Service difficulty reports · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR EE4Y2025110523420Rib · corrodedDURING THE ACCOMPLISHMENT OF TASK CARD 57-50-033-1295, AZORRA AVIATION IDENTIFIED CORROSION ON THE RH WING IINBOARD FLAP RIB 1 LOWER FLANGE. THIS CONDITION WAS REPORTED ANDREPAIRED IAW ETD2025-190-925075 DTD JUL 24 2025 AND DOCUMENTED BY COOPESA COO-EO-2025-22SDR EE4Y2025110523419Rib · corrodedDURING THE ACCOMPLISHMENT OF TASK CARD 57-50-033-1295, AZORRA AVIATION IDENTIFIED CORROSION ON THE RH WING INBOARD FLAP RIB 1 LOWER FLANGE. THIS CONDITION WAS REPORTED AND REPAIRED IAWETD2025-190-925074 DTD JUL 24 2025 AND DOCUMENTED BY COOPESA COO-EO-2025-227SDR EE4Y2025100623293Inlet · dentedDURING THE STRUCTURAL INSPECTION, IT WAS FOUND P/N 341-1010-511A, S/N 1395001, AIR INLET MODULE WITH SEVERAL DENTS ON THE INNER BARREL UPPER AND LOWER ACOUSTIC PANELS. THE DENTS WERE EVALUATED AS PER SRM 71-61-01/AD53. MOST OF THE DENTS ARE BEYOND THE LIMITS FSDR EE4Y2025100623292Inlet · dentedDURING THE STRUCTURAL INSPECTION, IT WAS FOUND P/N 341-1010-509F, S/N 1192001, AIR INLET MODULE WITH SEVERAL DENTS ON THE INNER BARREL UPPER AND LOWER ACOUSTIC PANEL. THE DENTS WERE EVALUATED AS PER REF. SRM 71-61-01/AD53. MOST OF THEM ARE BEYOND THE LIMITS FOSDR EE4Y2025100623291Skin · damagedAZORRA REPORTS THAT DURING THE STRUCTURE INSPECTION, WE FOUND THE CENTER FUSELAGE I – AT FR31+380MM, S-26R+30MM EXTERNAL SKIN WITH LIGHTNING STRIKE. THE DAMAGE WAS REMOVED BY DRILLING A HOLE (Ø4.0MM). THIS CONDITION WAS REPORTED AND REPAIRED IAW ETD2025-190-92SDR EE4Y2025100623290Skin · damagedAZORRA REPORTS THAT DURING THE STRUCTURE INSPECTION, WAS FOUND THE CENTER FUSELAGE I – AT FR27+370MM, S-26R+60MM EXTERNAL SKIN WITH LIGHTNING STRIKE. THE DAMAGE WAS REMOVED BY DRILLING A HOLE (Ø4.0MM). DURING THE DOCUMENT CLOSING PROCESS, THE DAMAGE WAS LOCATESDR EE4Y2025100623289Skin · damagedDURING THE STRUCTURAL INSPECTION, IT WAS FOUND ON FORWARD FUSELAGE, AT FR18+18MM AND STGR-26R+85MM, EXTERNAL SKIN WITH A LIGHTNING STRIKE DAMAGE. EVALUATED THOUGH DAMAGE AND FOUND OUT OF LIMITS IAW ERJ190, PART II SRM 53-10-01, AD53, PARAGRAPH 4.B.(3): THE DISSDR EE4Y2025100623287Skin · scratchedDURING THE STRUCTURAL INSPECTION IT WAS FOUND ON FORWARD FUSELAGE, RH-LATERAL SEAT TRACK FROM FR19 TO FR20 OTBD CROWN AREA WITH SCRATCH. EVALUATED BLEND OUT AREAS AND FOUND OUT OF LIMITS PER ERJ190, PART II SRM 53-10-10, AD51, PARAGRAPH 4.B. (NO DAMAGES AREA ASDR EE4Y2025091723170Skin · damagedDURING STRUCTURE INSPECTION, FOUND FWD FUSELAGE, FR 18+50MM, & S27L + 155MM (JUST 8.0MM FROM STR 28L FASTENER ROW), EXTERNAL SKIN WITH LIGHTNING STRIKE WITH EXISTING BLEND OUT. BLEND OUT WAS EVALUATED & CLASSIFIED AS NON-SIGNIFICANT IAW SRM 51-75-16. LIGHTNSDR EE4Y2025091723168Skin · damagedCENTER FUSELAGE I SKIN HAS A LIGHTNING STRIKE DAMAGE AT FRAME 30+290MM AND STRINGER 27R. SEE FIGURE 1. THE DAMAGE WAS REMOVED BY BLENDING AND WAS FOUND BEYOND LIMITS PER SRM 53-21-01/AD 51. SINCE THE DAMAGE IS LOCATED IN THE NOT ALLOWED REPAIR AREA (GREY AREA)SDR EE4Y2025091723167Heat Shield · misrepairedDURING THE STRUCTURE INSPECTION, AN EXISTING REPAIR WAS FOUND INSTALLED WITHOUT RECORDS AT RH ENGINE PYLON HEAT SHIELD BAY #8. DUE TO THIS FACT, THE REPAIR WAS REMOVED. THIS CONDITION WAS REPORTED AND REPAIRED IAW ETD2025-190-926307 DTD AUG 08 2025 AND DOCUMENSDR EE4Y2025091723166Seat · corruptedPER CUSTOMER REQUEST, PASSENGER CABIN SEATS DIAPHRAGMS 41191032-35, 41191032-36, 41191032-37, 41191032-38 WERE FOUND WITH CRACKS AND MUST BE REPAIRED.THE CONDITION REPORTED WAS REPAIRED IAW ETD2025-190-924987 REV. B, AND COOPESA COO-EO-2025-23053,