What was found
FUSELAGE SKIN, STA 948, STR 25R, 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, STA 948, STR 25R, LAP JOINT CRACKED. POSSIBLE CAUSE OF THE CRACK WAS FATIGUE. (X)