What was found
INSPECTION FOUND A 2 INCH CRACK IN LONGERON 36L AT FUSELAGE SKIN JOINT STA 1129. THE CRACKED SECTION OF LONGERON WAS REMOVED AND A NEW SECTION WAS FITTED IAW SRM 53-10-00.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCH CRACK IN LONGERON 36L AT FUSELAGE SKIN JOINT STA 1129. THE CRACKED SECTION OF LONGERON WAS REMOVED AND A NEW SECTION WAS FITTED IAW SRM 53-10-00.