What was found
FOLLOWING REMOVAL OF THE R/H PICKLE FORK FRAME ASSEMBLY CORROSION WAS FOUND AT TWO FASTENER HOLE LOCATIONS IN THE SKIN, BETWEEN BS. 665 TO BS. 667, RBL 70. / REPAIRED SKIN PER EA.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOLLOWING REMOVAL OF THE R/H PICKLE FORK FRAME ASSEMBLY CORROSION WAS FOUND AT TWO FASTENER HOLE LOCATIONS IN THE SKIN, BETWEEN BS. 665 TO BS. 667, RBL 70. / REPAIRED SKIN PER EA.