As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AT 2 EACH SKIN ATTACH FASTENER HOLES 7 INCHES AND 8 INCHES FORWARD OF BS 540 FRAME S15R STRINGER FUSELAGE. INSTALLED STRINGER SPLICE AND REPAIRED PER SRM 53-10-3 FIG 1 AND EA 43631. (X)