As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING LIGHTNING STRIKE DAMAGE INSPECTION OF RIGHT FUSELAGE FOUND AREA BETWEEN STRINGER 26R-27R AT FS 243 TO BE PREVIOUSLY BLENDED BEYOND LIMITS OF SRM 53-00-31. BLEND DEPTH .007 INCH. CUT OUT DAMAGED SECTION AND INSTALLED LOCALLY FABRICATED DOUBLER AND FILLER IAW BRAS EO 601R-53-5342. (M)