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 SIMA20161118003Pump · failedHYD SYSTEM NR 1 FAILURE IN FLIGHT. HYD NR 1 QUIANTY INDICATOR AMBER FULL SCALE LEFT. RAN PROCEDURE. REMOVED AND REPLACED THE NR 1 EDP IAW AMM 29-10-03, AND PRESSURE LINE. LEAK CHECKED GOOD.SDR SIMA20161118002Bulb · inoperativeRIGHT WING INSPECTION LIGHT INOPERATIVE. REPLACED THE BULB IAW AMM 33-50-10-04, OPS CHECKED GOOD.SDR ASOA201611207004Battery · dischargedAFT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD AIRCRAFT RELEASED AND RETURNED TO SERVICE.SDR SIMA20161117004Light · damagedLT EMERGENCY LIGHT EXTRUSION NR 1 AND NR 3 DAMAGED. R&R LT EMERGENCY LIGHT EXTRUSION NR 3 IAW AMM 33-50-12, SEE NRTC BOW233027 FOR THE INSTALLATION OF NR 1 EXTRUSION.SDR SIMA20161117003Light · inoperativeTHE SECOND EMERGENCY LIGHT STRIP FROM THE BACK INOP. REMOVED AND REPLACED THE SECOND EMERGENCY LIGHT STRIP FROM THE BACK IAW AMM 33-50-12,AND OPS CHECKED GOOD.SDR ASOA201611207005Engine · faultyENGINE 1 HI VIBRATION AND OIL SMELL IN THE COCKPIT. REMOVED AND REPLACED NR 1 ENGINE. OPS AND LEAK CHECK GOOD. AIRCRAFT RELEASED TO SERVICE.SDR SIMA20161117002Switch · obstructedAFTER ROTATION AND DURING GEAR RETRACTION, RECEIVED "ACCESS DOORS OPEN" CAUTION MESSAGE AND FOWARD AVIONICS ACCESS HATCH OPEN INDICATION ON MFD DOORS PAGE-C/A-UPON FURTHER INVESTIGATION FOUND SEAL OBSTRUCTING SWITCH. RESEATED DOOR AND OPS CHECK GOOD IAW EMB 14SDR SIMA20161117001Door · lack of lubeMAIN CABIN DOOR VERY HARD TO GET OPEN WHEN HANDLE FULL UP. COMPLIED WITH PAX DOOR INSPECTION IAW AMM 52-11-00 LUBE AS REQUIRED CHECK GOOD OK FOR SERVICESDR SIMA20161116001Carbon Seal · failedNR 2 ENGINE FAILED TO START. NO ROTATION. REMOVED AND REPLACED NR 2 STARTER IAW AMM 80-10-01. OPS AND LEAK CHECKED GOOD. REMOVED AND REPLACED NR 2 ENGINE ATS CLAMP IAW AMM 80-10-01. REMOVED AND REPLACED STARTER MAGNETIC CARBON SEAL IAW RRM 72-63-10. LEAK CSDR SIMA20161115001Fitting · crackedLT ENGINE FWD LOWER YOKE CRACKED. REMOVED AND REPLACED LT FWD PYLON LOWER YOKE IAW EO EM-54MR-386.SDR SIMA20161114006Connector · brokenUNDER FLOOR BOARD PANEL 251DF BROKEN OFF SPLICE ON AIRCRAFT SIDE FOR LIGHT STRIP. REPLACED CONNECTOR ON AIRCRAFT SIDE FOR LIGHT STRIP UNDER FLOOR BOARD PANEL 251DF IAW SWPM 20-21-00.SDR SIMA20161114005Rib · chafedLEFT WING RIB LOCATED BETWEEN 551CB AND 551DB, CHAFED UNDER THE PCA HOSES. REPAIRED THE RIB IAW ERS-EM-57MR-723.SDR SIMA20161114004Frame · crackedOUTBOARD RIVET HOLE CRACKED ON LOWER END OF FRAME 66. REPAIRED THE FRAME IAW ERS-EM-53MR-2405.SDR SIMA20161114003Shear Tie · corrodedFRAME 68 SHEAR TIE IS CORRODED AT CARGO DOOR CUT LOWER CORNER. REPAIRED THE SHEAR TIE IAW SRM 53-31-04.SDR SIMA20161114002Shear Tie · corrodedFRAME 65 SHEAR TIE CORRODED BELOW CARGO LOWER GUIDE AND AT CARGO DOOR SILL . REPAIRED THE SHEAR TIE IAW SRM 53-31-04.SDR RAIA201611140001Clamp · looseBLEED 2 LEAK ON CLIMB OUT. TIGHTEND CLAMPS ON THE NR 2 PRECOOLER. PERFORMED GROUND RUN, OPS CHECKED GOOD IAW AMM 36-11-04 AND 36-00-00.SDR RAIA201611130001Seal · wornNR 2 BLEED LEAK AFTER TAKE OFF. R & R BLEED SEALS 11 & 22 IAW AMM 21-20-00. NO LEAKS NOTED AT THIS TIME.SDR SIMA20161113001Bulb · inoperativeRIGHTT AFT UPPER OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULB