As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WHILE PERFORMING LIGHTNING STRIKE DAMAGE INSPECTION FOUND RIGHT FUSELAGE AREA BETWEEN STRINGER 24R-25R AT FS 220-235 TO BE PREVIOUSLY BLENDED BEYOND LIMITS OF SRM 53-00-31. BLEND DEPTH .010 INCH. CUTOUT DAMAGED SECTION AND INSTALLED LOCALLY FABRICATED DOUBLER AND FILLER IAW BRAS EO 601R-53-5343. (M)