What was found
LEFT UPPER WING TO FUSELAGE FAIRING UPPER ATTACHMENT ANGLE ON FUSELAGE HAS 1/4 INCH CRACK BETWEEN FRAMES 41 - 42. REPAIRED IAW SRM 53-23-12.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT UPPER WING TO FUSELAGE FAIRING UPPER ATTACHMENT ANGLE ON FUSELAGE HAS 1/4 INCH CRACK BETWEEN FRAMES 41 - 42. REPAIRED IAW SRM 53-23-12.