What was found
CRACK ON UPPER FLANGE OF FRAME BS 1050, RBL 9, WL 155 ON PREVIOUS REPAIR, CRACK EXTENDS .5 BEYOND STOP DRILL HOLE. *S/D* CUT OUT DAMAGED FRAME SECTION AND REPAIRED PER FED-EX SRM 53-40-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON UPPER FLANGE OF FRAME BS 1050, RBL 9, WL 155 ON PREVIOUS REPAIR, CRACK EXTENDS .5 BEYOND STOP DRILL HOLE. *S/D* CUT OUT DAMAGED FRAME SECTION AND REPAIRED PER FED-EX SRM 53-40-3.