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 V0XR201003180002Sill · corrodedRT SILL AT FRM 29-35 IS CORRODED BEYOND LIMITS. R & R RT SILL. W/C 1078.SDR V0XR201003180001Sill · corrodedFLOOR SUPPORT ANGLE AT FRM 23 FROM Y.0.0 TO RT OTBD SILL IS CORRODED BEYOND LIMITS. R & R ANGLE. W/C 1063.SDR V0XR201003170006Sill · corrodedLT SILL AT FRM 61-65 IS CORRODED BEYOND LIMITS. R & R LT SILL. W/C 1116SDR V0XR201003170005Gusset · corrodedCTR GUSSET AT FRM 59-61 IS CORRODED BEYOND LIMITS. R & R GUSSET. W/C 1115SDR V0XR201003170004Sill · corrodedRIGHT SILL AT FRM 59-60.5 IS CORRODED BEYOND LIMITS. R & R SILL. W/C 1113SDR V0XR201003170003Gusset · corrodedGUSSET ON LT OMEGA BEAM AT FRM 29-55 IS CORRODED BEYOND LIMITS. R & R GUSSET. W/C 1077SDR V0XR201003170002Sill · corrodedPROFILE LY 0-479.0 TO LT OTBD SILL AT FRM 22 IS CORRODED BEYOND LIMITS. R & R PROFILE. W/C 1065SDR V0XR201003170001Seat Track · corrodedLT UPPER SEAT TRACK ON CTR FUSELAGE III BETWEEN FRM 30-35 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2151SDR RAIA2010031600002Connector · wornDURING TAKEOFF CLIMB, THE CREW REPORTED RECEIVING A LANDING GEAR AIR/GND FAIL MESSAGE ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE CONNECTION ON THE LT MAIN LANDING GEAR AT THE FORWARD WOW SWITCH. OPS CHECK OF THE EXTENSION AND RETRACTION SYSTEM WAS GOSDR V0XR201003160005Seat Track · corrodedLT UPPER SEAT TRACK BETWEEN FRM 24-30 CENTER FUSELAGE III IS CORRODED BEYOND LIMITS. R & R LT UPPER SEAT TRACK. W/C 2162SDR V0XR201003160004Seat Track · corrodedLT UPPER SEAT TRACK BETWEEN FRM 47-52 CTR FUSELAGE III IS CORRODED BEYOND LIMITS. R & R LT UPPER SEAT TRACK. W/C 2156SDR V0XR201003160003Seat Track · corrodedRT SEAT TRACK BETWEEN FRM 47-52 CTR FUSELAGE III IS CORRODED BEYOND LIMITS. R & R RT SEAT TRACK. W/C 2156SDR V0XR201003160002Sill · corrodedLT SILL FRM 23-29 IS CORRODED BEYOND LIMITS. R & R LT SILL. W/C 1142SDR V0XR201003160001Sill · corrodedRT SILL FRM 61-65 IS CORRODED BEYOND LIMITS. R & R RT SILL. W/C 1112SDR C2XA10IA097Ballast · overheatedIAH - FLIGHT 3027, THE CREW REPORTED AN ELECTRICAL BURNING SMELL AROUND ROW 2A. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LIGHT BALLAST AT SEAT 2A, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRASDR RAIA2010031100001Cable · out of adjustCREW REPORTED THAT THE PASSENGER DOOR WAS DIFFICULT TO OPEN FROM THE INSIDE. MAINTENANCE ADJUSTED THE DOOR CABLES IAW AMM PROCEDURES. THE DOOR OPS CHECKED GOOD.SDR C2XA10IA093Brake · malfunctionedIAH - FLIGHT 2102, THE CREW REPORTED THAT AFTER T/O, RECEIVED A FLAP FAIL MESSAGE ON EICAS WITH THE FLAP LEVER AT 0 DEGREES AND THE FLAPS AT 9 DEGREES. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT SDR V0XR201003100001Threshold · corrodedSERVICE DOOR THRESHOLD IS CORRODED BEYOND LIMITS. R & R THRESHOLD. W/C 2088SDR V0XR201003090005Seat Track · corrodedRT UPPER SEAT TRACK FR 23-30 IS CORRODED BEYOND LIMITS. R & R RT UPPER SEAT TRACK. W/C 2147SDR V0XR201003090004Seat Track · corrodedLT UPPER SEAT TRACK FR 51-57 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2156SDR V0XR201003090003Seat Track · corrodedLT UPPER SEAT TRACK FR 45-51 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2154SDR V0XR201003090002Seat Track · corrodedRT UPPER SEAT TRACK FR 30-46 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2151SDR V0XR201003090001Seat Track · corrodedRT UPPER SEAT TRACK FR 30-46 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2151SDR V0XR201003080018Seat Track · corrodedRT UPPER SEAT TRACK FRM 53-58 IS CORRODED BEYOND LIMITS. R & R RT UPPER SEAT TRACK. W/C 2157SDR V0XR201003080017Seat Track · corrodedUPPER SEAT TRACK FRM 46-52 IS CORRODED BEYOND LIMITS. R & R UPPER SEAT TRACK. W/C 2153SDR V0XR201003080016Seat Track · corrodedCTR SEAT TRACK FRM 30-35 IS CORRODED BEYOND LIMITS. R & R