Embraer EMB-145EP
Service difficulty reports · 2,197
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 = 'EMB145EP' 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.
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 = 'EMB145EP' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR V0XR201002090001Sill · corrodedLT SILL AT FRM 29-35 IS CORRODED BEYOND LIMITS. R & R SILL.SDR V0XR1002090001BSill · corrodedAFT SERVICE DOOR SILL AT FRM 22-23 IS CORRODED BEYOND LIMITS. R & R SILL.SDR C2XA10IA058Dau · defectiveXNA - FLIGHT 2660, THE CREW REPORTED A BLEED 1 LEAK IN FLIGHT THAT DID NOT GO AWAY. THE CREW SHUT DOWN THE NUMBER ONE ENGINE AS A PRECAUTION AND RETURNED TO XNA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED OPERATIONAL AND LEAK CHECKS, AND SUBSEQUESDR V0XR1002090001AAngle · corrodedANGLE AT FRM 23 YO.O - RY 780 IS CORRODED BEYOND LIMITS. R & R ANGLE.SDR V0XR201002080001Sill · corrodedLT SILL FROM FRM 18-23 IS CORRODED BEYOND LIMITS. R & R SILL.SDR RAIA2010020700001Power Supply · dischargedDURING THE PRE FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHTS AS BEING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT POWER SUPPLY IAW AMM PROCEDURES. SYSTEM OPS CHECKED GOOD FOLLOWING REPLACEMENT.SDR C2XA10IA055Clamp · defectiveIAH - FLIGHT 2069 THE CREW REPORTED A BLEED ONE LEAK DURING CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FORWARD CLAMP ON THE NUMBER ONE ENGINE BLEED VALVE. OPERATIONAL AND LEAK CHECKS WERE COMPLSDR RAIA2010020300001Light · detachedDURING THE PRE FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHT FLOOR STRIP AT ROW 1 WAS INOPERATIVE. MAINTENANCE RE-ATTACHED THE FLOOR STRIP AND PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM WITH NO DEFECTS NOTED.SDR C2XA10IA047Duct · leakingIAH - FLIGHT 2277, THE CREW REPORTED A BLEED ONE LEAK MESSAGE DURING CRUISE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT CARGO WALL "T" DUCT, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS NOTED, ASDR RAIA2010020100001Fuel Cap · looseWHILE IN CRUISE FLIGHT, THE CREW REPORTED A FUEL LEAK FROM THE RT WING FUEL CAP. MAINTENANCE INSPECTED THE CAP AND FOUND IT NOT TO BE SECURED PROPERLY. THE CAP WAS SECURED AND THE FLIGHT CONTINUED TO ITS DESTINATION.SDR RAIA2010012900001Switch · defectiveCREW REPORTED RECEIVING AN WING ANTI-ICE FAIL MESSAGE ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE WING ANTI-ICE BURST SWITCH IAW AMM PROCEDURES. SYSTEM OPS CHECKED GOOD FOLLOWING TROUBLESHOOTING AND REPAIR.SDR C2XA10IA045Light · inoperativeIAH - DURING MAINTENANCE INSPECTION THE EMERGENCY EXIT LIGHT AT ROW 12CB WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10IA041Thermostat · inoperativeIAH - FLIGHT 2413 - THE CREW REPORTED A BLEED 1 LOW TEMP DURING ICING TEST. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE BLEED THERMOSTAT, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE SDR V0XR20100127001Seat Track · corrodedFORWARD MOST LT SEAT TRACK ALONG THE SIDE WALL HAS CORROSION AROUND THE SCREWS. SEAT TRACK REMOVED AND REPLACED.SDR V0XR20100126003Seat Track · corrodedFORWARD SEAT TRACK ON LT YL 479.0 BEAM CORRODED BEYOND LIMITS. REMOVED AND REPLACED FWD SEAT TRACK.SDR V0XR20100126002Support Angle · corrodedSUPPORT ANGLE AT FRAME 59 BETWEEN Y-0 AND Y-479.0 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SUPPORT ANGLE.SDR V0XR20100126001Angle · corrodedANGLE ON LT OMEGA BEAM INBOARD FLOORBOARD LANDING ON EITHER SIDE OF FLOORBOARD CROSS SUPPORT AT FRAME 29 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED ANGLE.SDR V0XR20100125005Seat Track · corrodedSEAT TRACK YL AT 479.0 FROM FRAME 24-30 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK.SDR V0XR20100125004Gusset · corrodedGUSSET AT RT Y-439 FROM FRAME 59-61 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED GUSSET.SDR V0XR20100125003Floorboard · corrodedFLOORBOARD SILL AT LT Y-739 FRAME 61-65 HAS CORROSION BEYOND LIMITS. REMOVED AND REPLACED FLOORBOARD SILL.SDR V0XR20100125002Sill · corrodedFLOORBEAM SILL AT RT Y-739 FRAME 61-65 HAS CORROSION BEYOND LIMITS. REMOVED AND REPLACED FLOORBOARD SILL.SDR V0XR20100125001Gusset · corrodedGUSSET AT LT Y-439 FROM FRAME 59-61 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED GUSSET.SDR C2XA10IA039Duct · defectiveIAH - FLIGHT 2569, THE CREW REPORTED THAT THE PACK TWO VALVE CLOSED ON CLIMBOUT WITH NO PRESSURIZATION. