Service difficulty reports · 77
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR EE4Y2026030924077Rib · corrodedDURING A STRUCTURAL INSPECTION, CORROSION WAS FOUND AT A FASTENER HOLE LOCATED ON THE LH WINGLET LOWER SURFACE, AT THE SUPPORT STRUCTURE OF ACCESS PANEL 551AB, SEE FIGURE 1 FOR DAMAGE OVERVIEW. THE AFFECTED FASTENER HOLE INVOLVES BOTH THE WING SPAR II AND WINGSDR EE4Y2026030924076Skin · damagedCUSTOMER REPORTS TWO LIGHTNING STRIKE DAMAGES AFFECTING THE CENTER FUSELAGE I SKIN, LOCATED AT FR33 + 242 MM (DAMAGE #1) AND FR33 + 394 MM (DAMAGE #2) ON STR 26L. DAMAGE #1 WAS COMPLETELY REMOVED BY BLEND-OUT. DAMAGE #2, DEPTH EXCEEDED 50% OF THE SKIN THICKNESSDR EE4Y2026030924075Skin · damagedDURING THE STRUCTURAL INSPECTION, DAMAGE CAUSED BY A LIGHTNING STRIKE WAS FOUND ON THE EXTERNAL SKIN OF THE CENTER FUSELAGE I, AT FR24 + 327MM, STR-27LH + 8MM. AFTER PERFORMING A LIGHT BLEND-OUT, IT WAS DETERMINED THAT IN A POINT, THE DAMAGE EXCEEDED 50% OF TH
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