What was found
INSPECTION FOUND A 2 INCH CRACK AT LOWER END OF WEB JUST FORWARD OF AFT ENGINE MOUNT, NR 2 PYLON. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-01, FIGURE 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCH CRACK AT LOWER END OF WEB JUST FORWARD OF AFT ENGINE MOUNT, NR 2 PYLON. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-01, FIGURE 2.