What was found
FUSELAGE TO VERTICLE WEB SUPPORT ANGLE HAS A 1.00" CRACK AT STATION 1746 ON THE LT AND RT ENDS OF THE ANGLE. COMMON TO PANELS 324AR AND 324AL. REPLACED FUSELAGE TO VERTICLE WEB SUPPORT ANGLE IAW SRM 51-40-02, 51-21-04, AND 51-21-10.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE TO VERTICLE WEB SUPPORT ANGLE HAS A 1.00" CRACK AT STATION 1746 ON THE LT AND RT ENDS OF THE ANGLE. COMMON TO PANELS 324AR AND 324AL. REPLACED FUSELAGE TO VERTICLE WEB SUPPORT ANGLE IAW SRM 51-40-02, 51-21-04, AND 51-21-10.