CTR SEAT TRACK. W/C 1124SDR V0XR201003080014Seat Track · corrodedUPPER SEAT TRACK FRM 35-45 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2152SDR V0XR201003080013Seat Track · corrodedUPPER SEAT TRACK FRM 23-29 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2149SDR V0XR201003080012Seat Track · corrodedFWD LT SEAT TRACK AT LY-479.0 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 1076SDR V0XR201003080011Profile · corrodedPROFILE FWD SIDE OF PASSENGER ENTRY DOOR FROM LY-479.0 AT FRM 16 IS CORRODED BEYOND LIMITS. R & R PROFILE. W/C 1071SDR V0XR201003080010Seat Track · corrodedLT UPPER SEAT TRACK FRM 51-57 IS CORRODED BEYOND LIMITS. R & R LT UPPER SEAT TRACK. W/C 2156SDR V0XR201003080009Seat Track · corrodedLT UPPER SEAT TRACK FRM 45-51 IS CORRODED BEYOND LIMITS. R & R LT UPPER SEAT TRACK. W/C 2154SDR V0XR201003080008Seat Track · corrodedLT UPPER SEAT TRACK FRM 29-35 IS CORRODED BEYOND LIMITS. R & R LT UPPER SEAT TRACK. W/C 2150SDR V0XR201003080007Seat Track · corrodedLT UPPER SEAT TRACK FRM 18-23 IS CORRODED BEYOND LIMITS. R & R LT UPPER SEAT TRACK. W/C 2148SDR V0XR201003080005Floor Support · corrodedOMEGA BEAM AT LY - 479.0 FRM 20 IS CORRODED BEYOND LIMITS. R & R OMEGA BEAM. W/C 1065SDR V0XR201003080004Floor Support · corrodedCTR FLOORBOARD SUPPORT ANGLE PROFILE AT LY - 479.0 FROM FRM 18.5-20 IS CORRODED BEYOND LIMITS. R & R CTR FLOORBOARD SUPPORT ANGLE PROFILE. W/C 1063SDR V0XR201003080003Floor Support · corrodedCTR FLOORBOARD SUPPORT ANGLE PROFILE AT LY-479.0 FROM FRM 18.5-20 IS CORRODED BEYOND LIMITS. R & R CTR FLOORBOARD SUPPORT ANGLE PROFILE. W/C 1063SDR V0XR201003080002Floor Support · corrodedFLOORBOARD ANGLE AT Y0.0 FROM FRM 18.5-20 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FLOORBOARD ANGLE. W/C 1062SDR V0XR201003080001Floor Support · corrodedFLOORBOARD SUPPORT AT Y0.0 FROM FRM 18.5-20 IS CORRODED BEYOND LIMITS. R & R FLOORBOARD SUPPORT. W/C 1062SDR C2XA10IA090Unknown · odorIAH - FLIGHT 2863, ON SHORT FINAL AT 11 MILES OUT THE CREW REPORTED SMELLING STRONG ELECTRICAL FUMES CAUSED BY A POSSIBLE LIGHTNING STRIKE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE PERFORMED A LIGHTNING STRIKE INSPECTION, GROUND RAN BOTH SDR C2XA10IA089Ecu · inoperativeLCH - FLIGHT 2214, THE CREW REPORTED A FLAP FAIL DURING CRUISE. THE AIRCRAFT DIVERTED TO LCH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT (FECU), OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WASDR C2XA100IA088Unknown · odorIAH - FLIGHT 2863, ON SHORT FINAL AT 11 MILES OUT THE CREW REPORTED SMELLING STRONG ELECTRICAL FUMES CAUSED BY A POSSIBLE LIGHTNING STRIKE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE PERFORMED A LIGHTNING STRIKE INSPECTION, AND GROUND RAN BSDR V0XR201003050002Channel · corrodedDOUBLERS ON RT HAT CHANNEL BEAM AT FRM 20-22 ARE CORRODED BEYOND LIMITS. R & R DOUBLER. W/C 1058SDR V0XR201003050001Seat Track · corrodedLY 479.0 SEAT TRACK FRM 24-30 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 1123SDR V0XR201003040005Profile · corrodedPROFILE FROM LY-479.0 AT FRM 18 IS CORRODED BEYOND LIMITS. R & R PROFILE.SDR V0XR201003040004Gusset · corrodedGUSSET LY 479.0-Y0.0 FROM FRM 17.5 TO 18.5 CORRODED BEYOND LIMITS. R & R GUSSET.SDR V0XR201003040003Support Angle · corrodedOTBD RT SILL SUPPORT ANGLE FROM LY 479.0 AT FRM 18.5 IS CORRODED BEYOND LIMITS. R & R SUPPORT ANGLE.SDR V0XR201003040002Gusset · corrodedGUSSET THAT COVERS CENTER RT HAT CHANNEL BEAM AT Y0.0 FROM FRM 19-23 IS CORRODED BEYOND LIMITS. R & R GUSSET. W/C 1060SDR V0XR201003040001Channel · corrodedRT HAT CHANNEL BEAM AT Y 479.0 AND SPANS FRM 18-24 IS CORRODED BEYOND LIMITS. R & R RT HAT CHANNEL BEAM.SDR V0XR201003030006Sill · corrodedLT SILL FRM 53-59 IS CORRODED AND HAS FRETTING DAMAGE. R & R LT SILL.
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