What was found
RIGHT HAND UPPER NR 9 STRINGER END FOUND CRACK AT INSIDE ACCESS PANEL 638AB. REPAIR ANGLES FABRICATED AS PER SRM 57-20-00, FIGURE 10, VOLUME I AND INSTALLED AS PER SRM 57-20-00, FIGURE 10, SHEET 6, VOLUME I.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT HAND UPPER NR 9 STRINGER END FOUND CRACK AT INSIDE ACCESS PANEL 638AB. REPAIR ANGLES FABRICATED AS PER SRM 57-20-00, FIGURE 10, VOLUME I AND INSTALLED AS PER SRM 57-20-00, FIGURE 10, SHEET 6, VOLUME I.