What was found
FATIGUE CRACK FOUND IN THE VERTICAL STABILIZER SKIN AT STRINGER 10R AND THE FUSELAGE CREASE LINE. DAMAGE IS TRIMMED OUT AND AN EXTERNAL REPAIR DOUBLER IS INSTALLED PER ER/A 334183-14.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FATIGUE CRACK FOUND IN THE VERTICAL STABILIZER SKIN AT STRINGER 10R AND THE FUSELAGE CREASE LINE. DAMAGE IS TRIMMED OUT AND AN EXTERNAL REPAIR DOUBLER IS INSTALLED PER ER/A 334183-14.