Embraer EMB-145LR
Service difficulty reports · 36,797
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 SIMA20161201001Control Unit · failedWHEN GEAR SELECTED DOWN ON APPROCH, RECEIVED AN EICAS MESSAGE FOR BRAKE INBD INOPERATIVE. THE BRAKING ACTION ON THIS RUNWAY WAS SIGNIFICANTLY REDUCED. PERFORMED OPS CHECK OF THE MAIN BRAKE SYSTEM IAW AMM 32-41-00. NO DEFECT NOTED NO MESSAGES NOTED. OK FOSDR ASOA20161201007Light · inoperativeA/C WAS IN FOR A ROUTINE INSPECTION WHEN INSPECTION FOUND THE EMERGENCY STRIP AT ROLL 19 INOP. MAINTENANCE R&R THE LIGHT STRIP IAW AMM 33-50-12; OPS CHECK GOOD AND WAS RELEASED TO SERVICE.SDR ASOA20161201006Carbon Seal · wornA/C WAS DESCENDING AT 12,000 FEET WHEN A STRONG SMELL OF ENGINE OIL FROM PACKS APPEARED FROM ENGINE NR 1 SMELL CAME FROM NR 1 ENGINE BLEED ONLY. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE CARBON SEAL IAW RRMM 72-25-25. OPS CHECK WAS GOOD AND VIBE CHECKS SDR SIMA20161129004Connector · brokenEMERGENCY FLOOR STRIP BETWEEN SEAT ROW 14 AND ROW 16 HAS A BROKEN CONNECTOR. REMOVED AND REPLACED EMERGENCY FLOOR STRIP BETWEEN SEAT ROW 14 AND ROW IAW AMM 33-50-12SDR SIMA20161129003Ecu · failedFLAPS FAIL AND SPS ADVANCE ON EICAS DURING FLAP RETRACTION AFTER TAKE OFF FLAPS FAIL AT 9 DEGS. REMOVED AND REPLACED FLAP ELECTRONIC CONTROL UNIT IAW AMM 27-53-02. OPS CHECKED GOOD.SDR SIMA20161129002Flashlight · inoperativeCABIN FLASHLIGHT HAS NO RED CHARGE LIGHT. REMOVED AND REPLACED CABIN FLASH LIGHT IAW STANDARD MTX PRACTICES.SDR SIMA20161128005Skin · crackedDURING IMBV INSPECTION, QA FOUND THE FUSELAGE EXTERNAL SKIN CRACKED AROUND 1 FASTENER AT FR78 LT BETWEEN STGR 5L-6L. AIRCRAFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. INSTALLED BUSHING ON FUSELAGE EXTESDR SIMA20161128012Skin · crackedDURING IMBV INSPECTION, QA FOUND CRACKS AROUND ONE FASTENER AT FR 77 BETWEEN STGR 3R AND 4R. AIRCRAFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. PERFORMED PERMANENT REPAIR BY INSTALLING A BUSHING ON FR SDR SIMA20161128013Skin · crackedDURING IMBV INSPECTION, QA FOUND CRACKS AROUND ONE FASTENER AT FR 78 BETWEEN STGR'S 5R AND 6R. AIRCRAFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. PERFORMED PERMANENT REPAIR BY INSTALLING A BUSHING ON RSDR SIMA20161128011Trunnion · crackedRT AFT UPPER TRUNNION CRACKED. INSTALLED SERVICEABLE RT MLG AFT UPPER TRUNNION IAW ERS-EM-57MR-731.SDR SIMA20161128010Frame · chafedCHAFE ON FR 61 BETWEEN STGRS 4R-5R. PERFORMED PERMANENT REPAIR IAW ERS-EM-53MR-2442. DOUBLER P/N 145-64146-001.SDR SIMA20161128006Structure · crackedPOSSIBLE CRACK LOCATED APPROX 1" BELOW CARGO DOOR HANDLE CUTOUT. INSTALLED REPAIR DOUBLER, CARGO DOOR IAW ERS-EM-52MR-661.SDR SIMA20161128009Door Sill · corrodedCARGO DOOR ENTRANCE SILL CORRODED. R&R CARGO DOOR SILL IAW SRM 51-40-02.SDR SIMA20161128007Floor Support · corrodedCORROSION IN GALLEY AREA ON RT OMEGA BEAM FRAME 23 AT PREVIOUS REPAIR. INSTALLED DOUBLER AT RT OMEGA BEAM AT FR 23 IAW ERS-EM-53MR-2447.SDR SIMA20161128008Trunnion · crackedWHILE PERFORMING HFEC INSPECTION ON LT MLG AFT UPPER TRUNNION, FOUND TRUNNION TO BE CRACKED. FREQUENCY 400KHZ,ANGLE 130 DEGREES, H-GAIN 63.6,V-GAIN 77.6. USED EASI 6581. INSTALLED SERVICEABLE LT MLG AFT UPPER TRUNNION IAW ERS-EM-57MR-722.SDR ASOA201611283082Connector · unsecureDURING ROUTINE MAINTENANCE, THE EMERGENCY LIGHTS WERE FOUND INOPERATIVE IN THE GALLEY AND