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 SIMA20170607002Unknown · unknownTHUMPING NOISE IN COCKPIT DURING CLIMB AND CRUISE. REPAIRED LEFT FWD FUSELAGE IAW SRM 53-10-01.SDR ASOA201706075084Ballast · inoperativePILOT REPORTED EMERGENCY EXIT LIGHTS AT THE GALLEY DOOR FOUND INOPERATIVE. MX RESET BALLAST AND OPS CHECKED GOOD.SDR SIMA20170607001Roller · lack of lubeCABIN DOOR IS DIFFICULT TO OPEN AND CLOSE. LUBED MAIN CABIN DOOR FRAME ROLLERS IAW AMM 53-21-02. OK FOR SERVICE.SDR ASOA201706074043Sign · inoperativeTHE CREW REPORTED THAT THE EMERGENCY EXIT SIGN ABOVE THE FA SEAT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EXIT SIGN, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA20170606009Floor Support · corrodedLEFT OMEGA BEAM IS CORRODED BETWEEN FRAMES 58 AND 59. REPAIRED THE OMEGA BEAM IAW ERS-EM-53MR-2773.SDR SIMA20170606008Channel · corrodedFR 65 CHANNEL IS CORRODED AROUND SCREW HOLE AT STRINGER 14L. REPAIRED THE CHANNEL IAW ERS-EM-53MR-2761.SDR ASOA201706064042Display · shortedTHE CREW REPORTED THAT EICAS FAIL IN FLIGHT WITH ODOR OF BURNING ELECTRICAL. THE AIRCRAFT DIVERTED WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND MAINTENANCE REMOVED AND REPLACED THE DEFECTIVE DISPLAY UNIT, OPERATIONALLY TESTED WITHSDR SIMA20170606002Lamp · inoperativeSERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-10-000-801-A, & 33-50-10-400-801-A. OPS CHECKED GOOD.SDR SIMA20170606003Roller · lack of lubeMAIN CABIN DOOR HARD TO OPEN. LUBRICATED THE HINGE ROLLERS IAW AMM-53-21-62. OPS CHECKED GOOD.SDR SIMA20170605002Wire · brokenLEFT EMERGENCY LIGHT NR 4 WIRES ARE BROKEN. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12SDR ASOA201706055083Control Unit · faultyPILOT REPORTED RIGHT BRAKE PEDAL WHEN COMMANDED RESULTS IN ALMOST NO BRAKING ACTION. ADDITIONALLY THE RIGHT IB BRAKE TEMP ALWAYS STAYED AT ZERO DESPITE THE RIGHT OB BRAKE TEMP GOING INTO THE AMBER INDICATION AFTER MODERATE BRAKING. MX REMOVED AND REPLACED BRAKSDR RAIA201706050001Bulb · inoperativeMAIN DOOR EXTERIOR FLOOD LIGHT NR 1 LOCATED ON BOTTOM OF PLUG DOOR HINGE IS INOPERATIVE. R & R THE BULB, OPS CHECKED GOOD.SDR SIMA20170605001Light · inoperativeSERVICE DOOR ARM EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EXTERIOR EMERGENCY LIGHT IAW AMM 33-50-10-000-801 AND 33-50-10-400-801. OPS CHECKED GOOD.SDR SIMA20170604005Frame · crackedFRAME 73 CRACKED AT STRINGER 17R-C/A-REMOVED AND REPLACED FR 73 AT STRINGER 17R IAW EMB 145 SRM 51-40-02SDR SIMA20170604007Door Sill · corrodedSERVICE DOOR CUTOUT LOWER CENTER SILL CORRODED. REPAIRED SERVICE DOOR CUTOUT LOWER CENTER SILL IAW 53-21-02, AND 51-20-03SDR SIMA20170604006Skin · crackedLEFT AFT FUSELAGE FRAME 75 HAS A SKIN CRACK ABOVE STRINGER 2L. PERFORMED A PERMANENT REPAIR IAW SRM 53-31-01SDR SIMA20170604004Stator · damagedNR 4 WHEEL BRAKE ASSY DAMAGED 1ST STATOR DUE TO PISTON OVERTRAVEL. REMOVED AND REPLACED THE BRAKE ASSY IAW 32-600-14SDR SIMA20170604002Power Supply · failedCOCKPIT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY BATTERY AND CHARGER IAW AMM TASK# 33-50-04-000-802-A, 33-50-04-400-802-A, 33-50-04-000-801-A, AND 33-50-04-400-801-A. OPS CHECKED GOOD.SDR SIMA20170603004Structure · corrodedLAVATORY