What was found
CRACK FOUND ON EXTERNAL SKIN AT THE CHEM-MILLED STEP LOCATED AT BS 500D + 4.5" BELOW STR 15 L, CRACK LENGHT APROX. = 1.8". REPAIRED FUSELAGE SKIN IAW EO AEM-HC53-022/13 R0 AND EA 1-353-21716 REV 0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK FOUND ON EXTERNAL SKIN AT THE CHEM-MILLED STEP LOCATED AT BS 500D + 4.5" BELOW STR 15 L, CRACK LENGHT APROX. = 1.8". REPAIRED FUSELAGE SKIN IAW EO AEM-HC53-022/13 R0 AND EA 1-353-21716 REV 0.