What was found
INSPECTION FOUND A 1 INCH CRACK IN AFT FUSELAGE AC SERVICING PANEL CUTOUT FLANGE. REMOVED AND REPLACED DOUBLER IAW SRM 53-34-0, FIGURE 4, SHEET 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN AFT FUSELAGE AC SERVICING PANEL CUTOUT FLANGE. REMOVED AND REPLACED DOUBLER IAW SRM 53-34-0, FIGURE 4, SHEET 1.