What was found
AT C-CHECK, RIB CRACKED JUST FWD OF TOP CHORD FWD SPAR AT STA 349, RIGHT WING. STOP DRILLED CRACK, DYE PEN INSP. INSTALLED ANGLE REPAIR PER SRM 51-40-3, REPAIR 6 BY 1.5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, RIB CRACKED JUST FWD OF TOP CHORD FWD SPAR AT STA 349, RIGHT WING. STOP DRILLED CRACK, DYE PEN INSP. INSTALLED ANGLE REPAIR PER SRM 51-40-3, REPAIR 6 BY 1.5.