Embraer EMB-145ER
Service difficulty reports · 1,266
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 = 'EMB145ER' 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 = 'EMB145ER' 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 C2XA02SH121Angle · corrodedDURING C CHECK, LT FLOORBEAM RAMP ANGLE INBOARD AT FRAME 20 HAS CORROSION. MAINTENANCE REMOVED DAMAGE AND PERFORMED AN ANGLE REPAIR IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH120Strap · corrodedSHV- DURING C CHECK CENTER FLOOR BEAM STRAP AT DOUBLER WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 15 AND16. MAINTENANCE REMOVED DAMAGE AND PEFPORMED A DOUBLER REPAIR IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH119Beam · corrodedSHV-DURING C CHECK CROSS BEAM BETWEEN FRAMES 23 AND 24 FROM CENTER OMEGA BEAM T O RIGHT HAND OMEGA BEAM WAS FOUND TO HAVE CORROSION. MAITENANCE REMOVED DAMAGE AND REPLACED AFFECTED CROSS BEAM IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVISDR C2XA02SH118Sill · corrodedSHV-DURING C CHECK LEFT HAND SILL WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 23 AND 24. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH117Sill · corrodedSHV- DURING C CHECK NUTPLATES WITH CORROSION WERE FOUND JUST FOWARD OF SERVICE DOOR THRESHOLD. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED SILL IAW EMB SRM 51-20-03. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH116Support · corrodedSHV-DURING C CHECK THE SUPPORT RAMP ON CENTER OMEGA BEAM BETWEEN FRAMES 18 AND 20 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACE SUPPORT RAMP IAW EMB SRM51-20-03. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02IA232Uplock · inoperativeFLIGHT 3075, THE CREW NOTED THAT THE NOSE WHEEL WOULD NOT RETRACT, AIR RETURN TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR UPLOCK BOX, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED SDR CX2A02CL212Wire · brokenDURING ROUTINE MAINTENANCE THE NR 3 EMERGENCY FLOOR LIGHT STRIP WAS INOPERATIVE. MAINTENANCE INSPECTED AND FOUND THE LIGHT STRIP HAD BROKEN WIRES. THE LIGHT STRIP WAS REPLACED.OPERATIONAL CHECKS WERE GOOD.SDR C2XA02IA226Sensor · leakingIAH- FLIGHT 3498, THE CREW NOTED THAT #2 BLEED LEAK INFLIGHT,(FOLLOWED QRH, MX CONTROL ADVISED RETURN TO IAH), THE CREW RETURNED THE AIRCRAFT TO IAH, AND, LANDED WITHOUT INCIDENT. IAH- MAINTENANCE SECURED RIGHT WING ANTI ICE VALVE SENSOR LINE,PERFORMED A LESDR C2XA02SH115Floor Support · corrodedSHV DURING C CHECK THE CENTER OMEGA BEAM STRAP BETWEEN FRAMES 18 AND 23 WAS FOUND HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACED THE AFFECTED OMEGA BEAM STRAP IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XAO2SH114Threshold · corrodedDURING C CHECK AFT SUPPORT UNDER MAIN DOOR THRESHOLD WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED SUPPORT IAW 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH113Floorbeam · corrodedDURING C CHECK, THE CENTER FLOORBEAM AT FRAME 20 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED FLOORBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURNED TO SERVICE.SDR C2XA02SH112Frame · gougedDURING C CHECK, A GOUGE WAS FOUND ON FRAME 63 BETWEEM STRINGERS 6 AND 8. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW CONTINENTAL EXPRESS EC 5330-1200. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH111Frame · gougedDURING C CHECK, A GOUGE WAS FOUND ON FRAME 64 BETWEEM STRINGERS 6R AND 8R. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED SECTION IAW CONTINENTAL EXPRESS EC 5330-1200. THE AIRCRAFT WAS APPROVED TO RETURN SERVICE.SDR C2XA02CL207Proximity Switch · intermittentCLE FLIGHT 3292 THE CREW REPORTED A BANGING NOISE IN THE LANDING GEAR WHEELWELL ON GEAR EXTENSION.THE AIRCRAFT LANDED IN CLE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE RT MLG DOWNLOCK PROXIMITY SWITCHES. OPERATIONAL CHECKS WERE GOOD. TSDR C2XA02SH110Structure · gougedDURING C CHECK NR 1 ENG LOWER NACELLE WAS FOUND TO HAVE A GOUGE AT FORWARD OUTBOARD ATTACHEMENT. MAITENANCE REMOVED DAMAGE AREA AND REPAIRED AFFECTED EDGE MEMBER IAW EMB 145 SRM54-10-03. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH109Butt Strap · corrodedSHV-DURING C CHECK LAVARATORY'S FLOOR BEAMS WERE FOUND WITH CORROSION BETWEEN FRAMES 59 AND 61. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED BUTT STRAP IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH108Stiffener · wornDURING C CHECK NR 2 LOWER ENGINE NACELLE HAD WEAR MARKS 12 INCHES INBOARD OF CENTER. MAITENANCE REMOVED DAMAGE AREA AND PEFORMED AN ANGLE REPAIR IAW EMB SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH107Butt Strap · corrodedSHV-DURING C CHECK THE CENTER FLOOR BEAM STRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 18 AND 23. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED STRAP IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH106Structure · gougedDURING C CHECK NR 2 ENGINE LOWER NACELLE DISH AROUND INTERIOR OF ENGINE DRAIN WAS FOUND TO HAVE A GOUGE. MAINTENANCE REMOVED AND REPLACED DISH IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURNED TO SERVICESDR C2XA02SH105Floor Support · corrodedDURING C CHECK, SUPPORT UNDER PASSENGER DOOR THRESHOLD WAS FOUND WITH CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACED SUPPORT IAW EMB SRM 51-20-03. THE AIRCRAFT WAS APPROVED TO RETURN SERVICE.SDR C2XA02SH104Floorbeam · corrodedSHV- DURING C CHECK LT FLOORBEAM FOWARD OF FRAME 20 WAS FOUND WITH CORROSION. MAINTENANCE REMOVED DAMAGE AND PERFORMED AN ANGLE REPAIR IAW EMB 145 EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH103Floorbeam · corrodedSHV-DURING C CHECK SUPPORT RAMP ON CENTER FLOORBEAM BETWEEN FRAME 18 AND FRAME 20 WAS FOUND WITH CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACED SUPPORT RAMP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH102Fairing · crackedSHV- DURING C CHECK, RT FAIRING ON APU FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED RT FAIRING IAW CONTINENTAL EXPRESS EC 5350-01032. THE AIRCRAFT WAS APROVED TO RETURN TO SERVICE.SDR C2XA02SH101Floorbeam · corrodedSHV- DURING C CHECK, LT FLOORBEAM AT FRAME 20 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH100Butt Strap · corrodedDURING C CHECK, BUTT STRAP RT OF CENTER FLOORBEAM AT FRAME 18 WAS FOUND TO HAVE CORROSION ANROUND NUTPLATE HOLES. MAINTENANCE REMOVED DAMAGE AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5320-0179. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH098Floorbeam · corrodedSHV- DURING C CHECK THE CENTER FLOORBEAM WAS FOUND TO HAVE CORROSION AT FRAME 20. MAITENANCE REMOVED AND REPLACED AFFECTED FLOORBEAM IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH097Rib · gougedDURING C CHECK, NR 2 ENGINE NACELLE WAS FOUND TO HAVE A GOUGE ON THIRD RIB PLATE FROM THE END. MAINTENANCE REMOVED DAMAGE AND REPAIRED RIB PLATE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH096Stiffener · gougedDURING C CHECK, NR 1 ENGINE TOP NACELLE AFT STIFFENER 10 INCHES INBOARD OF CENTER WAS FOUND TO HAVE A GOUGED. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH095Rib · gougedDURING C CHECK INSPECTION, NR 2 ENGINE LOWER NACELLE OUTBOARD RIB WAS FOUND TO HAVE A GOUGE APPROXIMATE 4 INCHES AFT OF AFT HINGE. MAINTENANCE REMOVED DAMAGE AREA AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TOSDR C2XA02SH094Stiffener · gougedDURING C CHECK INSPECTION, NR 2 LOWER ENGINE NACELLE WAS FOUND TO HAVE A GOUGE ON AFT STIFFENER NEAR CENTER. MAINTENANCE REMOVED DAMAGE AREA AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH092Flap Track · crackedDURING C CHECK INSPECTION, RT HAND OUTBOARD FLAP CENTER TRACK WAS FOUND TO HAVE A CRACK DUE TO LIGHTING STRIKE. MAINTENANCE REPAIRED DAMAGE IAW CONTINENTAL EXPRESS EC 5750-01185. