What was found
LH UPPER WING TO FUSELAGE SUPPORT ANGLE. JUST AFT OF FRAME 50 HAS EVIDENCE OF 1" CRACK. -C/A-REPAIRED LH UPPER WING TO FUSELAGE SUPPORT ANGLE IAW SRM 53-23-12 AND SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LH UPPER WING TO FUSELAGE SUPPORT ANGLE. JUST AFT OF FRAME 50 HAS EVIDENCE OF 1" CRACK. -C/A-REPAIRED LH UPPER WING TO FUSELAGE SUPPORT ANGLE IAW SRM 53-23-12 AND SRM 51-40-02.