As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND BS 360 SKIN THICKNESS LOSS 10 PERCENT AT DIFFERENT STRINGER STATIONS IN BETWEEN STRINGER 10L AND STRINGER 10R, CROWN AREA INSPECTED PER AD 90-26-09. REMOVED AND REPLACED FASTENERS WITH OVERSIZE FASTENERS FROM STRINGER 5R TO 10R AND FROM STRINGER 5L TO 10L PER SB 727-53-0084. SKIN REPAIRED FROM STRINGER 5L TO 5R ON NR 19N00041.