As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WHILE WORKING EA 5310-05292 REV B OP10, A CRACK WAS FOUND IN BS 883.5 FRAME INNER CHORD EMANATING FROM FASTENER HOLE NR 4 AS SHOWN IN "EN PAGE 3" OF ECRA 5310-07095. REF ECRA 5310-07095 FOR A MORE DETAILED DESCRIPTION OF CRACK, INTERIM REPAIR ACP.