As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON ACCESSING THE FWD SIDE OF THE VAPOR BARRIER WEB; FOUND THE WEB CRACK AT 33LBL TO EXTEND UPWARDS 17.5' RUNNING UNDERNEATH THE VERTICAL STIFFENER AT 30LBL AND THOUGH THE VERTICAL STIFFENER ATTACH FASTENERS TURNING INBOARD TO THE CANNON PLUG DOUBLER AT 27LBL.<[01] REPAIRED IAW EA 24-157-03204.;[02] C/W EA 24-157-03202 AND EA 24-157-03204.;[03] C/W EA 24-157-03202 AND EA 24-157-03204.;[04] C/W