What was found
CRACK FOUND ON FUSELAGE SKIN AT UPPER AFT CORNER OF EXHAUST VLV CUT OUT. REPAIRED IAW SRM 53-20-00 FIG 2 WITH DEVIATIONS PROVIDED IN EA 8-5330-T0317819.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK FOUND ON FUSELAGE SKIN AT UPPER AFT CORNER OF EXHAUST VLV CUT OUT. REPAIRED IAW SRM 53-20-00 FIG 2 WITH DEVIATIONS PROVIDED IN EA 8-5330-T0317819.