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 CHQA20120906311Skin Splice · corrodedDURING INSPECTION, CORROSION WAS FOUND IN THE CIRCUMFERENTIAL SKIN SPLICE BETWEEN FRAMES 14 AND 16 AND STRINGERS 21L TO 20R. THE SKIN SPLICE WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-02.SDR CHQA20120906307Carbon Seal · leakingCREW REPORTED THAT THEY RECEIVED A LAVATORY SMOKE INDICATION AFTER TAKE-OFF. CREW ALSO REPORTED THAT THERE WAS NO SMOKE OR ODOR PRESENT IN THE CABIN OR COCKPIT AND THE MESSAGE CLEARED BEFORE LANDING. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENTSDR SIMA20120906004Unknown · odorON FLIGHT 3248 - THE CREW REPORTED A BAD ODOR IN THE COCKPIT AND WAS UNABLE TO DETERMINE THE ORGIN. ODOR MIGHT BE THE FLIGHT CREW SEAT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED DETAILED VISUAL INSPECTION OF THE FLIGHT COMPARTMENT. RAN PACKS, NO BADSDR SIMA20120906002Connector · looseDURING B INSPECTION FOUND THE ABOVE WING TO FUSELAGE EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. TIGHTEN CONNECTOR ON EMERGENCY LIGHT ASSEMBLY ABOVE WING TO FUSELAGE PANEL IAW EMB 145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THESDR SIMA20120806019Strip · damagedDURING MAINTENANCE INSPECTION FOUND THE LEFT EMERGENCY LIGHT STRIP EXTRUSION NR 1, 8 AND 7 DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT EMERGENCY LIGHT STRIP EXTRUSION NR 1, 8 AND 7 IAW EMB 145 ZMM 33-50-12. THE AIRCRAFT WASSDR SIMA20120806014Sill · corrodedDURING B INSPECTION FOUND THE RIGHT NR 2 FLOOR SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT NR 2 FLOOR SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20120906001Flashlight · inoperativeON FLIGHT 4269 THE CREW REPORTED THE AFT FLIGHT ATTENDANT FLASHLIGHT WILL NOT CHARGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRSDR SIMA20120905003Light · inoperativeDURING B INSPECTION FOUND THE GALLEY CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE GALLEY OVERHEAD SERVICE DOOR EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. THE AIRCRAFSDR ASOA20120905137Torque Box · gougedHE RT WING TORQUE BOX BOLT HOLE WAS GOUGED. A TEMPORARY REPAIR WAS DONE AND PLACED ON A DMI TO PERFORM A PERMANENT REPAIR WITHIN 300 F/C STARTING 05/21/12 IAW ETD 2012-145-005036. MX REAMED THE RT WING TORQUE BOX HOLE ON THE INBD SIDE TO 9.662 MM IAW EC 571SDR CHQA20120904320Stringer · corrodedDURING INSPECTION, CORROSION WAS FOUND ON STRINGER 21R FROM FRAME 8 TO FRAME 13. THE STRINGER 21R AT FRAME 8 TO FRAME 13 WAS REPLACED IN ACCORDANCE WITH SRM 51-20-02.SDR CHQA20120904317Web · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT WEB ASSEMBLY BETWEEN FRAMES 12 AND 13. THE RIGHT WEB ASSEMBLY BETWEEN FRAMES 12 AND 13 WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20120904319Stanchion · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT STANCHION AT FRAMES 11 AND 12. THE RIGHT STANCHION BETWEEN FRAMES 11 AND 12 WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20120904318Stanchion · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT STANCHION AT FRAMES 12 AND 13. THE RIGHT STANCHION BETWEEN FRAMES 12 AND 13 WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20120904316Web · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT WEB ASSEMBLY BETWEEN FRAMES 11 AND 12. THE RIGHT WEB ASSEMBLY BETWEEN FRAMES 11 AND 12 WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20120904306Smoke Detector · false activationCREW REPORTED A LAVATORY SMOKE INDICATION ON THE EICAS. THE FLIGHT CREW FURTHER REPORTED THAT NO SMOKE WAS OBSERVED AND THERE WAS NO SMELL OF SMOKE IN THE CABIN OR COCKPIT. THE INDICATION CLEARED ITSELF AND THE AIRCRAFT RETURNED TO FIELD. MAINTENANCE REPLACSDR SIMA20120904005Ecu · malfunctionedON FLIGHT 4204 THE CREW REPORTED THAT UPON LANDING AND CLEARING RUNWAY WENT TO RAISE THE FLAPS AND GOT A FLAP FAIL AND SPS ADVANCED EICAS MSG. FLAPS WERE STUCK AT 22 DEGREES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLAP ELECTRONIC COSDR SIMA20120904004Door · lack of lubeFOR FLIGHT 3543 THE FLIGHT ATTENDANT REPORTED THE MAIN DOOR WAS