What was found
LOWER FUSELAGE, CENTER CARGO DOOR, SUSPECTED CRACK ADJACENT TO ACTUATOR ARM LINK. REPAIRED IAW SRM 52-00-01, VOL I, FIG 9, SHT 6, PG 47 &48.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LOWER FUSELAGE, CENTER CARGO DOOR, SUSPECTED CRACK ADJACENT TO ACTUATOR ARM LINK. REPAIRED IAW SRM 52-00-01, VOL I, FIG 9, SHT 6, PG 47 &48.