BUCKET IS CORRODED AROUND TOILET WASTE VALVE. REMOVED AND REPLACED TOILET WASTE VALVE SUPPORT BUCKET IAW SRM 51-40-02SDR ASOA201706035081Battery Pack · unsecurePILOT REPORTED THE FLOOR EMERGENCY LIGHTS INOPERATIVE FROM ROWS 8 TO 18, EMERGENCY DOORS AND BACKSIDE OF THE CEILING PANEL ROW 18. MX FOUND NR 3 EMERGENCY LIGHT BATTERY UNSECURE, SECURED AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA20170603001Inverter · failedCENTER AISLE OVERHEAD EMERGENCY EXIT LIGHT AT SERVICE DOOR INOPERATIVE. REMOVED AND REPLACED NR 1 BATTERY POWER SUPPLY IAW AMM 33-50-04, OPS CHECKED FAILED. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT DC & AC INVERTER IAW AMM 33-50-11, AND OPS CHECKED FAISDR SIMA20170603003Bulb · inoperativeMAIN CABIN DOOR EMERGENCY LIGHT COVER BROKEN AND LIGHT INOPERATIVE. MAIN CABIN DOOR EMERGENCY LIGHT COVER AND LIGHT BULB REPLACED IAW AMM 20-21-00SDR SIMA20170603002Roller · out of adjustMAIN CABIN DOOR HARD TO OPEN. ADJUSTED BOTH UPPER PAX DOOR ROLLERS IAW AMM 52-10-01. OPS CHECKED GOOD. NO DEFECTS NOTED.SDR SIMA20170602004Lamp · inoperativeLEFT OVERWING EMERGANCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-10-000-801-A, & 33-50-10-400-801-A. OPS CHECKED GOOD.SDR SIMA20170602005Door · out of adjustMAIN CABIN DOOR HARD TO OPEN. JAMBS WHEN TRYING TO OPEN. PERFORMED AN ADJUSTMENT OF MAIN DOOR IAW AMM 52-10-01. OPS CHECKED GOOD. ACFT OK FOR SERVICE.SDR ASOA201706024041Skin · dentedDURING C-CHECK INSPECTION, THE CENTER FUSELAGE RT SKIN WAS FOUND WAS FOUND TO BE DENTED 3.5 INCH FWD OF FRAME 24 AND 1 INCH BELOW STRINGER 15R. MAINTENANCE REMOVED THE DAMAGED SECTION OF SKIN AND INSTALLED A REPAIR DOUBLER AND THE AIRCRAFT WAS APPROVED FOR RESDR ASOA201706024040Frame · crackedDURING C-CHECK INSPECTION, THE UPPER FRAME 10 ON THE RIGHT SIDE WAS FOUND TO BE CRACKED AT A RIVET LOCATION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FRAME SECTION AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA201706024039Crossbeam · crackedDURING A C-CHECK INSPECTION, THE NLG UPLOCK BOX CROSSBEAM WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA201706024033SGusset · corrodedDURING A C-CHECK INSPECTION, THE LEFT INBD FLOOR SUPPORT GUSSET WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND RPELACED THE AFFECTED GUSSET AND TYHE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA201706024035Crossbeam · corrodedDURING A C-CHECK INSPECTION, THE CENTER AISLE CROSSBEAM SUPPORT AT FRAME 20 WAS FOUND TO HAVE BARE METAL AND CORROSION BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CROSSBEAM AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA201706024034Gusset · corrodedDURING A C-CHECK INSPECTION, THE CENTER FLOOR SUPPORT GUSSET AT FRAMES 60 - 61 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED GUSSET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA201706024033Gusset · corrodedDURING A C-CHECK INSPECTION, THE LT INBD FLOOR SUPPORT GUSSET WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED GUSSET AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA20170601003Light · inoperativeMID CABIN FWD EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED MID CABIN FWD EMERGENCY LIGHT ASSY IAW AMM 33-50-15. OPS CHECKED