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 ASOA201802117009Battery · not reportedEMERGENCY LIGHT BATTERY NEEDS REPLACED. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY NR 4. OPS CK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.SDR SIMA20180208003Yoke · crackedLEFT ENGINE FORWARD YOKE I RADIUS CRACKED. COMPLIED WITH EO-EM-54MR-386.SDR SIMA20180207006Frame · crackedFRAME 66 IS CRACKED ON THE TOP FLANGE BETWEEN STRINGERS 18 AND 19L. REPAIRED THE FRAME IAW SRM 53-00-04.SDR SIMA20180207001Warning Message · false activationWING ANTI ICE FAILED WHEN OVERRIDE KNOB IN THE ALL POSITION, FAULT CODE 301M0200. FOLLOWING FIM 30-11-00-810-803-A, ITEM 1, PERFORMED AN OPS CHECK IAW AMM 30-00-00. OPS CHECKED GOOD. NO MESSAGE NOTED.SDR SIMA20180207004Engine · contaminatedCLIMBING OUT OF 16,000 FT, AN ODOR OF BURNING RUBBER WAS IN THE COCKPIT AND GALLEY. ODOR CAME AND WENT IN WAVES. FOUND EXCESSIVE AMOUNT OF DEICE FLUID IN THE NR 1 ENGINE AND APU COWLINGS, CLEANED. PERFORMED ENGINE RUNS IAW MM 72-00-00, AND NO DEFECTS NOTESDR SIMA20180207005Bulb · inoperativeMAIN DOOR EMERGENCY LIGHT INOPERATIVE. R & R THE BULB AND OPS CHECKED GOOD IAW AMM 33-50-06.SDR SIMA20180207003Shear Tie · crackedSHEAR TIE AT FRAME 65 BETWEEN STRINGERS 18L AND 19L WAS CRACKED. REMOVED AND REPLACED THE SHEAR TIE AW SRM 51-40-02.SDR ASOA201802077007Skin · dentedTYS A/C IS IN A C-CHECK STATUS WHEN INSPECTION FOUND FUSELAGE DENTED BETWEEN FRAME 20-21 STR-11L AND 12L. MAINTENANCE REPAIRED AREA IAW ETD 2018-002931. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR ASOA201802077005Skin · dentedTYS A/C WAS IN A-CHECK STATUS WHEN INSPECTION FOUND A DENT AT FR. 7 BELOW LT WIPER. MAINTENANCE REPAIRED THE DENT IAW ETD 2018-002936. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR SIMA20180206008Trunnion · crackedRIGHT MLG AFT UPPER TRUNNION IS CRACKED. REPLACED THE TRUNNNION IAW ERS-EM-57MR-916.SDR SIMA20180206009Trunnion · crackedLEFT MLG AFT TRUNNION HAS AN APPROXIMATELY 1.5 INCH CRACK ON THE OTBD RADIUS. REPLACED THE LT MLG AFT TRUNNION IAW WER-EM-57MR-917.SDR RAIA201802060001Skin · crackedFUSELAGE SKIN HAS CRACKS AT FRAME 78 BETWEEN STRINGERS 6L - 8L. CUTOUT THE DAMAGE AND INSTALLED A DOUBLER.SDR SIMA20180206007Frame · crackedFRAME 67 IS CRACKED ON TOP FLANGE BETWEEN STRINGERS 18 AND 19L. INSTALLED A NEW FRAME SECTION AND SPLICE IAW SRM 53-00-04, AND 51-40-02.SDR SIMA20180206006Attach Fitting · damagedLEFT AILERON PCA ATTACH FITTING IS DAMAGED. REPAIRED IAW EO EM-27MR-112SDR HNAA2018020700026Bulb · inoperativeOVERHEAD EMERGENCY LIGHT AT THE PAX DOOR WAS FOUND INOPERATIVE. R & R THE BULB.SDR SIMA20180206005Attach Angle · crackedRIGHT WING TO FUSELAGE LATERAL FAIRING LOWER ATTACH ANGLE CRACKED AT FRAME 47, 4TH ONE AFT. REMOVED AND REPLACED THE ATTACH ANGLE IAW ETN-EM-53-142.SDR SIMA20180206002Attach Angle · crackedRIGHT HAT BEAM ATTACH ANGLE CRACKED BETWEEN FRAMES 47 AND 48. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 53-23-02.SDR SIMA20180206003Support · crackedCARGO BAY DOOR HOLD OPEN STRUT SUPPORT IS CRACKED ON THE BACK SIDE IN 2 PLACES, REPLACED THE DOOR HOLD OPEN STRUT SUPPORT IAW SRM 51-40-02.SDR SIMA20180206004Attach Angle · crackedRIGHT WING TO FUSELAGE LATERAL FAIRING LOWER ATTACH ANGLE CRACKED AT FRAME 48, 5TH ONE AFT. INSTALLED A NEW ATTACH ANGLE BETWEEN FRAMES 48 AND 49 IAW ETN-EM-53-142, AND SRM 51-40-02.SDR SIMA20180205008Bracket · damagedCARGO FLOOR SUPPORT BRACKETS AT FRAMES 66 AND 67 BENT AND CRACKED. INSTALLED A NEW FLOOR SUPPORT BRACKET IAW SRM 51-40-02.SDR SIMA20180205006Frame · crackedPILOTS SIDE FRAME 10LT. IS CRACKED APPROX. 