What was found
CRACKED FUSELAGE SKIN AT BS 1380, BETWEEN LONGERONS 13-14L. REPAIRED IAW SRM 51-30-2, 51-30-5, 53-04, FIG 18, 51-10-3, PAR 14 AND 21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED FUSELAGE SKIN AT BS 1380, BETWEEN LONGERONS 13-14L. REPAIRED IAW SRM 51-30-2, 51-30-5, 53-04, FIG 18, 51-10-3, PAR 14 AND 21.