GOOD.SDR SIMA20170601001Light · inoperativeEMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED THE EXIT LIGHT IAW AMM 33-50-14, OPS CHECKED GOOD.SDR SIMA20170531009Engine · malfunctionedNR 2 ENGINE SPOOLED DOWN AT GATE, ENGINE OUT EICAS CAUTION MESSAGE. START STOP SELECTOR WAS IN RUN POSITION AT THAT TIME. COMPLIED WITH FIM TASK 72-00-00-810-815 , FIM TASK 72-00-00-810-809 AND PERFORMED OPERATIONAL TEST OF ENGINE AT MAXIMUM POWER IAW MM 7SDR SIMA20170531007Frame · crackedFRAME 73 CRACKED BETWEEN STRINGERS 16 - 17R. REMOVED AND REPLACEDTHE FRAME SECTION IAW SRM 51-40-02.SDR SIMA20170531006Floor Support · corrodedLEFT FLOOR SUPPORT CORRODED AROUND AND UNDER CARBON CROSSBEAM, BETWEEN FR 33-34. COMPLETED INSTALLATION OF REPAIR DOUBLER, FILLER AND SHIMS IAW SRM 53-00-10, AND SRM 51-40-02. RESTORED PROTECTIVE TREATMENT TO AREAS IAW CPM 51-21-06 AND ETN-EM-51-091.SDR SIMA20170531005Skin · corrodedINTERNAL FUSELAGE SKIN CORRODED BETWEEN FRAMES 9-10, STRINGRS 20 - 21L. PERFORMED DRILL OUT OF CORRODED AREA AND INSTALLED A RIVET IAW SRM 53-12-01 AND RESTORED PROTECTIVE TREATMENT IAW CPM 51-21-06 AND ETN-EM-51-091.SDR SIMA20170531004Door Sill · corrodedCARGO DOOR CUTOUT LOWER SILL CORRODED. REMOVED AND REPLACED CARGO DOOR SILL IAW SRM 51-40-02.SDR SIMA20170531003Frame · crackedLEFT FRAME 10 CRACKED BELOW DV WINDOW CUTOUT. REMOVED AND REPLACED THE FRAME SECTION IAW SRM 51-40-02, AND SRM 51-20-03.SDR SIMA20170531002Frame · crackedRIGHT FRAME 10 CRACKED BELOW DV WINDOW CUTOUT. REMOVED AND REPLACED THE FRAME SECTION IAW SRM 51-40-02, AND SRM 51-20-03.SDR SIMA20170531001Frame · crackedFRAME 72 CRACKED BETWEEN STRINGER 16 - 17L. REMOVED AND REPLACED THE FRAME SECTION IAW SRM 51-40-02.SDR ASOA201705305081Display · shortedMFD NR 2 WENT BLANK AT THE SAME TIME AS AN ELECTRICAL BURNING ODOR. MX REMOVED AND REPLACED NR 2 MFD WITH OPERATIONAL CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA201705304037Frame · damagedDURING A C-CHECK INSPECTION, FRAME 72 WAS FOUND TO BE DAMAGED BETWEEN STRINGERS 15 & 16R. MAINTENANCE REMOVED THE DAMAGED.SDR SIMA20170530002Flashlight · inoperativeFLASHLIGHT ABOVE FA JUMPSEAT DOEN NOT WORK. REPLACED THE FLASHLIGHT.SDR SIMA20170530001Transceiver · failedRADAR FAILED MESSAGE, WHEN IN TEST MODE. AMBER WX INSCRIPTION ON MFD WHEN IN WX MODE WITH NO RADAR RETURN. REMOVED AND REPLACED THE WEATHER RADAR RTA IAW AMM 34-42-01 OPS CHECKED GOOD.SDR ASOA201705295080Light · intermittentPILOT REPORTED EMERGENCY EXIT LIGHT NR 3 INOPERATIVE. MX PERFORMED OPERATIONAL CHECK, CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA201705294036Skin · damagedDURING A C-CHECK INSPECTION, THE AFT FUSELAGE SKIN WAS FOUND TO HAVE A SMALL NICK AT FRAME 68 BETWEEN STRINGERS 10 & 11L. MAINTENANCE BLENDED THE AFFECTED AREA IAW ETD2017-145-045392, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA201705281632Skin · crackedEXTERNAL FUSELAGE SKIN HAS A .25 INCH CRACK AT THE 1ST FASTENER BELOW STRINGER 2R AT FRAME 74. REPAIRED THE SKIN IAW SRM 53-31-01.SDR ASOA201705281616Skin · corrodedEXTERNAL FUSELAGE SKIN HAS A .25 INCH CRACK AT THE 1ST FASTENER BELOW STRINGER 2R, FRAME 74. REPAIRED THE SKIN IAW SRM 53-31-01.
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