What was found
UPPER WING TO FUSELAGE FAIRING ATTACH ANGLE ON FUSELAGE HAS A 1" CRACK AT FRAME 42. REMOVED AND REPLACED RT UPPER WING TO FUSELAGE FAIRING ATTACH ANGLE AT FRAME 42 IAW SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPPER WING TO FUSELAGE FAIRING ATTACH ANGLE ON FUSELAGE HAS A 1" CRACK AT FRAME 42. REMOVED AND REPLACED RT UPPER WING TO FUSELAGE FAIRING ATTACH ANGLE AT FRAME 42 IAW SRM 51-40-02.