IAW AMM 33-50-10. OPS CHECKED GOOD.SDR SIMA20161112004Skin · crackedLEFT REAR FUSELAGE SKIN CRACKED AT FRAME 75, BETWEEN STRINGERS 1 AND 2L. REPAIRED THE SKIN IAW SRM 53-31-01.SDR SIMA20161112002Inverter · inoperativeFOUND AFT GALLEY EMERGENCY LIGHT INOPERATIVE DURING PS-2 INSPECTION. REMOVED AND REPLACED THE NR 3 INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD.SDR SIMA20161111004Door Sill · corrodedCARGO DOOR LOWER SILL CORRODED REMOVED AND REPLACED CARGO DOOR SILL IAW SRM 53-40-02.SDR SIMA20161111003Stringer · crackedSTRINGER 6R CRACKED AT FRAME 13. REMOVED AND REPLACED THE STRINGER IAW SRM 51-40-02.SDR SIMA20161111002Frame · crackedAFT CARGO DOOR CUTOUT FRAME 68 FRAME CRACKED. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02.SDR SIMA20161111001Door Frame · corrodedLEFT OVERWING EMERGENCY EXIT LOWER FRAME CORRODED AT AFT GUIDE BLOCK AND FWD GROUNDING CLIP. REMOVED AND REPLACED THE DOOR FRAME IAW SRM 51-40-02SDR SIMA20161110003Door Sill · corrodedSERVICE DOOR CUTOUT LOWER CENTER SILL CORRODED. REPAIRED SERVICE DOOR CUTOUT LOWER CENTER SILL IAW EMB145 53-21-02, AND 51-20-03SDR SIMA20161110004Skin · corrodedFUSELAGE SKIN HAS CORROSION JUST AFT OF 123BL ACCESS PANEL BENEATH TCAS II ANTENNA, BETWEEN FRAMES 10 AND 11. REPAIRED THE SKIN IAW SRM 53-00-23.SDR SIMA20161110002Skin · corrodedFUSELAGE SKIN HAS CORROSION BENEATH TDR MODE-S ANTENNA, BETWEEN FRAMES 20 AND 21. REPAIRED THE SKIN IAW SRM 53-00-23.SDR ASOA201611103080Control Panel · malfunctionedTHE CREW REPORTED LAVATORY SMOKE INDICATION ON EICAS IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE LAVATORY SMOKE DETECTION PANEL. OPERATIONAL CHECKS WERE GOOD.SDR SIMA20161110001Hose · failedIN FLIGHT HYD LOW QTY E1 HYD PUMP FAIL. REMOVED AND REPLACED E1 HYD PRESSURE HOSE IAW AMM 29-10-03. OPS AND LEAK CHECKED GOOD. NO DEFECTS NOTED.SDR SIMA20161109003Contact · missingLEFT NR 1 EMERGENCY LIGHT CONTACT MISSING. INSTALLED CONTACT IAW SWPM 20-00-03.SDR SIMA20161109001Light · inoperativeRIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSY, OPS CHECKED GOOD, IAW AMM 33-50-10SDR SIMA20161109002Wire · damagedEMERGENCY LIGHTS INOPERATIVE AT ROW 17 AND 18. REPAIRED THE LIGHT WIRE SPLICE SP9212 IAW SWPM 20-21-00. OPS CHECKED GOOD IAW AMM 33-50-00SDR ASOA201611096154Floor Support · corrodedDURING C-CHECK THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 59. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-24-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA20161108001Display · failedWHILE SITTING AT GATE ON APU PWR STRONG ELEC SMELL FROM CA SIDE THEN CA PFD WENT OFF. FEW MINUTES LATER PFD CAME BACK ON STRONG ODOR. SHUT OFF AC POWER TO AIRCRAFT. SWAPPED FO'S MFD AND CA PFD BACK TO ORIGINAL LOCATIONS. REMOVED AND REPLACED CA PFD IAW AMM 34-SDR ASOA201611086147Yoke · crackedDURING C-CHECK, THE RT ENGINE LOWER FORWARD MOUNT YOKE WAS FOUND TO BE CRACKED AND VERIFIED WITH EDDY CURRENT. MAINTENANCE REMOVED AND REPLACED THE YOKE IAW ECTC EA 26-2014-063-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA20161107001Wire · chafedELECTRICAL SMOKE IN COCKPIT DURING THE DESCENT. IT APPEARED TO FOG OUT ON THE LEFT SIDE JUST BELOW THE GLARESHIELD. FOUND CHAFED WIRES ON CONNECTOR J1268 BEHIND CA WX CONTROLLER, REPAIRED