As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE INTERIOR BS 1176 -9 CHORD HAS 4 OPEN FASTENER HOLES BETWEEN LBL 17.5 AND RBL 17.5 WITH LOW EDGE DISTANCE AND NO EDGE DISTANCE. COMPLIED WITH EA 7-5310-143902 , INSTALLED NEW CHORD SECTION P/N 5310212 DIM. 65.5" LONG, AND FABRICATED AND INSTALLED 2EA SPLICES FROM 7075T73511 0.500" DIM 12" X 2" IAW EA 7-5310-143902.