What was found
1.906 INCH CRACK ON FUSELAGE SKIN, BS 1418 BETWEEN LONGERON 1 AND 2R. REPAIRED IAW ER/A 519149-14AD REV ORIGINAL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
1.906 INCH CRACK ON FUSELAGE SKIN, BS 1418 BETWEEN LONGERON 1 AND 2R. REPAIRED IAW ER/A 519149-14AD REV ORIGINAL.