As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING HMV, TWO CRACKS WERE FOUND ON FUSELAGE SKIN AT STA 197 BETWEEN LONGERON 16-17 OF .125 INCH LENGTH AND ANOTHER BETWEEN LONGERON 12 AND 13 OF .093 INCH AT DOOR STOP. ADJUST HOLES OF THE FWD PASSENGER DOOR JAMB LT SIDE REPAIRED IAW SRM 53-05D FIG 114.