What was found
INSPECTION FOUND A .5 INCH CRACK IN RT WING UPPER PANEL FORWARD OF NR 7 SPOILER. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. DOUBLERS WERE INSTALLED IAW SRM 57-30-4, FIGURE 10, 51-10-2 AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN RT WING UPPER PANEL FORWARD OF NR 7 SPOILER. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. DOUBLERS WERE INSTALLED IAW SRM 57-30-4, FIGURE 10, 51-10-2 AND 51-30-2.