What was found
RT WING TO FUSELAGE HEAVY ANGLE CRACKED ATH FWD BEND RADIUS APPROX 1.125 INCH IN LENGTH. MAINTENANCE INSTALLED REPAIR ANGLE I.A.W. SRM 53-90-23. REPAIR ANGLE 13.5 ". RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RT WING TO FUSELAGE HEAVY ANGLE CRACKED ATH FWD BEND RADIUS APPROX 1.125 INCH IN LENGTH. MAINTENANCE INSTALLED REPAIR ANGLE I.A.W. SRM 53-90-23. REPAIR ANGLE 13.5 ". RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1.