Embraer EMB-145

Service difficulty reports · 3,003

Newest first. General aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'EMB145'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR C2XA04IA114Bulb · burned outDURING MAINTENANCE INSPECTION, THE RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Aug 31, 2004 · N13965 · Emb EMB145 · Emergency LightingSDR SIMA200423912Solenoid · malfunctionedDFW - FLT 3819 - CAPTAIN REPORTED NOSE GEAR DOOR FAILED TO CLOSE AFTER GEAR RETRACTION. INSTALLED NEW NOSE LANDING GEAR DOOR SOLENOID VALVE IAW EMB AMM 32-33-02. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) SIMAAug 23, 2004 · N613AE · Emb EMB145 · Landing Gear Retraction/Extension SystemSDR C2XA04IA105Light · inoperativeDURING POSTFLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHT LOCATED ON THE COCKPIT STEP INOPERATIVE. MAINTENANCE PERFORMED AN OPERATIONAL CHECK WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Aug 20, 2004 · N13969 · Emb EMB145 · Emergency LightingSDR RAIA00408021Connector · inoperativeEMERGENCY LIGHTS AT 12A INOPERATIVE. MAINTENANCE RESECURED ELECTRICAL CONNECTOR.Aug 17, 2004 · N801HK · Emb EMB145 · Electrical ConnectorsSDR RAIA00408017Uplock · malfunctionedGEAR WOULD NOT RETRACT. MAINTENANCE REMOVED AND REPLACED LT MAIN LANDING GEAR UPLOCK ASSEMBLY.Aug 14, 2004 · N801HK · Emb EMB145 · Landing Gear Retraction/Extension SystemSDR RAIA00408013Potentiometer · malfunctionedNOSE WHEEL STEERING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED STEERING FEEDBACK POTENTIOMETER.Aug 12, 2004 · N803HK · Emb EMB145 · Steering UnitSDR C2XA04BT084Battery Pack · failedEWR LOG SQUAWK HALF OF AISLE PATH LIGHTS OUT. REMOVED AND REPLACED NR 2 BATTERY PACK IAW EMB145 AMM 33-50-04. OPS CHECK GOOD.Aug 7, 2004 · N14974 · Emb EMB145 · Emergency LightingSDR CHQA000531Bulb · inoperativeEXTERNAL EMERGENCY EXIT LIGHT OVER RT WING IS INOPERATIVE. REMOVED AND REPLACED EXTERNAL EMERGENCY EXIT LIGHT BULB IAW 145 MM 33-50-02.Jul 27, 2004 · N378 · Emb EMB145 · Emergency LightingSDR C2XA04IA087Battery Pack · dischargedPILOT REPORTED THAT THE EMERGENCY LIGHTING DID NOT WORK WHEN TESTED DURING PREFLIGHT INSPECTION. THE ENGINES WERE RUN TO RECHARGE THE BATTERY PACKS AND AN OPERATIONAL CHECK OF THE LIGHTING SYSTEM WAS ACCOMPLISHED. THE EMERGENCY LIGHTS TESTED GOOD AND THE DISCRJul 18, 2004 · N13969 · Emb EMB145 · Emergency LightingSDR RAIA00407009Warning Light · illuminatedSERVICE DOOR OPEN WARNING MSG ILLUMINATION. DEFERRED SERVICE DOOR 52-70-00-1. SUBSEQUENTLY CLEARED DMI BY CLEANING DOOR WARNING SWITCHES.Jul 9, 2004 · N821HK · Emb EMB145 · Door Warning SystemSDR C2XA04BT074Light · faultyCREW REPORTED, EMERGENCY LIGHT (AFT) STRIP INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AFT EMERGENCY PATH LIGHT STRIP, OPS CHECKED GOOD IAW EMB145 AMM 33-50-12. AIRCRAFT RETURNED TO SERVICE.Jul 4, 2004 · N14972 · Emb EMB145 · Emergency LightingSDR C2XA04SH419Battery · dischargedSHV - DURING ROUTINE MAINTENANCE THE AISLE PATH LIGHTS 1 THRU 3 WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY IAW EMB 145 SRM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICEJul 1, 2004 · N13969 · Emb EMB145 · Emergency LightingSDR C2XA04TY108Bushing · corrodedDURING A SCHEDULED 3C INSPECTION MAINT FOUND CORRODED BUSHING ON ALL RUDDER 2 HINGE POINTS. MAINT REMOVED AND REPLACED ALL OF THE HINGE POINT BUSHINGS IAW EMB 20-10-08. