What was found
LEFT HAND UPPER NR 9 STRINGER END FOUND CRACK AT INSIDE ACCESS PANEL 538AB. REPAIR SPLICE ANGLE FABRICATED AS PER SRM 57-20-00, VOLUME I; NEW STRINGER AND SPLICE ANGLES INSTALLED AS PER SRM 57-20-00, VOLUME I.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT HAND UPPER NR 9 STRINGER END FOUND CRACK AT INSIDE ACCESS PANEL 538AB. REPAIR SPLICE ANGLE FABRICATED AS PER SRM 57-20-00, VOLUME I; NEW STRINGER AND SPLICE ANGLES INSTALLED AS PER SRM 57-20-00, VOLUME I.