What was found
INSPECTION FOUND A 2 INCH CRACK IN BEAM BEHIND WEB AFTER REMOVAL OF NR 8 SPOILER FITTING. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1, PAGE 6A. A REPAIR WAS INSTALLED IAW SRM 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCH CRACK IN BEAM BEHIND WEB AFTER REMOVAL OF NR 8 SPOILER FITTING. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1, PAGE 6A. A REPAIR WAS INSTALLED IAW SRM 51-30-2.