What was found
INSPECTION FOUND A 4" CRACK IN FRAME TO LONGERON ATTACH WEB IN AFT ACCESSORY AREA AT FS 1430, R/H SIDE. THE CRACK WAS STOP DRILLED IAW SRM 53-01, FIGURE 2. A DOUBLER WAS INSTALLED IAW SRM 53-14-4, 51-10-4, 51-10-3, AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 4" CRACK IN FRAME TO LONGERON ATTACH WEB IN AFT ACCESSORY AREA AT FS 1430, R/H SIDE. THE CRACK WAS STOP DRILLED IAW SRM 53-01, FIGURE 2. A DOUBLER WAS INSTALLED IAW SRM 53-14-4, 51-10-4, 51-10-3, AND 51-30-2.