What was found
CRACK ON RINGPAN LOWER CORNER FWD STA 1156 RT SIDE. (CRACK LONG 0.385") 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 RINGPAN LOWER CORNER FWD STA 1156 RT SIDE. (CRACK LONG 0.385") AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.