What was found
INSPECTION FOUND A 2 INCH CRACK IN SUPPORT FITTING ON LT AFT END MLG DOOR CUTOUT. THE CRACK WAS TRIMMED OUT IAW SRM 53-05, FIGURE 71. A REPAIR WAS FABRICATED AND INSTALLED SRM 53-05, FIGURE 71 AND 51-10-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCH CRACK IN SUPPORT FITTING ON LT AFT END MLG DOOR CUTOUT. THE CRACK WAS TRIMMED OUT IAW SRM 53-05, FIGURE 71. A REPAIR WAS FABRICATED AND INSTALLED SRM 53-05, FIGURE 71 AND 51-10-3.