As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
BLEND IN FUSELAGE SKIN AROUND FASTENER AT BS1350 BETWEEN S5L AND S6L MEASURED AND EVALUATED PREVIOUS BLEND ON FUSELAGE SKIN AT BS 1350 BETWEEN S.5L AND S.6L IAW SRM 53-00-01-1A , FIG 101 DETAIL III AND FOUND TO BE OUT OF LIMITS. CARRIED OUT SMALL HOLE FLUSH REPAIR ON FUSELAGE SKIN AT BS 1350 BETWEEN S.5L AND S.6L IAW SRM 53-00-01-2R FIG 201 REPAIR 7.