What was found
CRACK OF 0.125" ON FUSELAGE SKIN AT BS 1418 BETWEEN LONGERONS 2-3L. REPAIRED IAW ER/A 521196-14AD.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK OF 0.125" ON FUSELAGE SKIN AT BS 1418 BETWEEN LONGERONS 2-3L. REPAIRED IAW ER/A 521196-14AD.