What was found
.625 INCH LONG CRACK, CONE SKIN 31 FROM I/B END OF FLAP, ALSO COVE SKIN TORN 32 FROM O/B END OF FLAP. BOTH AREAS REPAIRED PER MM 57-52-FIG 809.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
.625 INCH LONG CRACK, CONE SKIN 31 FROM I/B END OF FLAP, ALSO COVE SKIN TORN 32 FROM O/B END OF FLAP. BOTH AREAS REPAIRED PER MM 57-52-FIG 809.