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 ASOA20130527040Unknown · odorTHE CREW REPORTED ODOR COMING FROM PACK 1 WHEN ENGINE BLEEDS WERE SELECTED. MX INSPECTED AND PERFORMED OPS CHECKS OF PACK 1, ENGINE BLEED 1. NO DEFECTS WERE FOUND. THE ACFT WAS RELEASED FOR SERVICE.SDR SIMA20130527005Drain Line · contaminatedTHE CREW REPORTED THAT IN ICING CONDITIONS THEY GOT AMBER IAS AND ALT INDICATIONS AT 37,000 FEET. THE PROBLEM PERSISTED UNTIL 20,000. AT ONE POINT FOS AIRSPEED INDICATED 60KTS AND FOS ALTIMETER WAY OFF. THE CAPTAIN'S ALTIMETER JUMPED TO DIFFERENT INDICATIONSSDR SIMA20130527004Unknown · odorTHE CREW REPORTED AN ABNORMAL ODOR STARTING AT ROW 11 AND STRONGER IN THE AFT AERA. THE ACFT WAS REMOVED FROM SERVICE. RAN BOTH A/C PACKS IN HOT & COLD MODES USING APU. ILLUMINATED ALL CABIN LIGHTS FOR TEST. UNABLE TO DISCERN ANY OFFENSIVE ODORS. OK FOR SDR SIMA20130526006Carbon Seal · leakingNR 1 ENGINE SHOWING 8 QTS OF OIL IN FLIGHT. NOTICED A STRONG OIL ODOR ON DECENT. ACFT REMOVED FROM SERVICE. INSPECTED NR 1 ENGINE AND IT SHOWED SIGNS OF AN OIL LEAK. REMOVED AND REPLACED CARBON SEAL ASSEMBLY IAW AMM 72-25-25. NO LEAKS OR ODORS NOTED. AIRSDR RAIA201305250001Inverter · dirtyDURING SCHEDULED MX, THE EMERGENCY EXIT LIGHT ABOVE THE SERVICE DOOR WAS FOUND INOP. MX INSPECTED AND DISCONNECTED AND CLEANED THE DC/AC INVERTERS NR 2 & NR 3. THEY RECONNECTED THE INVERTERS AND SYS OPS CHECKED GOOD.SDR ASOA20130525052Control Unit · faultyCREW REPORTED OTBD BRAKE INOPERATIVE. MX R & R THE BRAKE CONTROL UNIT WITH OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA20130525003Battery · dischargedTHE CREW REPORTED WHEN EMERGENCY LIGHTS ARE TURNED OFF WITH BATTRIES ON. CENTER FLOOR STRIP AND WITH BATTERIES OFF AS WELL LIGHTS ONLY, GO OFF WITH EMERGENCY LIGHTS IN ARM. THE ACFT WAS REMOVED FROM SERVICE. R & R THE NR 3 EMERGENCY BATTERY AND POWER SUPPLYSDR SIMA20130524004Flashlight · inoperativeDURING MX INSP, FOUND THE CAPTAIN’S FLASHLIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE CAPTAIN’S FLASHLIGHT IAW AMM 33-50-16. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.SDR SIMA20130524003Light · inoperativeDURING B INSPECTION, FOUND THE SERVICE DOOR EMERGENCY LIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE SERVICE DOOR EMERGENCY LIGHT IAW TASK 33-50-09-000-801-A AND 33-50-09-400-801-A. THE OPS CHECK WAS GOOD AT THIS TIME. THE ACFT WAS RETURNED SDR SIMA20130524002Wire · brokenDURING B INSP, FOUND THE SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED TROUBLESHOOTING OF SERVICE DOOR EXTERAL EMERGENCY LIGHT, FOUND BROKEN WIRE. PERFORMED REPAIR IAW WM 20-21-00. THE OPS CHECK WAS GOOD AT SDR SIMA20130523001Hydraulic System · lowTHE CREW REPORTED THAT AFTER APPROX 1 HOUR OF CRUISE FLIGHT AT 36000 THEY RECEIVED AN EICAS MESSAGE "HYD 1 LOW LEVEL". THE MESSAGE EXTINGUISHED WITH GEAR EXTENTION. