What was found
CRACK INDICATION FOUND IN THE FUSELAGE SKIN ALONG THE CHEM-MILLED STEP LOCATED ABOVE STR 15L AND BS S00D+3" CRACK LENGTH:1.5" APPROX. 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 INDICATION FOUND IN THE FUSELAGE SKIN ALONG THE CHEM-MILLED STEP LOCATED ABOVE STR 15L AND BS S00D+3" CRACK LENGTH:1.5" APPROX. REPAIRED FUSELAGE SKIN IAW EO AEM-HC53-022/13 R0 AND EA 1-353-21716 REV 0.