What was found
CRACK ON SPLICE AND ANGLE ON INNER SKIN LT WING L/E STA XOS:296. SPLICE AND ANGLE WERE REPLACED ON INNER SKIN LT WING L/E STA XOS:296 PER SRM 51-41-02-0G, 51-41-05-0G, 57-40-01, AND DWG 9919326 REV E.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON SPLICE AND ANGLE ON INNER SKIN LT WING L/E STA XOS:296. SPLICE AND ANGLE WERE REPLACED ON INNER SKIN LT WING L/E STA XOS:296 PER SRM 51-41-02-0G, 51-41-05-0G, 57-40-01, AND DWG 9919326 REV E.