As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LWR FUSELAGE SKIN BETWEEN STA 950B AND 950C AT BL0 IS BULDGING WITH 2 EACH RIVET HEADS POPPED. COMPLIED WITH EA 7-5330-124049 PART 1 BY MANUFACTURING FILLER, DOUBLER AND TRIPLER OUT OF2024T3 180/90/100C. REMOVED DAMAGE AND INSTALLED PARTS ALL IAW EA 7- 5330-124049 PART 1. MAJOR REPAIR RII.