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE ACFT WAS REMOVED FROM SERVICESDR ASOA20130522051Bulb · inoperativeDURING SCHEDULED MX INSPECTION THE OVERHEAD GALLEY EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX R & R THE OVERHEAD GALLEY EMERGENCY LIGHT BULB WITH OPERATIONAL CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130522050Charger · inoperativeDURING SCHEDULED MX INSPECTION BOTH AFT OVERWING EXTERIOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX R & R THE NR 4 EMERGENCY LIGHT BATTERY CHARGER WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA20130522003Fadec · malfunctionedTHE CREW REPORTED THAT DURING CRUISE FLIGHT, NR 2 ENGINE (N1) SMOOTHLY ROLLED BACK ABOUT 25-30 PERCENT AND THEN SMOOTHLY CAME BACK UP, IT DID THIS 3 TIMES IN ABOUT 15 MINUTES AND THEN RETURNED TO NORMAL. ON LANDING, GOT E1 EXCEEDANCE ON EICAS. THE ACFT WAS RSDR SIMA20130521011Frame · crackedDVI FWD FUSELAGE FRAME 8 LOWER AVIONIC DOOR OPENING CRACKED. PERFORM DVI FWD FUSELAGE FRAME 8 LOWER AVIONIC DOOR IAW EO EM-53MR-2092, PART B ONLY NO FUTHER DAMAGE NOTED CONTINUED ON TDMI63253083F.SDR SIMA20130521010Flashlight · unserviceableDURING B INSP FOUND THE F/O EMERGENCY FLASHLIGHT WOULD NOT STAY ON. THE ACFT WAS REMOVED FROM SERVICE. R & R THE F/O EMERGENCY FLASHLIGHT IAW AMM 33-50-00. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.SDR SIMA20130521009Light · brokenDURING MX INSEPCTION, FOUND THE NR 1 EMERGENCY LIGHT STRIP HAD A BROKEN CONNECTION. THE ACFT WAS REMOVED FROM SERVICE. R & R THE NR 1 EMERGENCY LIGHT STRIP IAW AMM 33-50-12. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.SDR SIMA20130521008Connector · missingDURING B INSPECTION, FOUND THE EMERGENCY LIGHT STRIP CONNECTOR AT SEAT POSITION 9A MISSING CONNECTOR. THE ACFT WAS REMOVED FROM SERVICE. R & R THE EMERGENCY LIGHT STRIP CONNECTOR AT SEAT POSITION 9A IAW SWPM 20-21-00, STEP 5 AND REINSTALLED EMERGENCY LIGHT STSDR SIMA20130521007Actuator · failedTHE CREW REPORTED THAT WHILE OPERATING FLAPS, FLAPS FROZE AT 27 DEGREES WITH SIMULTANEOUS "FLAP FAIL" MFD MESSAGE AND "FLAP RT TRANSMISSION FAIL" CMC MESSAGE. LOUD GRINDING NOISE WHEN DEPLOYING FLAPS FROM 9 TO 22 DEGREES, APPROX 180 KTS. THE ACFT WAS REMOVED SDR SIMA20130521006Pump · failedTHE CREW REPORTED THAT DURING CLIMB OUT, THEY RECEIVED A HYD SYS 2 LOW MESSAGE. THE CREW COMPLETED THE AOM EMERGENCY AND NORMAL CHECKLIST. LATER THEY FOUND THE NR 2 HYD QTY WENT INTO THE AMBER RANGE. THE SYS MAINTAINED PRESSURE, BUT LATER IN FLIGHT THE CREW SDR SIMA20130521002Flashlight · faultyDURING B-INSPECTION, FOUND THE CAPTAIN’S FLASHLIGHT NOT CHARGING. THE ACFT WAS REMOVED FROM SERVICE. R & R THE CAPTAIN’S FLASHLIGHT ASSY IAW AMM 33-50-16-000 801-A AND 33-50-16-400-801-A. THE OPS CHECK WAS GOOD. NO DEFECTS NOTED AT THIS TIME. THE ACFT WASSDR SIMA20130520009Wire Harness · inoperativeAFTER LEAVING DEPARTURE AIRPORT FUEL TANK TEMPERATURE WAS ABOUT 27C. HALF WAY THROUGH THE FLIGHT THE TEMPERATURE HAD DROPPED TO 7C. DECLARED AN EMERGENCY AND DIVERTED. ACFT LANDED WITHOUT INCIDENT. COMPLIED WITH CONTINUITY/ RESISTANCE, INTERNAL SHORTS AND SDR CHQA20130520187Stringer · corrodedDURING INSPECTION, CORROSION WAS FOUND ON STRINGER 21 AT FRAME 13. THE STRINGER WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02 AND 