As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LOWER FUSELAGE STATION 1010 STRINGER 30 HAS AREA OF CORROSION ON EXTERIOR. REMOVED CORROSION AREA DAMAGED BEYOND LIMITS. NDT VERIFIED ORIG MATERIAL THICKNESS TO BE .071 "MATERIAL LOSS IS .009" REMAINING MATERIAL IS .062". FABRICATED REPAIR DOUBLER AND FILLER REF SRM 53-30-3, FIG 3A/NDT MAN PART 6, 51-00-00, FIG 23, SRM 51-10-2 PG 2-7. THIS IS CLASSIFIED AS A MAJOR REPAIR.