What was found
ATW - FLT 505 - ON CLIMB-OUT ACCELERATING THROUGH 240-250 KNOTS, FELT SLIGHT AIRFRAME VIBRATION. AS SPEED INCREASED, VIBRATION INCREASED. REPLACED PANEL ON RT TRAILING EDGE OF WING AND SEAL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ATW - FLT 505 - ON CLIMB-OUT ACCELERATING THROUGH 240-250 KNOTS, FELT SLIGHT AIRFRAME VIBRATION. AS SPEED INCREASED, VIBRATION INCREASED. REPLACED PANEL ON RT TRAILING EDGE OF WING AND SEAL.