What was found
CRACK ON RING PAN FWD UPPER CORNER STA Y= 1002 AND FWD LWR STA Y= 1136 RT. (CRACK LONG 0.400") 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= 1002 AND FWD LWR STA Y= 1136 RT. (CRACK LONG 0.400") AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.