What was found
AT SCHEDULED INSPECTION DISCOVERED EXFOLIATION AT LOWER FUSELAGE SKIN AT FS 250.750 STRINGER 15L. REMOVED DAMAGED SKIN AND INSTALLED REPAIR DOUBLER PER BEECH STRUCTURAL REPAIR MANUAL 51-70-06.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT SCHEDULED INSPECTION DISCOVERED EXFOLIATION AT LOWER FUSELAGE SKIN AT FS 250.750 STRINGER 15L. REMOVED DAMAGED SKIN AND INSTALLED REPAIR DOUBLER PER BEECH STRUCTURAL REPAIR MANUAL 51-70-06.