What was found
LT WING TO FUSELAGE HEAVY ANGLE CRACKED APPROX 1.750 AT FWD BEND RADIUS AT FS 288.0. MAINT REPAIRED THE LT TO FUSELAGE HEAVY ANGLE IAW. SRM 53-90. REPAIR APPROX 13.5 INCH. RII INSP COMPLIED IAW TASKCARD 8.2.1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT WING TO FUSELAGE HEAVY ANGLE CRACKED APPROX 1.750 AT FWD BEND RADIUS AT FS 288.0. MAINT REPAIRED THE LT TO FUSELAGE HEAVY ANGLE IAW. SRM 53-90. REPAIR APPROX 13.5 INCH. RII INSP COMPLIED IAW TASKCARD 8.2.1.