What was found
FUSELAGE EXTERIOR SKIN, HAS A CRACK BETWEEN BS 395 - 418 AT STRINGER 4 RT THAT MEASURES APPROX 0.4. REPAIRED IAW EA F-5330-T0318521 PART 1. REPAIR CLASSIFIED AS MAJOR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE EXTERIOR SKIN, HAS A CRACK BETWEEN BS 395 - 418 AT STRINGER 4 RT THAT MEASURES APPROX 0.4. REPAIRED IAW EA F-5330-T0318521 PART 1. REPAIR CLASSIFIED AS MAJOR.