What was found
LH WING-TO-FUSELAGE UPPER SUPPORT ANGLE HAS EVIDENCE OF A CRACK BY THE RIVET. APPROX 1" LONG AT FRAME 48.-C/A-REPAIRED IAW SRM 53-23-12 ITEM #3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LH WING-TO-FUSELAGE UPPER SUPPORT ANGLE HAS EVIDENCE OF A CRACK BY THE RIVET. APPROX 1" LONG AT FRAME 48.-C/A-REPAIRED IAW SRM 53-23-12 ITEM #3.