51-20-03.SDR CHQA20130520186Attach Bolt · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE FLAP POWER DRIVE UNIT ATTACH POINTS. THE ATTACH POINTS WERE REPAIRED IN ACCORDANCE WITH ETD 2013-145-010207.SDR CHQA20130520173Relay · failedCREW REPORTED THAT DURING CLIMBOUT THEY RECEIVED A YAW DAMPNER FAIL MESSAGE FOLLOWED BY A RUDDER SYSTEM ONE AND TWO INOPERATIVE MESSAGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND WAS ABLE TO RESET THE SYSTEM, HOWEVER, THE MESSAGES RETURNED. DISPATCHSDR CHQA20130520172Relay · failedCREW REPORTED THAT DURING CLIMBOUT THEY RECEIVED A YAW DAMPNER FAIL MESSAGE FOLLOWED BY A RUDDER SYSTEM ONE AND TWO INOPERATIVE MESSAGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND WAS ABLE TO RESET THE SYSTEM, HOWEVER, THE MESSAGES RETURNED. DISPATCHSDR CHQA20130520171Pressure Switch · malfunctionedCREW REPORTED THAT DURING CLIMBOUT THEY RECEIVED A YAW DAMPNER FAIL MESSAGE FOLLOWED BY A RUDDER SYSTEM ONE AND TWO INOPERATIVE MESSAGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND WAS ABLE TO RESET THE SYSTEM, HOWEVER, THE MESSAGES RETURNED. DISPATCHSDR ASOA20130520037Inverter · inoperativeTHE CREW REPORTED CENTER AISLE EXIT LIGHT WAS INOPERATIVE. MX REPLACED THE NR 6 EMERGENCY LIGHT INVERTER. OPS CHECKED GOOD.SDR ASOA20130520049Wire · brokenCREW REPORTED SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. MX FOUND A BROKEN WIRE SPLICE AND REPLACED WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA20130521001Beam · corrodedDURING MX INSPECTION FOUND THE CARGO DOOR SILL CORRODED. THE ACFT WAS REMOVED FROM SERVICE. R & R CARGO DOOR SILL IAW SRM 51-40-02, LEVEL 2 CORROSION. THE ACFT WAS RETURNED TO SERVICE.SDR SIMA20130520008Control Panel · inoperativeTHE CREW REPORTED THAT ON THE CLIMB THE MAIN PITCH TRIM FAILED. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. R & R THE TRIM CONTROL PANEL AND PERFORMED OPS TEST OF HORIZONTAL STABILIZER SYS IAW AMMSDR SIMA20130520002Sign · inoperativeDURING B INSPECTION, FOUND THE EMERGENCY EXIT SIGN MID AISLE INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED EMERGENCY LIGHT TEST IAW AMM 33-50-00. NO DEFECT NOTED. THE ACFT WAS RETURNED TO SERVICE.SDR SIMA20130520001Flashlight · inoperativeTHE F/A REPORTED THE FLASHLIGHT ABOVE THE JUMPSEAT DOES NOT APPEARS TO BE CHARGING AS THE RED LIGHT DID NOT ILLUMINATE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE BRACKET FOR FLASHLIGHT ABOVE THE JUMPSEAT IAW AMM 25-60-01. THE OPS CHECK WAS GOOD. THE ACFTSDR CHQA20130519191Structure · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR CUTOUT. THE SERVICE DOOR CUT OUT WAS REPAIRED IAW SRM 53-21-02.SDR CHQA20130519190Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT OMEGA BEAM AT THE SCREW HOLE FRAME 23. THE FRAME WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-010149.SDR CHQA20130519189Floor Support · corrodedDURING INSPECTION, A CRACK WAS FOUND ON THE LEFT OUTBOARD OMEGA BEAM SUPPORT BETWEEN FRAMES 47 AND 48. THE OMEGA BEAM SUPPORT WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20130519188Doubler · corrodedDURING