What was found
INSPECTION FOUND A 1.5 INCH CRACK IN NR 1 PYLON WEB AT STA 1021. THE CRACK WAS LOCATED AT INTERSECTION WITH UPPER SKIN. THE CRACKED AREA WAS REMOVED. REPAIR ANGLES WERE 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 1.5 INCH CRACK IN NR 1 PYLON WEB AT STA 1021. THE CRACK WAS LOCATED AT INTERSECTION WITH UPPER SKIN. THE CRACKED AREA WAS REMOVED. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 54-01, FIGURE 2.