THE FIRST 3 AISLES. MAINTENANCE INSPECTED AND SECURED THE CONNECTOR ON THE NR 2 BATTERY POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD.SDR ASOA201611283081Fuse · blownDURING ROUTINE MAINTENANCE, THE RIGHT WING EMERGENCY LIGHT AND LEFT OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE FUSE IN THE NR 4 BATTERY POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD.SDR SIMA20161128001Brake · overheatedRIGHT BRAKE OVERHEAT INBD. REMOVED AND REPLACED THE NR 3 BRAKE ASSY IAW W/C 32-600-14.SDR SIMA20161127001Lamp · inoperativeRH OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RT OVERWING EMERGENCY LIGHT LAMP IAW AMM 33-50-10. OPC GOOD. NO OTHER DEFECTS NOTED.SDR SIMA20161126004Floorbeam · crackedDURING IMBV INSPECTION, QA FOUND CRACKS AROUND NUT PLATE HOLES ON LAV LT FLOORBEAM, ONE AT FR 59 AND ONE AT FR 61. AIRCRAFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. REPAIRED CRACKS AT NUT PLATE HOLES SDR SIMA20161126002Charger · failedEMERGENCY LIGHTS AT ROW 12A TO REAR INOPERATIVE REMOVED AND REPLACED THE NR 4 BATTERY AND CHARGER IAW W/C 32-700-19.SDR SIMA20161126001Sensor · failedFLAP FAILED AFTER TAKE OFF. REMOVED AND REPLACED FVS IAW AMM 27-51-12. OPS CHECKED GOOD. NO MESSAGE FOUNDSDR SIMA20161125001Cradle · brokenFA FLASHLIGHT CRADLE BROKEN. REMOVED AND REPLACED THE CRADLE IAW AMM 33-50-16-000-801-A/400 AND 33-50-16-400-801-A/400 OPS CHECKED GOOD.SDR RAIA201611240001Motor · inoperativeFLAPS FAILED IN FLT. REMOVED & REPLACED FLAP POWER DRIVE IAW AMM 27-53-04. OPS CHECK GOOD AT THIS TIME.SDR SIMA20161124002Anti-Ice Valve · failedNR 1 ENGINE ANTI ICE FAIL MESSAGE DURING PNEUMATIC INFLIGHT TEST. TURNED ICE DETECTION KNOB TO AUTO AND THE NR 1 ANTI ICE VALVE REMAINED OPEN. VALVE CLOSED AFTER SECOND ATTEMPT. SWITCHING ALL TO AUTO. PERFORMED CONTINUITY AND VOLTAGE TEST AND FUNCTIONAL TEST SDR SIMA20161124001Cradle · crackedAFT F/A FLASHLIGHT BASE CRACKED. REMOVED AND REPLACED THE FLASHLIGHT BASE IAW AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. OPS CHECKED GOOD.SDR SIMA20161123004Profile · corrodedDURING IMBV INSPECTION, QA FOUND CORROSION ON CARGO DOOR STRUCTURE UPPER NUT PLATE HOLES. AIRCRAFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. REMOVED AND REPLACED CARGO DOOR STRUCTURE UPPER NUT PLATE PROSDR SIMA20161123003Channel · corrodedDURING IMBV INSPECTION, QA FOUND CORROSION ON THE CENTER HAT BEAM AT FR 20. AIRCRAFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER IMBV INSPECTION. REMOVED AND REPLACED CENTER HAT BEAM BETWEEN FR16 AND FR23 IAW SRM 51-40-02SDR SIMA20161123001Display · failedPFD 1 CA INOP PFD1 CB D13 POPPED ELECTRIC SMOKE SMELL IN COCKPIT-C/A-FO FMD DISPLAY TRANSFERRED TO CAPTAINS PFD AND DEFERRED PER MEL 34-1 M PROCEDURES C/W. SWAPPED FO'S MFD BACK TO CAPT'S PFD. REMOVED AND REPLACED CAPT'S PFD IAW AMM/EMB 34-22-01. CAPT'S PFD SDR ASOA201611225090Unknown · odorPILOT REPORTED A STRONG SMELL FROM PACKS(MOSTLY PACK ONE)ON FLIGHT DECK. SMELLS LIKE EXHAUST FUMES, F/O GOT HEADACHE FROM IT. MX COULD NOT DUPLICATE. PACKS OPS AND SMELL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA20161122003Flashlight · inoperativeFWD FLIGHT ATTENTDANT FLASHLIGHT INOPERATIVE. REMOVED & REPLACED THE FLASHLIGHT. OPS CHECKED GOOD IAW AMM 33-50-16.SDR SIMA20161122002Skin · crackedLEFT AFT FUSELAGE FRAME 75 SKIN CRACKED ABOVE STRINGER 2L. REPAIRED THE SKIN IAW SRM 53-31-01 