What was found
LT WING, FIXED UPPER TE PANEL BULGED, SEALANT BLOWN OUT, AND STRESSED FASTENERS, AT REAR SPAR 26-31 INCHE OTBD OF FUSELAGE. REPAIRED IAW PRI 570403-14AD, REV 0, 1, 2, 3, 4, AND ER/A 570403-14AD, REV ORIGINAL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT WING, FIXED UPPER TE PANEL BULGED, SEALANT BLOWN OUT, AND STRESSED FASTENERS, AT REAR SPAR 26-31 INCHE OTBD OF FUSELAGE. REPAIRED IAW PRI 570403-14AD, REV 0, 1, 2, 3, 4, AND ER/A 570403-14AD, REV ORIGINAL.