What was found
DURING HMV, LONGERON 2L WAS FOUND CRACKED AT BS 160 OF FUSELAGE INTERNAL STRUCTURE. DAMAGE 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, LONGERON 2L WAS FOUND CRACKED AT BS 160 OF FUSELAGE INTERNAL STRUCTURE. DAMAGE LONGERON WAS REPAIRED IAW SRM 53-02 FIG 18.