What was found
CRACK ON RING PAN AFT UPPER CORNER STA Y=1155 RT. (CRACK LONG 0.0380") 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 AFT UPPER CORNER STA Y=1155 RT. (CRACK LONG 0.0380") AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.