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 SKIN ATTACH FASTENER HOLES 5 INCHES TO 11 INCHES FOWARD OF BS 540 FRAME S15L STRINGER (FUSELAGE). INSTALLED STRINGER SPLICE, REPAIRED PER SRM 53-10-3 FIG 1 AND EA 43631. (X)