What was found
CRACKED LONGERON 2RT STA Y=655 AT FUSELAGE INTERNAL STRUCTURE (F/S) (REF NRC:T0 263597) SECTION LONGERON WAS REPLACED IAW 53-02 RII COMPLETED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED LONGERON 2RT STA Y=655 AT FUSELAGE INTERNAL STRUCTURE (F/S) (REF NRC:T0 263597) SECTION LONGERON WAS REPLACED IAW 53-02 RII COMPLETED.