What was found
DURING HMV, E/C A21-540-01 FUSELAGE / CENTER FUSELAGE / TI-ANGLE CONNECTION / BELLY FAIRING & KEEL BEAM SIDE PANEL FR41/42 RH / CRACK - PERMANENT REPAI
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING HMV, E/C A21-540-01 FUSELAGE / CENTER FUSELAGE / TI-ANGLE CONNECTION / BELLY FAIRING & KEEL BEAM SIDE PANEL FR41/42 RH / CRACK - PERMANENT REPAI