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.Jul 1, 2004 · N13968 · Emb EMB145 · Rudder ActuatorSDR C2XA04TY107Bracket · corrodedDURING A SCHEDULED 3C INSPECTION CORROSION WAS FOUND ON THE SINK DRAIN BRACKETS. MAINT REMOVED THE SINK BRACKETS, FAB A NEW PART, ALODINED, PRIMED AND PAINTED AND INSTALL THE NEW BRACKET IAW EMB 13/145 SRM 51-40-02; 51-30-03; 51-21-03; 04; 05 AND 51-40-02. AJul 1, 2004 · N13968 · Emb EMB145 · Fuselage Miscellaneous StructureSDR C2XA04TY106Floorbeam · corrodedDURING A SCHEDULED 3C INSPECTION THE LEFT INBD FLOOR SUPPORT WAS FOUND CORRODED AT BOTTOM OF RAMP IN GALLEY. MAINT CUT OUT DAMAGE AND FAB A NEW REPAIR FOR THE EFFECTED AREA AND INSTALL NEW REPAIR PART IAW EMB 135/145 SRM 53-21-10; 53-21-03 AND 51-40-06 ALSO CJul 1, 2004 · N13968 · Emb EMB145 · Fuselage Main, Floor BeamSDR C2XA04TY105Frame · gougedDURING A SCHEDULED 3C INSPECTION THE BOTTOM OF THE APU FIREWALL HAD A GOUGE. MAINT FOUND THE GOUGES TO BE ON FR 81, BLENDED DYE PEEN GOUGE AREA, REMOVED RIVETS, FAB DOUBLER AND INSTALL IAW EC 5330-01352. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COJul 1, 2004 · N13968 · Emb EMB145 · APU Cowling/ContainmentSDR C2XA04TY104Floorbeam · corrodedDURING A SCHEDULED 3C INSPECTION, CORROSION WAS FOUND ON THE RIGHT LAV FLOORBEAM TOP CAP IN SEVERAL PLACES. MAINT REMOVED AND REPLACED THE RIGHT TOP CAP IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.Jul 1, 2004 · N13968 · Emb EMB145 · Fuselage Main, Floor BeamSDR C2XA04TY103Floor Support · corrodedDURING A SCHEDULED 3C INSPECTION CORROSION WAS FOUND ON LEFT SIDE LAV FLANGE. MAINT REMOVED AND REPLACED THE FLOOR SUPPORT FLANGE IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.Jul 1, 2004 · N13968 · Emb EMB145 · Fuselage Miscellaneous StructureSDR C2XA04TY102Sill · corrodedDURING A SCHEDULED 3C INSPECTION THE PAX DOOR SILL WAS FOUND CORRODED. MAINT REMOVED AND REPLACED THE DOOR SILL IAW EMB 135/145 SRM 51-40-02; 03 AND EMB CPM51-21-03. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.Jul 1, 2004 · N13968 · Emb EMB145 · Fuselage Miscellaneous StructureSDR C2XA04TY100Sill · corrodedDURING A SCHEDULED C-CHECK INSPECTION, THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. THE SILL WAS REMOVED AND REPLACED IAW EMB SRM. THE ACFT WAS SUBSEQUENTLY RELEASED FOLLOWING C-CHECK INSPECTION.Jun 29, 2004 · N13970 · Emb EMB145 · Fuselage Miscellaneous StructureSDR C2XA04TY101Floorbeam · corrodedDURING A SCHEDULED C-CHECK INSPECTION, CORROSION WAS FOUND THE FLOOR CROSSBEAM ANGLE AT FRAME 23. THE CROSSBEAM ASSEMBLY WAS REMOVED AND REPLACED IAW EMB SRM AND THE ACFT WAS SUBSEQUENTLY RELEASE FOLLOWING THE COMPLETION OF THE C- CHECK INSPECTION.Jun 29, 2004 · N13970 · Emb EMB145 · Fuselage Main, Floor BeamSDR C2XA04SH392Floorbeam · corrodedSHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 24 TO 25. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jun 26, 2004 · N13969 · Emb EMB145 · Fuselage Main, Floor BeamSDR C2XA04SH391Floorbeam · corrodedSHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 24 TO 25. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jun 26, 2004 · N13969 · Emb EMB145 · Fuselage Main, Floor BeamSDR C2XA04SH390Floorbeam · corrodedSHV - DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jun 26, 2004 · N13969 · Emb EMB145 · Fuselage Main, Floor BeamSDR RAIA00402024Wire · shorted3551- RIC - "BRAKE OTBD INOP" WARNING MESSAGE. MAINTENANCE REPAIRED SHORTED WIRING BETWEEN CONNECTORS P1044AND J1055.Jun 24, 2004 · N807HK · Emb EMB145 · Landing Gear System WiringSDR RAIA00406023Seal · deteriorated5747 - STL - BLEED 2 LEAK WARNING MESSAGE. MAINTENANCE REMOVED AND REPLACED COUPLING SEAL.Jun 24, 2004 · N821HK · Emb EMB145 · Pneumatic Distribution SystemSDR RAIA00406021Seal · deteriorated5766 - OKC - LEFT BLEED LEAK INDICATION. MAINTENANCE REMOVED AND REPLACED BLEED LINE COUPLING SEAL.Jun 23, 2004 · N821HK · Emb EMB145 · Pneumatic Distribution SystemSDR C2XA04SH386Buttstrap · corrodedSHV - DURING C-CHECK THE CENTER FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED AROUND A NUT PLATE HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5320-01127. