As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SKIN CRACK ON RT WING AT STA XFS 63.540. REMOVED EXISTING FASTENERS AND STOP DRILLED AT EACH END OF CRACK PER MD88 SRM 57-06B FIG 33 (SHEET 2) NDT INSP OF STOP DRILLED CRACK ENDS PER SRM 57-06B 27D (1)(B) NO CRACKING BEYOND STOP DRILLED HOLES INDICTED. FABRICATED REPAIR DOUBLER FROM .063 7075-0 DOUBLER HEAT TREATED ON SHOP ORDER OF8385 INSTALLED DOUBLER PER SRM 57-06B.