What was found
DURING HMV, A CRACK WAS FOUND ON LONGERON 4 RT BS 541 OF INTERNAL FUSELAGE STRUCTURE. LONGERON WAS REPAIRED IAW SRM 53-02 FIG 18.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING HMV, A CRACK WAS FOUND ON LONGERON 4 RT BS 541 OF INTERNAL FUSELAGE STRUCTURE. LONGERON WAS REPAIRED IAW SRM 53-02 FIG 18.