As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPPER AFT FUSELAGE COMPT: (AFT DOGHOUSE) RH SIDE SKIN WITH EXFOLIATION CORROSION AROUND NUTPLATE LONG. 9-11 NEAR AFT BULKHEAD BELOW WIRE HARNESS. REPAIRED AND FABRICATED DOUBLER AND INSTALLED DOUBLER ON R/H TAIL AFT BODY SECTION BETWEEN STA. 2092-STA. 2122, L-11 L-12. ALL WORK PERFORMED PER E.A.# 1-5330-T0373744, FUSELAGE-TAIL AFT BODY SECTION R/H SKIN BETWEEN STA.2092 AND 2122, L-11 AND L-12 CORROSION.