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-REMOVED AND REPLACED LH WING TO FUSELAGE #2 LOWER ATTACHMENT ANGLE IAW ETN-53-142, AND 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-REMOVED AND REPLACED LH WING TO FUSELAGE #2 LOWER ATTACHMENT ANGLE IAW ETN-53-142, AND SRM 51-40-02.