What was found
LOWER FUSELAGE SKIN AT BS 1501 BETWEEN LONGERONS 50 - 51R HAD A 2 INCH CRACK PROPAGATING THROUGH TWO FASTENERS HOLES. REPAIRED IAW EA 8-5330-T0339089.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LOWER FUSELAGE SKIN AT BS 1501 BETWEEN LONGERONS 50 - 51R HAD A 2 INCH CRACK PROPAGATING THROUGH TWO FASTENERS HOLES. REPAIRED IAW EA 8-5330-T0339089.