What was found
#4 ENG R/H CORE COWL FRAME #5 (COUNT FROM FWD) FOUND CRACKED. FRAME CRACK AREA REPAIRED AS PER SRM 54-41-02-2R-2 REPAIR 2 FIG 201. NO FURTHER DEFECTS NOTED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
#4 ENG R/H CORE COWL FRAME #5 (COUNT FROM FWD) FOUND CRACKED. FRAME CRACK AREA REPAIRED AS PER SRM 54-41-02-2R-2 REPAIR 2 FIG 201. NO FURTHER DEFECTS NOTED.