Embraer EMB-145LR
Service difficulty reports · 36,799
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 = 'EMB145LR' 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 = 'EMB145LR' 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 CHQA20140515158Floor Support · corrodedDURING INSPECTION, THE CTR OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. THE FRAME WAS REPAIRED IAW SRM 51-40-02.SDR RAIA201405150001Warning Message · false activationBLEED 1 LEAK IN CLEAR ABOVE THE CLOUDS DURING CLIMB, RETURNED TO BLOCK. MAINTENANCE INSPECTED AND REPLACED SEVERAL BLEED DUCT SEALS, LEAK AND OPS CHECKED GOOD.SDR SIMA20140515005Structure · crackedACCESS DOOR 272DR STRUCTURE IS CRACKED UNDER PIP PIN EYELE. PERFORMED REPAIR TO ACCESS DOOR 272DR STRUCTURE IAW ERS-EM-52MR-135.SDR SIMA20140515002Sensor · faultyFLAP FAIL, TRANSFERRED TO NRWC 616-ORD-02038. TROUBLE SHOT & FOUND LT FLAP VELOCITY SENSOR MOUNTING SCREWS LOOSE & ALSO FAILED WIRING CHECKS. R & R LT FLAP VELOCITY SENSOR IAW MM 27-51-12. OPERATIONS CHECKED GOOD IAW MM 27-51-00.SDR SIMA20140515004Charger · inoperativeEMERGENCY LIGHT STRIP & RT & LT OVERWING LIGHTS INOPERATIVE. R & R NR 4 BATTERY CHARGER & THE BATTERY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD AT THIS TIME.SDR SIMA20140515001Flap · malfunctionedFLAP FAIL, TROUBLE SHOT IAW FIM TASK 27-51-00-810-816-A. TRANSITORY COND OF FLAP CONTROL SYS. OPERATIONS CHECKED GOOD IAW AMM 27-51-00-700-801A.SDR CHQA20140514173Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LT OMEGA BEAM AT FRAME 20. THE FRAME WAS REPLACED IAW SRM 53-0010 & SRM 51-40-02.SDR CHQA20140514162Floor Support · corrodedDURING INSPECTION, THE CTR OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 59 & 60. THE BEAM WAS REPAIRED IAW ETD 2014-145-040625.SDR CHQA20140514157Frame · crackedDURING INSPECTION, FRAME 23 AT STRINGER 15L WAS FOUND TO BE CRACKED. FRAME 23 WAS REPAIRED IAW SRM 53-00-04.SDR RAIA201405140001Thermostat · malfunctionedBLEED NR 2 OVERTEMP ILLUMINATED DURING CLIMB OUT WITH BLEED 1 LEAK ON EICAS, ACFT RETURNED TO BLOCK. MAINTENANCE INSPECTED, OPS CHECK BLEED LEAK AND OPS CHECK GOOD AND REPLACED THE NR 2 BLEED THERMOSTAT, OPS CHECKED GOOD.SDR SIMA20140514011Wire · brokenSERVICE DOOR EMERGENCY LIGHT INOPERATIVE. R & R OF EMERGENCY LIGHT ASSEMBLY IAW TASK 33-50-09-000-802-A, A BROKEN WIRE WAS DISCOVERED, REPLACED FEMALE CONNECTOR & MALE PLASTIC COVER IAW WM 33-50-00. OPS CHECKED GOOD.SDR SIMA20140514006Flashlight · inoperativeFIRST OFFICER'S FLASHLIGHT DEAD. R & R FIRST OFFICER'S FLASHLIGHT IAW AMM 33-50-16, OPERATIONS CHECKED GOOD.SDR SIMA20140514010Light · inoperativeFWD CEILING EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT IAW AMM 33-50-08, OPERATIONS CHECKED GOOD.SDR SIMA20140514002Flashlight · inoperativeCABIN FLASHLIGHT STOPPED FLASHING AT 18B. R & R RECHARGEABLE FLASHLIGHT AT 18B IAW AMM 33-51-01, OPERATIONS CHECKED NORMALLY.SDR SIMA20140514007Nut Plate · brokenLEFT FWD EXTERNAL EMERGENCY LIGHT ASSEMBLY HAS BROKEN NUTPLATES. R & R LT FWD EXTERNAL EMERGENCY LIGHT ASSEMBLY IAW AMM 33-50-10, OPERATIONS CHECKED GOOD.SDR SIMA20140514008Battery · dischargedLEFT FWD WING EXT EMERGENCY LIGHT INOPERATIVE. AFTER T/S R & R NR 1 EMERGENCY LIGHT CHARGER & BATTERY IAW WC 33-700-19. OPERATIONS CHECKED GOOD IAW WC 33-700-17.SDR ASOA20140515064Control Panel · inoperativeDURING CRUISE, THE AIRCREW RECEIVED AN EICAS MESSAGE THAT THE EMERGENCY LIGHTS WERE NOT ARMED. MAINTENANCE R & R THE F/A LIGHTING CONTROL PANEL. THE EMERGENCY LIGHTING SYSTEM OPS CHECKED GOOD. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140513070HModule · inoperativeTHE CREW REPORTED AN EMERGENCY LIGHTS NOT ARMED EICAS MESSAGE IN FLIGHT. ACFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ACFT AND R & R THE OVERHEAD LIGHT CONTROL MODULE, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA20140513001Light · inoperativeAISLE OVERHEAD EMERGENCY LIGHT AT SEAT 17 AB INOPERATIVE. R & R AISLE OVERHEAD EMERGENCY LIGHT LAMP AT SEAT 17 AB IAW AMM 33-50-10, OPERATIONS CHECKED GOOD.SDR ASOA20140513063Stringer · crackedDURING C-CHECK STRINGER 6R WAS FOUND TO BE CRACKED BETWEEN FRAME 12-13. MAINTENANCE R & R THE STRINGER IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140513062Bracket · gougedDURING C-CHECK THE LT WINDSHIELD PILLAR BRACKET AT FRAME 10, STRINGER 5L, WAS FOUND TO BE GOUGED. MAINTENANCE R & R THE BRACKET IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140513061Skin · corrodedDURING C-CHECK THE CENTRAL FUSELAGE LOWER SKIN WAS FOUND TO BE CORRODED AT FRAME 21, STRINGERS 21L AND 21R. MAINTENANCE R & R THE SKIN IAW EC5330-02895. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140513060VShear Tie · corrodedDURING C-CHECK THE CARGO DOOR CUTOUT FWD SHEAR TIE WAS FOUND TO BE CORRODED AT FRAME 65, STRINGERS 15L-16L. MAINTENANCE R & R THE SHEAR CLIP IAW SRM 53-31-04. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140513059Fitting · crackedDURING C-CHECK THE NR 2 ENGINE FORWARD LOWER YOKE FITTING WAS FOUND TO BE CRACKED AND VERIFIED WITH EDDY CURRENT. MAINTENANCE R & R THE FITTING IAW EC5450-01088. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR CHQA20140512161Fitting · damagedDURING INSPECTION, THE LT AILERON PCA ROD END ATTACH FITTING ON THE AILERON OTBD ROD INBD HAT BUSHING WAS FOUND TO BE MIGRATED OUTWARD. THE LT AILERON PCA ROD END ATTACH FITTING WAS REPLACED IAW SRM 51-40-02, 51-20-03 & CPM 51-21-04.SDR CHQA20150512160Fitting · damagedDURING INSPECTION, THE RT AILERON DAMPER ROD END ATTACH FITTING WAS ON THE AILERON INBD HAT BUSHING WAS FOUND TO BE MIGRATED OUT. THE FITTING WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140512159Fitting · gougedDURING INSPECTION, THE LT AILERON DAMPNER ROD END FITTING WAS FOUND TO BE GOUGED ON THE INBD SIDE. THE LT AILERON DAMPNER ROD END FITTING WAS REPLACED IAW SRM 51-60-02.SDR CHQA20140512156Hinge Fitting · damagedDURING INSPECTION, THE RT AILERON OTBD HINGE ATTACH FITTING ON THE AILERON HAT BUSHING WAS FOUND TO BE MIGRATED & THE INBD SIDE HOLE ELONGATED. THE RT AILERON OTBD HINGE FITTING WAS REPLACED IAW SRM 51-40-02.SDR SIMA20140512004Switch · inoperativeBLEED 2 VLV FAIL. R & R BLEED 2 PUSH BUTTON IAW AMM 20-13-04, OPERATIONS CHECK OF E2 BLEED VLV GOOD IAW AMM 36-11-05.SDR ASOA20140512054Control Unit · malfunctionedPILOT REPORTED DURING LANDING, LOST ALL NORMAL BRAKING. CREW WAS ABLE TO SLOW ACFT WITH THRUST REVERSERS. RECEIVED BRAKE DEGRADED EICAS MESSAGE AND BRAKING RETURNED TO NORMAL. MAINTENANCE R & R BRAKE CONTROL UNIT WITH OPS CHECK AND HIGH SPEED TAXI CHECKS GOSDR SIMA20140512001Inverter · inoperativeAFT EMER FLOOR LIGHTS INOPERATIVE. R & R NR 4 EMER LIGHT INVERTER IAW AMM 33-50-11.SDR CHQA20140511147Skin · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LOWER AIRSTAIR DOOR SKIN. THE DOOR WAS REPAIRED IAW ETD2014-145-039320.SDR SIMA20140511004Battery Pack · dischargedEMERGENCY LIGHTS HAD BEEN LEFT ON. FRONT 2/3 OF AISLE LIGHTS DO NOT WORK. R & R EMERGENCY LIGHTING BATTERY PACKS NR 1, 2 & 3 IAW AMM 