INSPECTION, CORROSION WAS FOUND ON A REPAIR DOUBLER ON THE INBOARD SIDE OF THE LEFT OMEGA BEAM AT FRAME 20. THE DOUBLER WAS REPLACED IN ACCORDANCE WITH 53-00-10.SDR SIMA20130519006Flashlight · malfunctionedDURING MAINTENANCE INSPECTION, FOUND F/A FLASHLIGHT SWITCH INTERMITENT, LIGHT IS DIM. ACFT REMOVED FROM SERVICE. R & R FLASHLIGHT, OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.SDR SIMA20130519005Light · inoperativeDURING B INSPECTION, FOUND LT OVERWING EMERGENCY LIGHT INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R EMERGENCY LIGHT ASSEMBLY IAW AMM 33-50-10, STEPS 2M(1)(A-F) AND 3IL(1)(A-G). OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.SDR SIMA20130519004Flashlight · inoperativeFLIGHT 3951, CREW REPORTED F/O FLASHLIGHT INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R FLASHLIGHT IAW AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.SDR SIMA20130519003Door · lack of lubeON FLIGHT 3451, F/A REPORTED MAIN CABIN DOOR WAS DIFFICULT TO OPEN AND CLOSE. ACFT REMOVED FROM SERVICE. LUBRICATED DOOR IAW MM 52-18-00. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.SDR RAIA201305180002Pump · leakingDURING CRUISE FLIGHT THE CREW REPORTED HYD SYS 1 HAD A LOW FLUID QTY WARNING MESSAGE. THE SYS SLOWLY DROPPED TO ZERO. AFTER ABOUT 20 MINUTES THE CREW REPORTED HYD SYS 1 WAS LOST. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MX INSPECTED AND R SDR SIMA20130517015Skin · corrodedSKIN CORRODED BETWEEN FRAMES 13 AND FR 14 BETWEEN S21L AND 20R. REPAIRED IAW EO EM-53MR-2137R1 AND NRTC E311748.SDR SIMA20130517016Skin · corrodedSKIN CORRODED BETWEEN FR 13 AND FR 14 AND STR 20R AND 18R. REPAIRED IAW EO EM-53MR-2137R1.SDR SIMA20130517014Yoke · crackedLEFT PYLON FWD LOWER YOKE NR 1 CRACKED. R & R YOKE IAW EO-EM-53MR-386.SDR RAIA201305170001Switch · brokenDURING PRE-FLIGHT INSPECTION, THE FLIGHT CREW FOUND THE EMERGENCY LIGHT SWITCH ON THE OVERHEAD PANEL BROKEN. MX INSPECTED AND R & R THE SWITCH. SYS OPS CHECKED GOOD.SDR CHQA20130517182Angle · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE ANGLE BRACKET AT THE TOP OF FRAME 10 AND THE RIGHT COCKPIT WINDOW SEAL. THE ANGLE WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02 AND SRM 53-12-02.SDR ASOA20130517048Charger · inoperativeDURING MX INSPECTION, THE ROW 12 RT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX R & R THE NR 3 BATTERY CHARGER WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR CHQA20130516165Gcu · failedCREW REPORTED THAT DURING CLIMBOUT THEY RECEIVED A GENERATOR OFF BUSS MESSAGE FROM GENERATORS 1, 3, 4, AND THE APU GENERATOR. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND THE GENERATORS DID NOT COME BACK ONLINE. DURING THE RETURN TO FIELD FOR THIS ISSUSDR CHQA20130516164Generator · failedCREW REPORTED THAT DURING CLIMBOUT THEY RECEIVED A GENERATOR OFF BUSS MESSAGE FROM GENERATORS 1, 3, 4, AND THE APU GENERATOR. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND THE GENERATORS DID NOT COME BACK ONLINE. DURING THE RETURN TO FIELD FOR THIS ISSU
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