As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ABI - DURING A VISIT INSPECTION, FOUND A DENT ON RIGHT FORWARD FUSELAGE SKIN PANEL BETWEEN FRAMES 3 AND 4. CUT OUT DAMAGED AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO INDICATION OF CRACKS. APPLIED ALODINE TO EDGES OF CUT OUT. FABRICATED AN EXTERNAL DOUBLER .050 THICK. TREATED AREA AND ATTACHED TO FUSELAGE. RESTORED SURFACE FINISH. (M)