What was found
C INSPECTION, RT SIDE FUSELAGE LONGERON BOX LOWER SKIN PANEL CRACKED AND FASTENER HOLES ENLARGED. PERMANENT REPAIR ACCOMPLISHED IAW RI-53-40-10471, REV A AND EO 5330-53545-A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
C INSPECTION, RT SIDE FUSELAGE LONGERON BOX LOWER SKIN PANEL CRACKED AND FASTENER HOLES ENLARGED. PERMANENT REPAIR ACCOMPLISHED IAW RI-53-40-10471, REV A AND EO 5330-53545-A.