What was found
LEFT HAND WING (S10) STRINGER END FOUND CRACK INSIDE FUEL TANK PANEL 538AB. STRINGER NR 10 CRACK REMOVED AS PER SRM 57-20-00 FIG 10 VOL I & INSTALLED REPAIRED ANGLES AS PER SRM 51-33-01 VOL II & SRM 57-20-00 FIG 10 VOL I.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT HAND WING (S10) STRINGER END FOUND CRACK INSIDE FUEL TANK PANEL 538AB. STRINGER NR 10 CRACK REMOVED AS PER SRM 57-20-00 FIG 10 VOL I & INSTALLED REPAIRED ANGLES AS PER SRM 51-33-01 VOL II & SRM 57-20-00 FIG 10 VOL I.