What was found
CRACKED LT RING PAN LOWER/AFT CORNER STA Y=636 INTERNAL STRUCTURE (FUS). RING PAN WAS REPAIR PER B717 SRM 56-20-02 FIG 202.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED LT RING PAN LOWER/AFT CORNER STA Y=636 INTERNAL STRUCTURE (FUS). RING PAN WAS REPAIR PER B717 SRM 56-20-02 FIG 202.