What was found
RT FUSELAGE UPPER SKIN AT BS 380 STR 24R LAP JOINT HAD A 2 INCH CRACK. REPAIRED IAW EA 26-153-02262. EA-26-153-02262 COMPLIED WITH. NO INSPECTION OR RII REQUIRED ON EA.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RT FUSELAGE UPPER SKIN AT BS 380 STR 24R LAP JOINT HAD A 2 INCH CRACK. REPAIRED IAW EA 26-153-02262. EA-26-153-02262 COMPLIED WITH. NO INSPECTION OR RII REQUIRED ON EA.