DIFFICULT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED MAIN PASSENGER DOOR IAW EMB 145 AMM 52-18-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20120904002Unknown · malfunctionedON FLIGHT 4202 THE CREW REPORTED THE REAR FLASHLIGHT HOLDER RED CHARGE LIGHT WAS INTERMITTENT WHEN IN THE CRADLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. DEFERRED AFT FLASHLIGHT PER 25-53. PERFORMED OPERATIONAL CHECK OF EMERGENCY FLASHLIGHTS. NO DEFECTS FOUSDR SIMA20120904001Cradle · brokenON FLIGHT 4138 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT CRADLE WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT ASSEMBLY PER EMB 145 AMM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR CHQA20120903345Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT OMEGA BEAM AT FRAME 23. THE RIGHT OMEGA BEAM AT FRAME 23 WAS REPAIRED IN ACCORDANCE WITH SRM 53-21-10.SDR ASOA20120903075Starter Gen · shortedAPU FIRE INDICATION ON EICAS AT GATE. CREW DISCHARGED APU FIRE EXTINGUISHER. MX PERFORMED APU FIRE WARNING INSPECTION AND FOUND FIRE TO BE LIMITED TO APU STARTER GENERATOR AND ASSOCIATED DUCTING AND OUTLET SCOOP. APU PLACED ON MEL. ACFT APPROVED FOR RETURN TOSDR SIMA20120903001Battery · dischargedDURING B INSPECTION FOUND THE FORWARD EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY POWER SUPPLY AND BATTERY IAW AE W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SESDR SIMA20120829007Frame · chafedDURING INSPECTION QC DISCOVERED A CHAFE ON FRAME 65 BETWEEN STRINGERS 12R AND 13R. THE AIRCRAFT WAS REMOVED FROM SERVICE. DOUBLER INSTALLED IAW EO EM-53MR-2020. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR RAIA201209020002Valve · defectiveDURING CRUISE, BLEED NR 1 OVERTEMP APPEARED. THE CREW RETURNED THE A/C TO STL. MAINTENANCE INSPECTED AND REPLACED NR 1 FAN AIR VALVE, OPS CHECK GOOD.SDR RAIA201209020001Warning System · false activationDURING CRUISE, THE PACK NR 2 OVERLOAD MSG APPEARED, PACK NR 2 VALVE CLOSED. THE CREW RETURNED A/C TO STL. MAINTENANCE PERFORMED OPS CHECK OF PACK NR 2, OPS CHECK GOOD.SDR SIMA20120901014Frame · crackedREAR ELECTRONICS COMPARTMENT ACCESS HATCH 272DR INNER FRAME CRACKED AT HINGE PIN FITTING. REPAIRED REAR ELECTRONICS COMPARTMENT ACCESS HATCH 272DR IAW EO-EM-52MR-325.SDR SIMA20120901013Shear Tie · corrodedSHEAR TIE AT FRAME 65 CORRODED ABOVE STRINGER 18L. REPAIRED SHEAR TIE IAW EO EM-53MR-1129.SDR SIMA20120901015Floor Support · corrodedRT GALLEY OMEGA BEAM CORRODED AFT OF FR-18 AT SCREW HOLE. REPAIRED OMEGA BEAM IAW AE EO EM-53MR-2022.SDR SIMA20120901006Display · failedON FLIGHT 3244 THE CREW REPORTED THE EICAS WENT BLACK THEN SMOKE WAS COMING OUT OF DASH. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S MFD IAW EMB 145 AMM 34-22-01 OPC GOOD IAW EMB 145 AMM 34-22-00. THE AIRCRAFT WAS RETURNESDR SIMA20120901012Light · inoperativeDURING MAINTENANCE INSPECTION FOUND THE NR 1 EMERGENCY LIGHT FLOOR STRIP INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT STRIP IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURSDR SIMA20120901011Floor Support · crackedDURING MAINTENANCE INSPECTION FOUND THE RIGHT OMEGA BEAM FRAME BETWEEN 47 AND 48 LOWER FLANGE CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OMEGA BEAM FRAME BETWEEN 47 AND 48 LOWER FLANGE IAW EMB SRM 53-23-02 AND 51-40-02. TSDR SIMA20120901010Floor Support · corrodedDURING MAINTENANCE INSPECTION, FOUND RIGHT GALLEY OMEGA BEAM CORRODED AFT OF NR 18 SCREW HOLE. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED EO-EM-53MR-2022. AIRCRAFT RETURNED TO SERVICE.SDR ASOA20120901072Light · odorREPORTED BURNING ODOR FROM CABIN LIGHT OVER 11A SIDEWALL LIGHT. MX R & R CEILING LIGHT ASSY OVER 11A WITH OPS CHECK SUCCESSFUL. ACFT APPROVED FOR RETURN TO SERVICE.SDR SIMA20120901005Flashlight · defectiveDURING MAINTENANCE INSPECTION FOUND THAT THE CAPTAIN'S FLASHLIGHT WOULD NOT CHARGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT ASSEMBLY IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETSDR SIMA20120901001Yoke · crackedDURING MAINTENANCE INSPECTION FOUND THE LEFT ENGINE LOWER FORWARD YOKE CRACKED