What was found
INSPECTION FOUND A CRACK APPROXIMATELY .25 INCH LONG AT HOLE IN STRINGER 21L BETWEEN STA 460 - 480. THE HOLE WAS REAMED TO 0.312 INCH. AN ANGLE REPAIR WAS INSTALLED IAW SRM 53-00-03.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A CRACK APPROXIMATELY .25 INCH LONG AT HOLE IN STRINGER 21L BETWEEN STA 460 - 480. THE HOLE WAS REAMED TO 0.312 INCH. AN ANGLE REPAIR WAS INSTALLED IAW SRM 53-00-03.