33-50-04. OPERATIONS CHECKED NORMALLY IAW AMM 33-50-00. NR 2 PN 2013-1A & SN 67267.SDR SIMA20140511003Battery · dischargedPAX DOOR EMERGENCY LIGHT, OVERHEAD BY COCKPIT DOOR EMERGENCY LIGHT & LT WING LATERAL PANEL EMERGENCY LIGHT INOPERATIVE. R & R BATTERY POWER SUPPLY & BATTERY FOR NR 1 EMERGENCY SYS IAW AMM 33-50-04 & REPLACED LT WING EMERGENCY LIGHT BULB IAW AMM 33-50-10. OPESDR SIMA20140511001Light · inoperativeOVERWING AFT EMERGENCY LIGHT INOPERATIVE. R & R OVERWING AFT EMERGENCY LIGHT LAMP, OPERATIONS CHECK GOOD IAW AMM 33-50-10.SDR CHQA20140510174Floor Support · corrodedDURING INSPECTION, THE RT OMEGA BEAM REPAIR AT FRAME 23 HAS CORROSION. THE REPAIR DOUBLER WAS REPLACED IAW ETD 2014-145-041404.SDR CHQA20140510168Floor Support · corrodedDURING INSPECTION, THE LT OMEGA BEAM CTR FLOOR FLANGE WAS FOUND TO BE CORRODED AT FRAME 24 & FRAME 25. THE BEAM WAS REPAIRED IAW SRM 53-00-10 & 51-40-02.SDR CHQA20140510166Angle · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE MAIN ENTRY DOOR STRUCTURE AT THE MID FWD FRAME & STRINGER 12L. THE Z RIB & L ANGLE WERE REPLACED IAW SRM 51-40-02.SDR CHQA20140510165Rib · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE MAIN ENTRY DOOR STRUCTURE AT THE MID FWD FRAME & STRINGER 12L. THE Z RIB & L ANGLE WERE REPLACED IAW SRM 51-40-02.SDR CHQA20140510164Profile · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE MAIN ENTRY DOOR STRUCTURE AT THE MID FWD FRAME & MID FRAME AT STRINGER 14L. THE FRAME PROFILE WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140510163Profile · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE MAIN ENTRY DOOR STRUCTURE AT THE MID FWD FRAME & STRINGER 15L. THE FRAME PROFILE WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140510155Fitting · crackedDURING INSPECTION, THE SHEAR CLIP AT FRAME 28 BETWEEN STRINGERS 15R & 16R WERE FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.SDR RAIA201405100001Bulb · inoperativePASSENGER DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED BULB, OPS CHECK GOOD.SDR SIMA20140510005Power Supply · inoperativeLT & RT OVER THE WING EMERGENCY LIGHT INOPERATIVE. R & R NR 4 EMERGENCY LIGHT POWER SUPPLY ASSEMBLY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD AT THIS TIME.SDR SIMA20140510003Wire · damagedFLOOR EMERGENCY LIGHT PROX STRIP AT ROW 18 HAS A DAMAGED WIRE. R & R, OPERATIONS CHECKED EMERGENCY LIGHTS PROX STRIP AT ROW 18 IAW AMM 33-50-12, OPERATIONS CHECKED GOOD.SDR SIMA20140510001Adc · failedADC1 FAIL IN FLIGHT RED X OVER AIRSPEED ALTITUDE & RED VS REVERSIONARY WORKED FINE. R & R NR 1 COMPUTER MICRO AIR DATA, OPERATIONS CHECKED GOOD IAW AMM 34-15-01.SDR CHQA20140509172Profile · corrodedDURING INSPECTION, A CRACK WAS FOUND ON THE STRUCTURE UNDER THE MIDDLE FWD STEP SUPPORT BRACKET ON THE MAIN ENTRY DOOR. THE PROFILE WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140509171Profile · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE MAIN ENTRY DOOR STRUCTURE AT THE AFT FRAME & STRINGER 10L. THE PROFILE WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140509169Door Frame · corrodedDURING INSPECTION, THE MAIN ENTRY DOOR STRUCTURE AT THE MID AFT FRAME & STRINGER 14 WAS FOUND TO BE CORRODED. THE MID AFT FRAME WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140509167Profile · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE STRUCTURE OF THE MAIN ENTRY DOOR AT THE AFT FRAME AT STRINGER 12L. THE FRAME PROFILE WAS REPLACED IAW SRM 51-40-02.
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