What was found
FUSELAGE SKIN AT FRAME 34, STRINGER 43L - 43R, CHAFE. REPAIRED IAW EA 5300-02120, OP 1, STEP 4.1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN AT FRAME 34, STRINGER 43L - 43R, CHAFE. REPAIRED IAW EA 5300-02120, OP 1, STEP 4.1.