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 SIMA20170913001Inverter · failedOVERHEAD EMERGENCY EXIT SIGN AND AT THE SERVICE DOOR INOPERATIVE. TROUBLESHOT AND FOUND THE NR 1 INVERTER TO BE BAD IAW WM 33-50-50. INSTALLED A USED INVERTER AND OPS CHECKED IAW W/C 33-700-17, OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED.SDR SIMA20170912005Floor Support · corrodedRIGHT OMEGA BEAM HAS CORROSION AROUND NUTPLATE HOLE AT FRAME 60 AND Y-479. REPAIRED THE OMEGA BEAM IAW SRM 53-24-10SDR SIMA20170912004Floor Support · corrodedLEFT OMEGA BEAM HAS CORROSION AROUND NUTPLATE HOLE AT FRAME 59 AND Y-479. REPAIRED THE OMEGA BEAM IAW SRM 53-24-10.SDR SIMA20170912006Floor Support · corrodedLEFT OMEGA BEAM HAS CORROSION AROUND NUTPLATE HOLE AT FRAME 60 AND Y-479. REPAIRED THE OMEGA BEAM IAW SRM 53-24-10.SDR SIMA20170912001Engine · smokeEICAS FOR A LAVATORY SMOKE INDICATION AT 500 FT. F/A INDICATED SMOKE AT ROWS 12 - 18 THAT QUICKLY DISSIPATED. PERFORMED ETN -EM-72-034. FOUND SOURCE OF SMOKE TO BE THE NR 2 ENGINE. R & R THE NR 2 ENGINE IAW W/C 71-000-00. ALL LEAKS AND OPS CHECKED GOOD.SDR ASOA201709125106Light · inoperativeDURING MX INSPECTION, ROW 3CD EMERGENCY LIGHT WAS DISCOVERED INOPERATIVE. MX REMOVED AND REPLACED THE LIGHT AND OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.SDR RAIA201709120001Bulb · inoperativeRIGHT OVERWING EMERGENCE LIGHT WAS INOPERATIVE. R & R THE BULB, OPS CHECKED GOOD.SDR SIMA20170912002Charger · inoperativeAFT CABIN CEILING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT CHARGER IAW AMM 33-50-04.SDR SIMA20170911001Roller · bindingFA REPORTED THE MAIN DOOR VERY HARD TO OPERATE. PERFORMED MAIN DOOR FRAME ROLLERS SERVICE IAW AMM 53-21-02. OPS CHECKED GOODSDR HNAA2017091400306Warning Light · false activationBOTH BLEEDS WENT OVERTEMP DURING ICE TEST. DOWNLOADED CMC TO MFD WITH NO RELATED CMC MESSAGES PRESENT AND NO RECENT HISTORY OF DISCREPANCY. PERFORMED AN ICE PROTECTION TEST SEVERAL TIMES WITH NO DEFECTS NOTED. OPS CHECKED GOOD. ALL SYSTEMS OPERATE NORMALLY SDR ASOA201709107013Frame · damagedA/C IS IN FOR A C-CHECK INSPECTION WHEN THE INSPECTOR FOUND FRAME 62 DAMAGED BETWEEN STRINGER 4R AND 5R. MAINTENANCE R&R THE DAMAGED SECTION OF FRAME 62 AT STR. 5R TO 1R IAW SRM 53-00-04. ALL WORK COMPLETED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR SIMA20170909005Shear Tie · crackedCRACKED SHEAR TIE AT FRAME 67, STRINGERS 6 - 7L. REMOVED AND THE SHEAR TIE IAW SRM 51-40-02.SDR SIMA20170909009Skin · damagedSEVERAL HOLES IN FUSELAGE SKIN ARE ELONGATED WHERE SERVICE DOOR OR THRESHOLD ATTACHES TO SKIN STRINGER 16R, FRAMES 20 - 22. REAMED DISCREPANT HOLES TO REMOVE DAMAGE AND PREP FOR INSTALLATION OF FREEZ PLUG BUSHING.SDR SIMA20170909004Stiffener · crackedFRAME 18, STRINGER 3L STIFFENER CRACKED. INSTALLED A NEW STIFFENER.SDR SIMA20170909003Threshold · corrodedCORROSION AROUND THREE NUTPLATES FOR THE SERVICE DOOR THRESHOLD BETWEEN FRAMES 20 - 22. BLENDED THE CORROSION IAW SRM 51-10-03. REPLACED THE THRESHOLD.SDR SIMA20170909002Shear Tie · crackedCRACKED SHEAR TIE AT FRAME 66 STRINGERS 6 - 7. