What was found
INSPECTION FOUND A 6 INCH CRACK IN RT WING L/E RIB AT TRACK NR 8, XRS 248. THE CRACK WAS STOP DRILLED IAW SRM 57-01, FIGURE 3. A REPAIR ANGLE WAS INSTALLED IAW SRM 57-10, FIGURE 3 AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 6 INCH CRACK IN RT WING L/E RIB AT TRACK NR 8, XRS 248. THE CRACK WAS STOP DRILLED IAW SRM 57-01, FIGURE 3. A REPAIR ANGLE WAS INSTALLED IAW SRM 57-10, FIGURE 3 AND 51-30-2.