As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
PIT - DURING Q-1 CHECK, FOUND 9 INCH BY 14 INCH AREA OF SKIN DELAMINATION/HEAT DAMAGE AT LEFT STUBWING BETWEEN FRAMES 24011 AND 24611 AND STRINGERS 22 AND 23 ON FUSELAGE SKIN. DETECTED BY VISUAL/TAP TEST/CONDUCTIVITY TEST. CUT OUT DAMAGED AREA AND INSTALLED AN EXTERNAL DOUBLER PER EA 29200A. (M)