway. | The speed is established with the remaining engine at the take-off thrust setting, |
| the aircraft loaded at the most unfavorable weight and center of gravity and the aircraft trimmed for take-off, without | without exceeding 180 pounds of rudder control force by the pilot with the rudder boost system operating. Conditions of crosswind and RCR may increase Vmcg. |