As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE EXTERNAL SKIN DAMAGED AFT OF SECTION 41 AROUND STRINGER 19 LT, REMOVED DAMAGE FABRICATED REPAIR DOUBLER FILLER AND INSTALLED IAW SRM 53-30-3 FIG 24. PREP AND PAINTED AREA I.A.W. M/M 51-20-151-7. THIS IS A CLASS B REPAIR WITH AN INSPECTION THRESHOLD OF 45,000 CYCLES PER SRM 53-30-3 FIG 24