What was found
ON CLIMB-OUT ABOVE 6000 FT AND AT OR ABOVE 230 KTS, FELT EXCESSIVE VIBRATION THOUGH OUT AIRFRAME. REMOVED AND REPLACED LATERAL CONTROL SPOILER POWER CYLINDER AND CONTROL VALVE (LEFT WING). OPS AND LEAK CHECKED PER MM 27-62-9.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ON CLIMB-OUT ABOVE 6000 FT AND AT OR ABOVE 230 KTS, FELT EXCESSIVE VIBRATION THOUGH OUT AIRFRAME. REMOVED AND REPLACED LATERAL CONTROL SPOILER POWER CYLINDER AND CONTROL VALVE (LEFT WING). OPS AND LEAK CHECKED PER MM 27-62-9.