What was found
FUSELAGE SKIN, BETWEEN STA 306 TO STA 311, STR 24R, LAP JOINT CRACKED. POSSIBLE CAUSE OF THE CRACK WAS FATIGUE. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN, BETWEEN STA 306 TO STA 311, STR 24R, LAP JOINT CRACKED. POSSIBLE CAUSE OF THE CRACK WAS FATIGUE. (X)