ITEM 11.SDR SIMA20161121007Wire · brokenLEFT NR 7 AND 9 EMERGENCY LIGHT STRIPS HAD BROKEN WIRES. REPLACED THE LIGHT STRIPS IAW AMM 33-50-12SDR SIMA20161121010Battery Pack · inoperativeNR 4 EMERGENCY LIGHT BATTERY IS DEAD. R & R THE BATTERY IAW AMM 33-50-04.SDR SIMA20161121005Frame · crackedFRAME 25 UPPER FLANGE CRACKED BETWEEN 15R AND 16R. REPAIRED THE FRAME IAW ERS-EM-53MR-2472.SDR SIMA20161121008Yoke · crackedRIGHT ENGINE FWD LOWER YOKE CRACKED. REMOVED AND REPLACED THE YOKE IAW EO EM-54MR-386SDR SIMA20161121009Frame · corrodedFRAME 65 CORRODED UNDER FWD LOWER CARGO DOOR STRIKER PLATE. FABRICATED AND INSTALLED A REPAIR ANGLE IAW SRM 53-31-04 ITEM 4E AND ERS-EM-53MR-2466SDR SIMA20161121006Door Frame · corrodedSERVICE DOOR CUTOUT AFT FRAME IS CORRODED BEHIND LOWER PLASTIC GUIDE. REPAIRED IAW ERS-EM-53MR-2479SDR ASOA201611215089Unknown · odorPILOT REPORTED ODOR OF COMBUSTION ON TAKEOFF FROM PACK/OIL BURNING SMELL. ITEM INITIALLY PLACED MEL 21-51-00-1. ON 11/25/16 MX RAN PACK NR 1 MULTIPLE TIMES AND COULD NOT DUPLICATE MEL CLEARED. A/C WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA20161121003Power Supply · inoperativeCABIN FWD AISLE EXIT LIGHTS AND RT OVERWING FWD EMERGENCY EXIT LIGHTS INOPERATIVE. NR 2 POWER SUPPY BATTERY PACK AND BATTERY POWER SUPPLY R & R IAW WORKCARD 33-70-19. OPS CHECKED GOOD.SDR SIMA20161121004Stringer · crackedSTRINGER 2L CRACKED AT FRAME 75. REPAIRED THE STRINGER IAW ERS-EM-53MR-2414.SDR HNAA2016112100354Warning Light · false activationDURING TAKEOFF, EICAS CAUTION MESSAGE HS VALVE ILLUMINATED, NR 1 ENGINE N2 WAS ABOVE 80%. MESSAGE EXTINGUISHED AFTER REJECTED TAKEOFF AND THRUST LEVERS AT IDLE. GROUND RAN AIRCRAFT. PERFORMED HIGH STAGE VALVE FUNCTION TEST IAW MM 36-11-02-700-801-A/500. OPSDR SIMA20161121002Door · unsecureCAPTAIN`S ESCAPE ROPE DOOR CAME OFF DURING TAKEOFF AND WILL NOT STAY SECURED. SECURED ESCAPE ROPE DOOR IAW STANDARD MAINTENANCE PROCEDURES.SDR ASOA201611205088Unknown · odorPILOT REPORTED A STRONG FUEL ODOR AFTER LANDING. MX PERFORMED INSPECTION OF BOTH ENGINES AND APU WITH NO LEAKS FOUND. ENGINE GROUND RUNS PERFORMED AND NO FUEL ODOR NOTED. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA20161120001Door · out of adjustAIRCREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN FROM THE OUTSIDE HANDLE. ADJUSTED THE DOOR IAW ETN EM-52-013R1.SDR SIMA20161119006Fitting · crackedDURING IMBV INSPECTION, QC FOUND LT ENGINE FWD LOWER YOKE FITTING CRACKED. AIRCRAFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER INSPECTION. REMOVED AND REPLACED LT ENGINE FWD LOWER YOKE FITTING IAW EO-EM-54MR-386. AIRCRAFSDR SIMA20161119003Frame · bentFRAME 72 IS BENT AT STRINGER 16R INSIDE CARGO. REMOVED AND REPLACED THE FRAME LOWER SECTION IAW SRM 51-40-02.SDR SIMA20161119002Flashlight · inoperativeFA FLASHLIGHT INOPERATIVE. REPLACED THE FLASHLIGHT IAW 33-50-16. OPS CHECKED GOOD.SDR SIMA20161119001Sign · inoperativeFOUND REAR LT DOOR EMERGENCY EXIT SIGN INOPERATIVE DURING PS-1 CHECK. REMOVED AND REPLACED THE SIGN IAW AMM 33-50-13. OPS CHECKED GOOD.SDR SIMA20161118009Fitting · crackedDURING IMBV INSPECTION, QC FOUND RT ENGINE FWD LOWER YOKE FITTING CRACKED. AIRCRAFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER INSPECTION. REMOVED AND REPLACED RT ENGINE FWD LOWER YOKE FITTING IAW EO-EM-54MR-386. AIRCRAF
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