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02IA220Proximity Switch · inoperativeIAH- THE CREW NOTED THAT THE NOSE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH, AND, LANDED WITHOUT INCIDENT. IAH- MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR PROX SWITCH, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THESDR C2XA02IA219Uplock · inoperativeTHE CREW NOTED THAT THE NOSE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH, AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NLG UPLOCK BOX, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETSDR C2XA02IA218Proximity Switch · inoperativeIAH- THE CREW NOTED THAT THE NOSE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH, AND, LANDED WITHOUT INCIDENT. IAH- MAINTENANCE REMOVED AND REPLACED THE PROX SWITCH, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPRSDR C2XA02SH093Floorbeam · corrodedDURING C CHECK INSPECTION, CORROSION WAS FOUND AT CENTER FLOORBEAM SUPPORT RAMP BETWEEN FRAMES 18 AND 20. MAINTENANCE REMOVED DAMAGED SECTION, PERFORMED AN ANGLE REPAIR, AND REPLACED AFFECTED SUPPORT RAMP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVEDSDR C2XA02SH099Skin · gougedSHV-DURING C CHECK #1 ENGINE LOWER COWLING WAS FOUND TO HAVE A GOUGE ON INERIOR SKIN 24 INCHES AFT CENTER OF COWLING. MAINTENANCE REMOVED DAMAGE AREA AND PERFORMED A DOUBLER REPAIR IAW EMB SRM 54-10-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02IA217Light · inoperativeDURING POST FLIGHT THE CREW NOTED THAT THE EMERGENCY OVERHEAD LIGHTS FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA02IA216Light · inoperativeDURING POST FLIGHT THE CREW NOTED THAT THE EMERGENCY OVERHEAD LIGHTS FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND THE AIRCRAFT SDR C2XA02SH089Skin · dentedDURING C CHECK, DENT WAS FOUND ON SKIN DOUBLER JUST BELOW PANEL 113EL. MAITENANCE REMOVED DAMAGE AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-11-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH090Floorbeam · corrodedDURING C CHECK INSPECTION, LT LATERAL FLOORBEAM WAS FOUND TO HAVE CORROSION AT RE-ENFORCEMENT ANGLE BETWEEN FRAMES 19 AND 21. MAINTENANCE REMOVED DAMAGE AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 51-30-01, SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURNSDR C2XA02SH091Floorbeam · corrodedSHV- DURING C CHECK INSPECTION CENTER FLOORBEAM BUTT STRAP BETWEEN FRAMES 59 AND 61 WAS FOUND TO HAVE CORROSION ON NUTPLATES AND NUTPLATES HOLES. MAINTENANCE REMOVED AND REPLACED AFFECTED BUTTSRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TSDR C2XA02SH088Angle · gougedSHV DURING C CHECK INSPECTION GOUGE WAS FOUND ON NR 1 ENGINE LOWER COWLING AFT OF ENGINE DRAIN. MAINTENANCE REMOVED DAMAGED SETION AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH087Angle · gougedSHV DURING C CHECK INSPECTION SUPPORT ANGLE WAS FOUND GOUGED ON NR 1 ENGINE LOWER COWLING JUST AFT OF MOST FOWARD PIVOT POINT. MAINTENACE REMOVED DAMAGED AREA AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVISDR C2XA02SH086Sill · corrodedDURING C CHECK CORROSION WAS FOUND ON NUTPLATE HOLES ON LT SILL BETWEEN FRAMES 20 AND 23. MAINTENANCE REMOVED AND REPLACED AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH085Floorbeam · corrodedSHV DURING C CHECK INSPECTION, THE RT FLOORBEAM AT FRAME 20 WAS FOUND TO HAVE CORROSION AT NUTPLATE HOLES AND UNDER DOUBLER. MAINTENANCE REMOVED DAMAGED SECTION AND PERFORMED A FLOORBEAM REPAIR IAW EC 5320-01077. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICESDR C2XA02SH084Floorbeam · corrodedSHV DURING C CHECK, NUTPLATE HOLES WERE FOUND WITH CORROSION ON LT LATERAL FLOORBEAM BETWEEN FRAMES 15 AND 17. MAITENANCE REMOVED DAMAGED SECTION AND PERFORMED FLOORBEAM REPAIR IAW EC 5320-01078. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH083Bushing · damagedDURING C CHECK, ALL HAT BUSHINGS ON THE RUDDER ATTACHING BRACKETS WERE FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED ALL HAT BUSHINGS ON RUDDEDR ATTACHING BRACKETS IAW EMB AMM 20-10-08. THE AURCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH082Floorbeam · corrodedDURING C CHECK INSPECTION, RT FLOORBEAM BUTT STRAP BETWEEN FRAMES 59 AND 61 WAS FOUND TO HAVE CORROSION IN NUTPLATE HOLES. MAITENANCE REMOVED AND REPLACED AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH081Floorbeam · corrodedSHV-DURING C CHECK, LT CARGO SILL FLOORBEAM WAS FOUND TO HAVE CORROSION. MAITENANCE REMOVED AND REPLACED AFFECTED SILL FLOORBEAM IAW EMB SRM 57-220-03, SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.
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