What was found
FUSELAGE - SECTION 46 - BS 1640 TO 1740 LEFT SIDE AT STRINGER 34 - SKIN PANEL INSPECTION -SB 747-53A2487 R4- AD 2002-23-15. SKIN PANEL MODIFICATION AS PER EO NO.4453A036 FIG 3 AND RI NO. RI-53-60-15609 REV.A</P>)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE - SECTION 46 - BS 1640 TO 1740 LEFT SIDE AT STRINGER 34 - SKIN PANEL INSPECTION -SB 747-53A2487 R4- AD 2002-23-15. SKIN PANEL MODIFICATION AS PER EO NO.4453A036 FIG 3 AND RI NO. RI-53-60-15609 REV.A</P>)