What was found
CRACK ON RING PAN FWD UPPER CORNER STA Y= 522 AND AFT LWR STA Y=943 RT. (CRACK LONG 0.380") AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON RING PAN FWD UPPER CORNER STA Y= 522 AND AFT LWR STA Y=943 RT. (CRACK LONG 0.380") AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.