What was found
DISBOND DETECTED ON LEFT FUSELAGE SKIN PANEL BETWEEN FUSELAGE STA 488.50 AND STA 510.00 AND BETWEEN STR 23 AND STR 24.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DISBOND DETECTED ON LEFT FUSELAGE SKIN PANEL BETWEEN FUSELAGE STA 488.50 AND STA 510.00 AND BETWEEN STR 23 AND STR 24.