What was found
INSPECTION FOUND A .25 INCH CRACK IN RIB AT WS 629. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR WAS INSTALLED IAW EA 5762-1050, FIGURE 8.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .25 INCH CRACK IN RIB AT WS 629. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR WAS INSTALLED IAW EA 5762-1050, FIGURE 8.