What was found
RIVET HOLES IN LEADING EDGE LOWER SKIN (AFT FASTENER ROW) JUST FWD OF I/B HAS CRACKS. REMOVED DAMAGE, INSTALLED FILLER & EXTERNAL DOUBLER PER SRM 57-43-01, DEFECT SIZE: 7 INCHES TOTAL ACCUMULATIVE LENGTH, 2 EA.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIVET HOLES IN LEADING EDGE LOWER SKIN (AFT FASTENER ROW) JUST FWD OF I/B HAS CRACKS. REMOVED DAMAGE, INSTALLED FILLER & EXTERNAL DOUBLER PER SRM 57-43-01, DEFECT SIZE: 7 INCHES TOTAL ACCUMULATIVE LENGTH, 2 EA.