What was found
CRACK ON RT INTERNAL FUSELAGE LONGERON 2 RT ON STA Y=579. LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18, 51-30-2, 51-30-5, 51-10-3 PAR 14 AND 21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON RT INTERNAL FUSELAGE LONGERON 2 RT ON STA Y=579. LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18, 51-30-2, 51-30-5, 51-10-3 PAR 14 AND 21.