WIRES ON CONNECTOR J1268 IAW SWPM 20-21-00 AND SWPM 20-13-01. OPC GOOD ISDR SIMA20161106006Inverter · inoperativeMID CENTER CEILING AFT EMERGENCY LIGHT INOP. REMOVED AND REPLACED MID CENTER CEILING AFT EMERGENCY LIGHT NR 4 INVERTER. OPERATIONAL CHECK GOOD IAW AMM 33-50-11, 33-50-00SDR SIMA20161106007Mount · crackedRT ENGINE FWD ENGINE MOUNT HAS POSSIBLE CRACK. REMOVED AND REPLACED RT ENGINE FWD LWR ENGINE MOUNT YOKE IAW EO EM-54MR-386.SDR 4VAA20161106002Warning System · false activationCREW RECEIVED BRAKE DEGRADED MESSAGE ON EICAS WHEN LANDING GEAR WAS SELECTED DOWN FOR LANDING AT AIRPORT. PROBLEM REPORTED TO ATC WHO DECLARED AN EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT. AFTER LANDING CREW REPORTED NR 3 BRAKE DISPLAYED COLD ON MFD WHILESDR SIMA20161106002Light · inoperativeRIGHT EXTERIOR OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECKED NORMAL.SDR SIMA20161106001Roller · lack of lubeFA REPORTS MAIN DOOR DIFFICULT TO OPEN. LUBRICATED MAIN DOOR FRAME ROLLER IAW AMM 53-21-02. OPS CHECKED GOOD.SDR ASOA201611054107Drag Angle · crackedDURING AN A CHECK INSPECTION, THE RIGHT VERTICAL STAB DRAG ANGLE WAS FOUND TO BE CRACKED AT FRAME 76, MAINTENANCE REMOVED AND REPLACED THE AFFECTED DRAG ANGLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA201611054105Skin · crackedDURING AN A CHECK INSPECTION, THE RIGHT AFT FUSELAGE SKIN WAS FOUND TO HAVE A 20MM CRACK AT FRAME 75 STRINGER 1R, MAINTENANCE PERFORMED A DOUBLER REPAIR TOP THE AFFECTED AREA, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA201611040855O-Ring · failedCREW REPORTED WHILE IN CLIMB, THRUST PACK 1 DISTRIBUTES A STRONG ODOR THAT BURNS EYES. REMOVED AND REPLACED O-RING ON THE CARBON SEAL OF THE NR 3 GENERATOR. OPS CHECK GOOD. A/C APPROVED FOR RETURN TO SERVICE.SDR SIMA20161103001Clamp · unsecureDURING CLIMB, CREW RECEIVED NR 1ENGINE BLEED LEAK MESSAGE. CREW COMPLIED WITH AOM VOL 1 PROCEDURES, DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE WITHOUT INCIDENT. PERFORMED LEAK CHECK BLEED 1 SYSTEM JOINT NO LEAKS FOUND. DURING INSPECTION FOUND BLEED 1 SDR SIMA20161102002Sleeve · blownNR 1 BLEED LEAK AFTER TAKE OFF, RAN CHECKLISTS AND BLEED LEAK INDICATION WENT OUT AFTER ABOUT 5 MINUTES. INSPECTED AND FOUND THE NR 1 PACK DUCTING SLEEVE TO BE BLOWN. REMOVED AND REPLACED THE SLEEVE IAW AMM 21-51-00. OPS CHECKED GOOD.SDR SIMA20161102001Inverter · inoperativeEMERGENCY EXIT SIGN ABOVE SERVICE DOOR INOPERATIVE. R & R NR 2 INVERTER IAW AMM 33-50-11 OPS CHECKED GOOD.SDR SIMA20161101002Structure · crackedPOSSIBLE CRACK LOCATED APPROX 1'' BELOW CARGO DOOR HANDLE CUTOUT. INSTALLED REPAIR DOUBLER, CARGO DOOR IAW ERS-EM-52MR-661. SEE TASKS AND WIPS FOR DETAILS.SDR SIMA20161101003Skin · crackedRT UPPER FUSELAGE SKIN CRACKED AFT OF FRAME 75 AND ABOVE STRINGER 2R, APPROX 3/8' LONG. INSTALLED REPAIR DOUBLER, FILLER, SHIM DRAG ANGLE ON RT UPPER FUSELAGE AFT OF FRAME 75 AND ABOVE STRINGER 2R IAW SRM 53-31-01. SEE WIPS AND TASKS FOR DETAILS.SDR SIMA20161031002Cup · corrodedDURING IMBV INSPECTION, QA FOUND TOILET WASTE DRAIN VALVE CUP CORRODED. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE TOILET WASTE DRAIN VALVE CUP IAW SRM 51-40-02, 51-20-01 AND 51-20-03.
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