What was found
DURING SCHEDULED 1/2 D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 534 AND 530, AT S14L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED 1/2 D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 534 AND 530, AT S14L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.