As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE / FS 680 AND STR 26L - REPAIR OF LIGHTNING STRIKE: DAL ER/A 385076-14 PROVIDES INSTRUCTIONS TO TRIM OUT THE DAMAGED SKIN AND INSTALL AN EXTERNAL DOUBLER AND STRUCTURAL FILLER. THE FUSELAGE SKIN IS M/F 2024-T3 CLAD ALUMINUM WITH A LOCAL THICKNESS OF 0.056 INCH AND 0.042 INCH IN THE TRIMMED AREA.