As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LOWER FUSELAGE STA Y390 BETWEEN LONGERON 29R AND 30, EXTERNAL SKIN WITH DENT. COLD FORMED SKIN BACK TO ORIGINAL CONTOUR AT LOWER FUSELAGE STA 390 BETWEEN LONG 29R AND 30, FABBED AND INSTALLED INTERNAL REPAIR DOUBLER IAW SRM 53-04 FIG 38 VIEW G AND NDT CHECKED NO CRACKS NOTED PER NDTSPM 06-10-01.001, MATERIAL USED FOR REPAIR DOUBLER IS .032" 2024-T3 BATCH 0001500932.