As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK INDICATION ON FRAME 54 (2 INCH AFT SIDE) AND STGR 44 LT (2 INCH UPPER) OPEN HOLE IN AFT CARGO COMPARTMENT (1 EA) (CRACK DIRECTION 12 O CLOCK) PERFORMED REPAIR LOC. ON FRAME 54 (2 INCH AFT SIDE) AND STGR 44 LT (2 INCHES UPPER) OPEN HOLE IN AFT CARGO COMPARTMENT IAW EA 6-5316-T0359314 TITLE: FUSELAGE CENTER SECTION - JUNCTION BETWEEN LATERAL PANEL AND S-36LT AND S-44LT AT FR 54 - ALI 531582- 01 - CRACK INDICATION.