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERJun 23, 2004 · N13969 · Emb EMB145 · Fuselage Miscellaneous StructureSDR C2XA04SH387Crossbeam · corrodedSHV - DURING C-CHECK THE CROSSMEMBER BETWEEN THE LEFT HAND SILL AND THE LEFT HAND BUTTSTRAP BETWEEN FRAMES 59 AND 60 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSMEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RJun 23, 2004 · N13969 · Emb EMB145 · Fuselage Main, StructureSDR C2XA04386Buttstrap · corrodedSHV - DURING C-CHECK THE CENTER FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED AROUND A NUT PLATE HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5320-01127. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERJun 23, 2004 · N13969 · Emb EMB145 · Fuselage Main, Floor BeamSDR C2XA04TY094Gusset · corrodedDURING A SCHEDULED 3C INSPECTION FR 22 GUSSET CAP WAS FOUND CORRODED AROUND THE RIVETS. REMOVED FR 22 GUSSET CAP, FAB A NEW CAP, ALODINED, PRIMED AND PAINTED. THEN INSTALL FAB PART IAW EMB 135/145 SRM 51-30-03; SRM 51-40-02; 03; 04. ALL WORK WAS ACCOMPLISHEJun 23, 2004 · N13968 · Emb EMB145 · Fuselage Main, StructureSDR C2XA04TY095Floorbeam · corrodedDURING A SCHEDULED 3C INSPECTION THE FWD DIGITAL HAD SMALL AREAS OF CORROSION IN THE GALLEY. PERFORMED THE REPAIR IAW EC 5320-01074. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.Jun 23, 2004 · N13970 · Emb EMB145 · Fuselage Main, Floor BeamSDR C2XA04TY093Floorbeam · corrodedDURING A SCHEDULED 3C INSPECTION, FR 23 LT OMEGA BEAM SPLICE, THE RIVETS ALONG THE AISLE SUPPORT FRAMING SHOWED EVIDENCE OF CORROSION. REMOVED AND REPLACED THE OMEGA BEAM BY SPLICE METHOD FROM FR 19 TO FR 20 IAW EC 5320-01126 AND SRM 51-40-02. ALL WORK WAS AJun 23, 2004 · N13970 · Emb EMB145 · Fuselage Main, Floor BeamSDR C2XA04TY092Bearing · wornDURING A SCHEDULED 3C INSPECTION THE RT HORIZONTAL SPHERICAL BEARING WAS FOUND WORN. REMOVED AND REPLACED THE RT SPHERICAL BEARING IAW EC 5510-01083. ALL WORK WAS ACCOMPLISHED AND THE DIEHEDRAL AND INCIDENCE CHECKS WERE ALL GOOD. A/C WILL BE RELEASED UPON CJun 23, 2004 · N13970 · Emb EMB145 · Horizontal Stabilizer StructureSDR C2XA04BT068Lever · faultyCREW REPORTED, LANDING GEAR WOULD NOT RETRACT. AIR RETURNED TO NEWARK. MAINTENANCE TROUBLESHOT LANDING GEAR SYSTEM, SWUNG LANDING GEAR SEVERAL TIMES, SERVICED NOSE STRUT, CHECKED ALL LANDING GEAR PROXIMITY SWITCHES AND ALL ITEMS OPS CHECKED GOOD. RELIABILITJun 22, 2004 · N13956 · Emb EMB145 · Landing Gear SelectorSDR C2XA04BT067Connector · disconnectedCREW REPORTED THAT THE GALLEY EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE RESECURED THE CANNON PLUG ON THE GALLEY EMERGENCY LIGHT, OPS CHECKED LIGHT GOOD. AIRCRAFT RETURNED TO SERVICE.Jun 22, 2004 · N14974 · Emb EMB145 · Electrical ConnectorsSDR C2XA04TY098Floorbeam · corrodedDURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER OMEGA BEAM AT FRAME 16. MAINTENANCE REMOVED AND REPLACED THE CENTER OMEGA BEAM IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.Jun 22, 2004 · N13968 · Emb EMB145 · Fuselage Main, Floor BeamSDR C2XA04SH385Doubler · corrodedSHV - DURING C-CHECK THE RIGHT HAND OMEGA BEAM BUTTSTRAP DOUBLERS AT FRAMES 20 AND 23 WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLERS IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jun 22, 2004 · N13969 · Emb EMB145 · Fuselage Main, Floor BeamSDR C2XA04SH384Buttstrap · corrodedSHV - DURING C-CHECK THE LEFT HAND OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 65 AND 68. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jun 22, 2004 · N13969 · Emb EMB145 · Fuselage Main, Floor BeamSDR C2XA04SH383Doubler · corrodedSHV - DURING C-CHECK THE LEFT HAND SIDE WALL DOUBLER AT FRAME 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jun 22, 2004 · N13969 · Emb EMB145 · Fuselage Miscellaneous StructureSDR C2XA04SH382Sill · corrodedSHV - DURING C-CHECK THE RIGHT HAND FLOOR SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 59 AND 60. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jun 22, 2004 · N13969 · Emb EMB145 · Fuselage Miscellaneous StructureSDR C2XA04SH381Buttstrap · corrodedSHV - DURING C-CHECK THE RIGHT HAND OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 59 AND 61. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jun 22, 2004 · N13969 · Emb EMB145 · Fuselage Main, Floor BeamSDR C2XA04SH380Sill · corrodedSHV - DURING C-CHECK THE LEFT HAND FLOOR SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 59 AND 60. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jun 22, 2004 · N13969 · Emb EMB145 · Fuselage Miscellaneous StructureSDR C2XA04SH379Sill · corrodedSHV - DURING C-CHECK THE LEFT HAND CARGO FLOOR SILL WAS FOUND TO BE CORRODED BETWEEN FRAME 60 AND FRAME 61. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jun 22, 2004 · N13969 · Emb EMB145 · Fuselage Miscellaneous StructureSDR C2XA04SH378Buttstrap · corrodedDURING C-CHECK THE CENTER BUTTSTRAP FROM FRAME 59 TO FRAME 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jun 22, 2004 · N13969 · Emb EMB145 · Fuselage Miscellaneous StructureSDR RAIA00406020Linkage · out of adjustFLAP FAIL MESSAGE AT FLAP RETRACTION. MAINTENANCE ADJUSTED FLAP MECHANICAL LINKAGE.Jun 21, 2004 · N806HK · Emb EMB145 · Trailing Edge Flap Control SystemSDR C2XA04TY097Angle · corrodedDURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE RAMP ANGLE UNDER THE CARBON FIBER BEAM AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE CENTER RAMP ANGLE IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.Jun 21, 2004 · N13968 · Emb EMB145 · Fuselage Miscellaneous StructureSDR C2XA04TY096Angle · corrodedDURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE RAMP ANGLE AND AFT NUT PLATE OF THE CENTER TOP CAP UNDER THE GALLEY FLOOR. MAINTENANCE REMOVED AND REPLACED THE CENTER TOP CAP IAW EMB SRM 51-40-02 AND 57-20-03. THE AIRCRAFT WILL BE RELEASED UPON COMPJun 21, 2004 · N13968 · Emb EMB145 · Fuselage Miscellaneous StructureSDR CX2A04RI005Lamp · burned outIAH - DURING ROUTINE INSPECTION, MAINTENANCE FOUND AFT EMERGENCY LIGHT STRIP NOT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED AFT EMERGENCY LIGHT STRIP. OPERATIONAL TESTS WERE SATISFACTORY. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.Jun 20, 2004 · N19966 · Emb EMB145 · Emergency LightingSDR C2XA04SH376Light · inoperativeSHV-DURINC CHECK THE NR 6 AISLE PROXIMITY STRIP WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP IAW EMB 145 AMM 33-50-08, THE ENSUING OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jun 19, 2004 · N14974 · Emb EMB145 · Emergency Lighting
Back to Embraer EMB-145