FORWARD OF ENGINE MOUNT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED LEFT ENGINE LOWER FORWARD YOKE FORWARD OF ENGINE MOUNT IAW EO EM-54MR-386. THE AIRCRAFT WAS RETURNED TO SSDR CHQA20120831304Light · inoperativeDURING INSPECTION, THE LEFT AFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE RELAMPED THE LEFT AFT OVERWING EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR SIMA20120831007Battery · defectiveDURING MAINTENANCE INSPECTION FOUND THE BATTERY VOLTAGE PROPS RAPIDLY BELOW 23.5 VOLTS AS SOON AS GENERATOR POWER IS SHUTDOWN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BATTERY 1 AND 2 IAW WC 24-600-00. THE OPERATIONAL CHECK WAS GOOD. THESDR SIMA20120831006Hinge · out of adjustON FLIGHT 3309 THE CREW REPORTED THE MAIN CABIN DOOR WAS VERY HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. ADJUSTED MAIN DOOR SIDE HINGE IAW ETN #EM-52-013R1. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20120831005Light · inoperativeDURING B INSPECTION FOUND THE MAIN DOOR HINGE EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR EMERGENCY LIGHT IAW EMB AMM TASK: 33-50-10-000-801-A, AND 33-50-10-400-801-A. THE OPERATIONAL CHECK WAS GOOD.SDR SIMA20120831004Light · inoperativeDURING B INSPECTION FOUND THE EMERGENCY FLOOR LIGHT STRIP AT SEAT 1A INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED 1A FLOOR PROXIMITY STRIP IAW EMB AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD PER WC 33-700-17. THE AIRCRAFT WAS RETURNED TO SSDR SIMA20120831002Battery Pack · unserviceableFOR FLIGHT 3546 THE CREW REPORTED THAT WHEN THEY ARRIVED AT THE AIRCRAFT THE EMERGENCY LIGHTS WERE ON. THE AIRCRAFT HAD BEEN UNOCCUPIED FOR AT LEAST 25 MINUTES AND COULD NOT DETERMINE STATUS OF THE EMERGENCY LIGHT BATTERIES. THE AIRCRAFT WAS REMOVED FROM SERSDR CHQA20120830348Angle · corrodedDURING INSPECTION, RAMP ANGLE CENTER OMEGA FRAME 20 WAS FOUND CORRODED. THE RAMP ANGLE CENTER OMEGA FRAME 20 WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02, 51-20-03, AND CPM 51-22-04/03.SDR CHQA20120830344Frame · damagedDURING INSPECTION, A MISDRILLED HOLE WAS FOUND ON FRAME 31 AT STRINGER 15R. FRAME 31 AT STRINGER 15R WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-04.SDR SIMA20120830005Flashlight · brokenDURING B INSPECTION FOUND THE AFT CABIN FLASHLIGHT RECEPTACLE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN FLASHLIGHT. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20120830004Battery · odorON FLIGHT 4272 THE CREW REPORTED THE CAPTAINS FLASHLIGHT HAS A FOUL SMELL COMING FROM IT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED CAPTAINS FLASHLIGHT BATTERY IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE ODOR WAS NO LONGER PRESENT. SDR SIMA20120830002Light · inoperativeDURING MAINTENANCE INSPECTION FOUND THAT THE LEFT OVERWING EMERGENCY LIGHT FAILS TO ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT BULB IAW EMB 145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD AT THSDR SIMA20120830001Door · dirtyON FLIGHT 3253 THE CREW REPORTED THE MAIN CABIN DOOR IS STICKY AND HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBED IAW AMM 52-18-00. THE OPERATIONAL CHECK WAS GOOD. NO DEFECT NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR ASOA20120830091Structure · corrodedDURING C-CHECK, CARGO DOOR LOWER CUTOUT STRUCTURE CORRODED (LOCAL LEVEL 2). MX R & R CARGO DOOR LOWER CUTOUT IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20120830090Skin · crackedDURING C-CHECK, CRACK AROUND RIVET FRAME 75, STRINGER 2L-3L VERIFIED WITH EDDY CURRENT. MX PERFORMED REPAIR BY INSTALLING FABRICATED REPAIR DOUBLER AND FILLER AT FRAME 75 BETWEEN STRINGER 2L-3L IAW EC5330-02313. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20120830089Floor Support · corrodedDURING C-CHECK CENTER OMEGA BEAM AT FRAME 44 LOWER CROSSBEAM ATTACHMENT POINT HAS CORROSION (LOCAL LEVEL 2). MX PERFORMED AND COMPLETED REPAIR OF CENTER OMEGA BEAM AT FRAME 44 LOWER CROSSBEAM ATTACHMENT POINT IAW EC5310-01466. THE ACFT WAS APPROVED FOR RETUR
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