Narrative:

Upon landing in a crosswind and gust of 15 knots from around 310 degree directional control was temporarily compromised right after the touchdown. The maximum left rudder was applied but the direction was not adjusted enough to follow the straight line. The airplane veered to the right. Instead of applying heavy braking; due to a doubt of sufficient braking action; the airplane was directed to the unpaved area between the runway and taxiway. The airplane was slowed and stopped on the taxiway. After a short explanation was given to the tower the airplane was taxied to the fuel pump. Visual inspections gave no indication of any kind of damages to the airplane. After refueling; return flight was made normally. One possible contributor was the rudder trim; which was trimmed to the left during the flight and was not returned to the neutral position. During the landing; the rudder authority was not as good as expected although the crosswind component was within the limit specified in the operation manual. Secondary; the gust in the cross wind might have been exceeded the limit together with the steady component of the wind.

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Original NASA ASRS Text

Title: A Commander 112 pilot reported a runway excursion while landing in a crosswind.

Narrative: Upon landing in a crosswind and gust of 15 knots from around 310 degree directional control was temporarily compromised right after the touchdown. The maximum left rudder was applied but the direction was not adjusted enough to follow the straight line. The airplane veered to the right. Instead of applying heavy braking; due to a doubt of sufficient braking action; the airplane was directed to the unpaved area between the runway and taxiway. The airplane was slowed and stopped on the taxiway. After a short explanation was given to the tower the airplane was taxied to the fuel pump. Visual inspections gave no indication of any kind of damages to the airplane. After refueling; return flight was made normally. One possible contributor was the rudder trim; which was trimmed to the left during the flight and was not returned to the neutral position. During the landing; the rudder authority was not as good as expected although the crosswind component was within the limit specified in the operation manual. Secondary; the gust in the cross wind might have been exceeded the limit together with the steady component of the wind.

Data retrieved from NASA's ASRS site and automatically converted to unabbreviated mixed upper/lowercase text. This report is for informational purposes with no guarantee of accuracy. See NASA's ASRS site for official report.