As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFTER REMOVAL OF "Z" STIFFENER FROM R/H UPPER TRANSCOWL, IT WAS DISCOVERED THAT A CRACK EXISTS AT THETOP HOLE LOCATIION ON THE SKIN DIRECTLY UNDER THE "Z" STIFFENER. (C CHECK RO 5/23/22) PERMANENTLY REPAIRED R/H UPPER TRANSCOWL INNER SKIN CRACK REF MHIRJ REO 690-54-21-418 REV -- DATED 2022-04-13. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY