What was found
A 0.187 INCH CRACK ON FUSELAGE SKIN, BS 1418 BETWEEN LONGERONS 2 - 3L AND A CRACK OF 0.531" BETWEEN LONGERON 1 AND 2R. FUSELAGE SKIN WAS REPAIRED IAW ER/A 536455-14AD, REV ORIGINAL AND ETI 88-15-204, REV 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A 0.187 INCH CRACK ON FUSELAGE SKIN, BS 1418 BETWEEN LONGERONS 2 - 3L AND A CRACK OF 0.531" BETWEEN LONGERON 1 AND 2R. FUSELAGE SKIN WAS REPAIRED IAW ER/A 536455-14AD, REV ORIGINAL AND ETI 88-15-204, REV 2.