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02.SDR SIMA20170909001Floor Support · corrodedCENTER OMEGA BEAM AR FR 18-23 IS CORRODED WITH 100% MATERIAL LOSS. REMOVED AND REPLACED THE OMEGA BEAM IAW SRM 51-40-02.SDR SIMA20170909006Wire · broken1ST EMERGENCY LIGHT STRIP WIRES BROKEN AT STRIP. NR 1 EMERGENCY LIGHT OPS TESTED IAW AMM 33-50-12 AND ETN EM-33-058SDR SIMA20170909008Bracket · crackedNOSE LANDING GEAR UP LOCK BRACKET IS CRACKED. REMOVED AND REPLACED THE LT AND RT SUPPORTS FOR NLG UPLOCK BOX IAW SRM 51-40-02 AND AMM 20-10-01SDR ASOA201709092009O-Ring · leakingNR 1 ENGINE PRODUCED SMOKE ON EXHAUST DURING WALK AROUND. REPLACE LPT SHAFT PLUG O-RING. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR HNAA2017091400307Light · inoperativeEMERGENCY LIGHT NOT ILLUMINATING. CLEANED AND RESEATED EMERGENCY LIGHT, OPS CHECKED GOOD. OK FOR SERVICE.SDR SIMA20170907003Door Sill · corrodedCARGO DOOR SILL CORRODED. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-40-02.SDR SIMA20170907001Mount · crackedPAX DOOR INNER HANDLE TORQUE BOX SUPPORT HAS A ONE INCH CRACK. THE MOUNTING BRACKET WAS REPAIRED IAW EM-52-MR-162.SDR ASOA201709075104Smoke Warning · false activationPILOT REPORTED A SPURIOUS LAVATORY SMOKE MESSAGE DURING CLIMBOUT. MX PERFORMED INSPECTION AND OPERATIONAL CHECK OF LAVATORY SMOKE DETECTOR SYSTEM. NO FAULTS NOTED. OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA20170907002Carbon Seal · leakingLAVATORY SMOKE DURING TAKEOFF ON EICAS. FA SMELLED SMOKE AT ROWS 6. 7. 8. REMOVED AND REPLACED THE RT ENGINE CARBON SEAL IAW MM 72-25-25-400-801. PERFORMED LEAK TEST AT MAX TAKEOFF POWER IAW MM 72-00-00-790-002. LEAK CHECKED GOOD. ENGINE RUNS IAW ETN-EM-79-SDR SIMA20170906006Bulkhead · crackedAFT WALL OF RIGHT MLG WHEEL WELL HAS A 1 INCH CRACK THAT IS VISIBLE FROM THE AFT SIDE OF WALL. REPAIRED RT MLG WW BULKHEAD IAW SRM 53-23-12.SDR SIMA20170906003Attach Angle · crackedRIGHT UPPER WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE HAS A 1/2 INCH CRACK JUST FWD OF SPAR 2. REPAIRED THE ATTACH ANGLE IAW ETN-EM-53-142.SDR SIMA20170906004Attach Angle · crackedRIGHT UPPER WING TO FUSELAGE FAIRING UPPER ATTACH ANGLE ON FUSELAGE HAS 1/8 INCH CRACK BETWEEN FRAMES 48-49. REPAIRED THE ATTACH ANGLE IAW SRM 53-23-12.SDR SIMA20170906005Attach Angle · crackedLEFT UPPER WING TO FUSELAGE LOWER ATTACH ANGLE ON WING HAS 1/8 INCH CRACK JUST AFT OF SPAR 2. R & R THE ATTACH ANGLE IAW SRM 51-40-02.SDR SIMA20170906001Roller · stiffFA REPORTED THAT THE CABIN DOOR WAS DIFFICULT TO OPEN. FOUND THE DOOR ROLLERS STIFF, LUBRICATED THE ROLLERS. OPS CHECKED GOOD.SDR SIMA20170905005Attach Angle · crackedLEFT FUSELAGE TO WING FAIRING LATERAL PANEL. LOWER ATTACH ANGLE CRACKED AT THE AFT END. R & R THE ATTACH ANGLE IAW ETN-EM-53-142.SDR SIMA20170905004Bulb · inoperativeDURING PS-1, FOUND THE LAST ASILE EMERGENCY LIGHT INOPERATIVE. REPLACED THE BULB IAW AMM 33-50-08, OPS CHECKED GOOD.SDR SIMA20170905001Flashlight · inoperativeFA`S FLASHLIGHT AT ROW 18 IS INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM 25SDR SIMA20170904002Duct · detachedNR 1 PACK VALVE CLOSES IN FLIGHT. REMOVED AND REPLACED THE NR 1 A/C PACK VALVE IAW AMM 21-51-01. PERFORMED AN OPS CHECK IAW AMM 21-60-00, OPS CHECKED FAILED DUE TO THE NR 1 PACK OVERHEAT. FOUND THE NR 1 A/C PACK ACM DUCT DETACHED. SECURED IAW AMM 21-20-00SDR SIMA20170904001Lamp · inoperativeMAIN DOOR EXTERNAL 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 SIMA20170903003Power Supply · inoperativeNR 2 AND 3 EMERGENCY LIGHTS FOUND INOPERATIVE. INSTALLED A NEW POWER SUPPLY AND BATTERY IAW AMM 33-50-04, OPS CHECKED GOOD.SDR SIMA20170903004Light · damagedNR 5 EMERGENCY LIGHT IS DAMAGED. REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12.SDR SIMA20170903006Sign · inoperativeSIGN ON AFT SIDE OF G2 GALLEY INOPERATIVE. INSTALLED A NEW POWER SUPPLY AND BATTERY IAW AMM 33-50-04. OPS CHECKED GOOD.SDR SIMA20170903005Light · damagedNR 4 EMERGENCY LIGHT IS DAMAGED ON THE END. REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12.SDR SIMA20170903002Light · damagedR1 AND R7 EMERGENCY LIGHT PROFILES ARE CRACKED AND DAMAGED. REPLACED THE R1 AND R7 EMERGENCY LIGHT PROFILES IAW AMM 33-50-12.SDR ASOA201709034050Battery Pack · dischargedIAH - FLIGHT 4352 DURING PREFLIGHT THE CREW REPORTED AN EMERGENCY EXIT ROW LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SSDR HNAA2017090700302Inverter · inoperativeEMERGENCY EXIT LIGHT ABOVE FA SEAT INOPERATIVE. REMOVED & REPLACED THE EMERGENCY LIGHT DC/AC INVERTER IAW 33-50-11-000/400-801-A. OK FOR SERVICE.SDR HNAA2017090500296Spring · out of adjustCAPT'S WINDSHIELD WIPER WILL NOT PARK AND BOUNCES OFF OF WINDSHIELD AT SPEEDS ABOVE 160 KNOTS. ADJUSTED WIPER ARM SPRING TENSION IAW AMM 30-41-03 OPS CHECK GOOD AT THIS TIME.SDR HNAA2017090700301Light · inoperativeEMERGENCY LIGHT AT ROW 17 INOPERATIVE. R & R EMERGENCY LIGHT ASSY IAW AMM 33-50-08-000/400-802-A, OPS CHECKED GOOD.SDR SIMA20170901001Inverter · inoperativeFWD CABIN CEILING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED THE NR 6 INVERTER FOR THE FWD CEILING EMERGENCY EXIT LIGHT IAW AMM 33-50-11, OPS CHECKED GOOD.SDR SIMA20170831001Sensor · failedDURING CLIMB, RETRACTED FLAPS TO 0 DEGREES ON THE SELECTOR. RECIEVED FLAP FAIL ON EICAS. FLAPS INDICATED 9 DEGREES. RETURNED FOR LANDING AND LANDED. REMOVED AND REPLACED THE RT VELOCITY SENSOR IAW AMM 27-51-12. REMOVED AND REPLACED FLAP CONTROL UNIT IAW AMSDR SIMA2017080230001Door · bindingFA REPORTS MAIN CABIN DOOR DIFFICULT TO OPEN.AIRCRAFT FOUND TO BE WITHIN 5LBS OR LESS THAN THE MAX LOAD CRITERIA (45-50LBS)-C/A-DEFERRED PER FMR REF ETN-EM-52-029 TDMI AUTHORIZATION NUMBER 620T5251. PERFORMED THE ADJUSTMENT OF THE PASSENGER MAIN DOOR IN ACCORDSDR SIMA20170830002Battery · dischargedWHILE PERFORMING PS-1 INSPECTION FOUND NR 4 AND NR 5 FLOOR PROXIMITY EMERGENCY LIGHT STRIPS INOP. REMOVED AND REPLACED NR 3 EMERGENCY BATTERY POWER SUPPLY IAW AMM 33-50-04. OPS CHECK GOOD. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 79752.SDR ASOA201708295099Duct · loosePILOT REPORTED A BURNING ODOR DURING ICE TEST. MX INSPECTED AND FOUND LOOSE DUCTS ON THE NR 1 PACK. SECURED THE DUCTS AND PERFORMED AN ANTI-ICE TEST, OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA201708297012Seal · leakingACFT HAD A STRONG OIL ODOR WHILE THE PACKS WERE BEING POWERED BY THE APU. MAINTENANCE R & R THE STARTER GENERATOR OIL SEAL ASSEMBLY IAW CMM 49-26-01-030-037 AND DECONTAMINATED THE ACFT SYSTEM IAW AMM 21-20-00-100-805-A/700. OPS AND LEAK CHECKED GOOD AND ACFT
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