What was found
LH WING-TO-FUSELAGE UPPER ATTACHMENT ANGLE. HAS EVIDENCE OF A CRACK APPROX. 1/2" LONG. JUST BELOW A RIVET AT FRAME 50.-C/A-RAR LH WING-TO-FUSELAGE UPPER ATTACHMENT ANGLE IAW SRM 51-40-02
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LH WING-TO-FUSELAGE UPPER ATTACHMENT ANGLE. HAS EVIDENCE OF A CRACK APPROX. 1/2" LONG. JUST BELOW A RIVET AT FRAME 50.-C/A-RAR LH WING-TO-FUSELAGE UPPER ATTACHMENT ANGLE IAW SRM 51-40-02