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE PACK 2 EXHAUST DUCT, OPERATSDR RAIA2010012400002Wire · brokenDURING THE PRE FLIGHT INSPECTION THE CREW REPORTED THAT THE FLOOR EMERGENCY LIGHT AS BEING INOPERATIVE. MAINTENANCE INSPECTED THE LIGHT AND FOUND A BROKEN WIRE. THE WIRE WAS REPAIRED AND THE LIGHTS OPS CHECKED GOOD.SDR V0XR20100123003Doubler · corrodedRT LOWER DOUBLER AT FRAME 61 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED DOUBLER.SDR V0XR20100123002Doubler · corrodedBOTH DOUBLERS ON RT BEAM Y-479.0 AT FRAME 20-22 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED DOUBLERS.SDR V0XR20100123001Doubler · corrodedLT LOWER DOUBLER AT FRAME 61 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED DOUBLER.SDR V0XR20100122001Beam · corrodedSHORT BEAM ASSY FROM LT TRACK BEAM TO OUTBOARD AT FRAME 16 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SHORT BEAM.SDR C2XA10IA037Battery Pack · dischargedIAH - DURING MAINTENANCE INSPECTION, THE EMERGENCY LIGHTS IN THE REAR OF THE AIRCRAFT WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROSDR C2XA10IA034Clamp · looseIAH - FLIGHT 2165, THE CREW REPORTED THAT THE BLEED 1 VALVE CLOSED FROM T/O TO 10'000 FEET. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND RE-SECURED SEVERAL CLAMPS, OPERATIONAL AND LEAK CHECKS WERE ACCSDR C2XA10IA033Clamp · looseIAH - FLIGHT 2165, THE CREW REPORTED THAT THE PACK 2 VALVE CLOSED TWICE DURING CLIMB. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, RE-SECURED SEVERAL CLAMPS, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APSDR C2XA10IA031Ballast · malfunctionedDFW - FLIGHT 2324 THE CREW REPORTED A FAINT ELECTRICAL BURNING SMELL IN FLIGHT. THE AIRCRAFT LANDED AT DFW WITHOUT INCIDENT, WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED SIDEWALL LIGHTS 2A & 3A ON MEL 33-20-00/1 CAT C, AND THE AIRCRAFT WAS APPROVED FORSDR RAIA2010012100001Light · inoperativeDURING THE PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHT ABOVE THE SERVICE DOOR AS BEING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB AT THE LIGHT ASSEMBLY. OPS CHECKED GOOD.SDR RAIA2010012000002Probe · faultyDURING CLIMBOUT OF ORD, THE CREW REPORTED RECEIVING A NR 1 TAT PROP HEAT INOP MESSAGE ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE NR 1 TAT PROBE AND OPS CHECKED IT GOOD IAW AMM PROCEDURES.SDR V0XR2010011900012Gusset · corrodedGUSSET THAT SPANS OVER THE CTR BEAM TO LT BEAM FROM FRM 15.5-17 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED GUSSET.SDR V0XR2010011900011Beam · corrodedRT SIDE BEAM FROM FRM 19-25 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED BEAM.SDR V0XR2010011900010Floor Support · corrodedLT CENTRAL FUSELAGE IV OMEGA BEAM FROM FRM 58-62 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED LT OMEGA BEAM.SDR V0XR2010011900009Floor Support · corrodedPROFILE ANGLE ON LT OMEGA BEAM AT FRM 20 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED ANGLE.SDR V0XR2010011900008Profile · corrodedSHORT PROFILE IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED PROFILE. W/C 1081SDR V0XR2010011900007Sill · corrodedLT SILL BETWEEN FRM 24-29 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SILL.SDR V0XR2010011900006Seat Track · corrodedSEAT TRACK Y0.0 BETWEEN FRM 24-30 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK.SDR V0XR2010011900005Seat Track · corrodedSEAT TRACK Y 0.0 BETWEEN FRM 30-35 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK.SDR V0XR201001190005Seat Track · corrodedSEAT TRACK YL 479.0 BETWEEN FRM 30 - 35 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK.SDR V0XR20100119114Sill · corrodedFLOOR SILL AT Y-739 RT FROM FRAME 59-61 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SILL.SDR V0XR20100119113Floor Support · corrodedLT CENTRAL FUSELAGE IV OMEGA BEAM FROM FRAME 58-62 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED LT OMEGA BEAM.SDR V0XR20100119112Floor Support · corrodedRT CENTRAL FUSELAGE IV OMEGA BEAM FROM FRAME 58-62 IS CORRODED BEYOND LIMITS. REPAIRED RT OMEGA BEAM.SDR V0XR20100119111Frame · corrodedOUTBOARD PROFILE ON LT SIDE OF FRAME 61 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED PROFILE.SDR V0XR201001190004Sill · corrodedFLOOR SILL AT LT Y.739 FROM FRM 59 - 61 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SILL.SDR V0XR20100119110Frame · corrodedOUTBOARD PROFILE ON RT SIDE OF FRAME 61 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED PROFILE.SDR V0XR20100119109Sill · corrodedSERVICE DOOR SILL IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SILL.
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