As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE EXTERIOR RT FWD SERVICE DOOR FWD UPPER CORNER CRACKED 1/4 INCH AT STA 160.000. PERFORMED MAJOR REPAIR PER SRM 53-2-0 PG 87-88 FIG 14. CUT OUT DAMAGED AREA PER SRM 53-2-0 PG 87-88 FIG 14. FABRICATED FILLER (7075T60.063) PER SRM 53-2-0 PG 87-88 FIG 14. CLEANED TREATED AND PRIMED PER SRM 51-1-8B.INSTALLED FILLER AND DOUBLER PER SRM 53-2-0 PG 87-88 FIG 14.