What was found
DURING HMV, A CRACKED LONGERON 3 L BS 160 OF FUSELAGE INTERNAL STRUCTURE. DAMAGED LONGERON REPAIRED IAW SRM 53-02 PARA 12 FIG 18.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING HMV, A CRACKED LONGERON 3 L BS 160 OF FUSELAGE INTERNAL STRUCTURE. DAMAGED LONGERON REPAIRED IAW SRM 53-02 PARA 12 FIG 18.