What was found
CRACK ON LONGERON 4R, BS 541 AT INTERNAL FUSELAGE STRUCTURE BEHIND LIFE RAFT SUPPORT. THE LONGERON WAS REPAIRED IAW 53-02, FIG 18.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON LONGERON 4R, BS 541 AT INTERNAL FUSELAGE STRUCTURE BEHIND LIFE RAFT SUPPORT. THE LONGERON WAS REPAIRED IAW 53-02, FIG 18.