1/2" BELOW DV WINDOW SILL. INSTALLED NEW FRAME SEGMENT BELOW THE DV WINDOW IAW SRM 51-40-02.SDR SIMA20180205007Frame · crackedFIRST OFFICER`S SIDE FRAME 10 LT. IS CRACKED APPROXIMATELY 1 INCH BELOW THE DV WINDOW SILL. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02.SDR SIMA20180205005Support · crackedCARGO DOOR TORSION BAR SUPPORT AT FRAME 61 RT. IS CRACKED APPROXIMATELY .250. REMOVED AND REPLACED CARGO DOOR TORSION BAR SUPPORT IAW SRM 51-40-02.SDR SIMA20180205003Attach Angle · crackedRIGHT WING TO FUSELAGE LATERAL FAIRING LOWER ATTACH ANGLE CRACKED BETWEEN FRAMES 48 AND 49, 6TH ONE AFT. FABRICATED A NEW ATTACH ANGLE IAW ETN-EM-53-142, AND SRM 51-40-02.SDR SIMA20180205004Attach Angle · crackedLEFT WING TO FUSELAGE LATERAL FAIRING LOWER ATTACH ANGLE 4TH ONE AFT OF FRAME 48 CRACKED. REMOVED AND REPLACED THE ATTACH ANGLE IAW ETN-EM-53-142, AND SRM 51-40-02.SDR ASOA201802053006Actuator · faultyTHE CREW REPORTED AN AUTO TRIM FAIL INFLIGHT WITH PITCH TRIM GOING TO DASHES ON INDICATION. MAINTENANCE INSPECTED AND REPLACED THE HORIZONTAL STAB ACTUATOR IAW 27-40-02. OPS CHECKED GOOD.SDR RAIA201802040001Line · not reportedBLEED 1 OVERTEMP EICAS MESSAGE AFTER TAKEOFF. R & R THE NR 1 FAN AIR CONTROL THERMOSTAT LINE. OPS CHECKED GOOD.SDR SIMA20180204001Uplock · failedLOUD RHYTHIMIC BANGING NOISE FROM NOSE WHEEL AREA AFTER RETRACTING GEAR ON TAKE OFF. GEAR INDICATED UP. NOISE WENT AWAY AFTER GEAR WAS DOWN. NO RELATED NLG CMC MESSAGES. REMOVED AND REPLACED NLG UPLOCK BOX IAW AMM 32-33-07. LANDING GEAR NORMAL AND EMERGENSDR SIMA20180204003Flashlight · inoperativeAFT CABIN FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM 33-50-16. TESTED SATISFACTORY.SDR SIMA20180204002Wire · brokenSERVICE DOOR LINING EMERGENCY LIGHT INOPERATIVE. FOUND A BROKEN WIRE DURING VISUAL INSPECTION. SPLICED THE WIRE IAW SWPM-2430-20-21-00. OPS CHECKED GOOD. NO FURTHER DISCREPANCIES FOUND.SDR SIMA20180202003Power Supply · failedLEFT AND RIGHT OVERWING EXTERNAL EMERGENCY LIGHTS FAILED TO ILLUMINATE. TROUBLESHOT IAW WM 33-50-50, AND R 7 R THE NR 4 EPSU IAW AMM 30-50-04. OPS CHECKED GOOD. BATTERY CHARGER ASSY.SDR SIMA20180202002Wire Harness · failedRECEIVED A LANDING GEAR AIR/GND FAIL CAUTION MESSAGE DURING CLIMBOUT. COULD NOT BRING GEAR UP. MESSAGE EXTINGUISHED 2 MINUTES LATER. BROUGHT GEAR UP. LANDED BACK AT DEPARTURE, GEAR DOWN. REMOVED AND REPLACED NLG AIR /GROUND WOW PROXIMITY SENSOR NR 2 IAW AMM 32SDR SIMA20180202004Sign · inoperativeEXIT SIGN ABOVE THE FLIGHT ATTENDANT SEAT IS INOPERATIVE. REMOVED AND REPLACED THE SIGN, OPS TESTED GOOD IAW AMM 33-50-00.SDR HNAA2018020500025Connector · failedNO TAKEOFF CONFIGURATION EICAS MESSAGE DISPLAYED DURING TAKEOFF ROLL. PARKING BRAKE LIGHT ILLUMINATED WHEN THRUST LEVERS WERE ADVANCED. TAKEOFF CONFIGURATION TESTED OK PRIOR TO TAKEOFF ROLL. R & R THE CONNECTOR IAW SWPM 20-50-01. OPS CHECKED IAW AMM 32SDR RAIA201802080002Support · damagedLT OMEGA BEAM SUPPORT AT FR 29 HAS DAMAGED/ELONGATED FASTENER HOLES. R & R LT OMEGA BEAM SUPPORT AT FR 29. SUPPORTING DOCUMENTS EMAILED TO PROGMGR UNDER THE SUBJECT: SDR RAIA201802010002.SDR RAIA201802010001Valve · defectiveA/C WOULD NOT PRESSURIZE AFTER TAKE OFF. R & R GROUND CONNECTION VALVE. PERFORMED OPS CHK OF PRESSURIZATION OPS CHECK GOOD.SDR HNAA2018020200024Heater · failedNR 3 PITOT INOPERATIVE CAUTION MESSAGE ON EICAS, FOUND HEATING ELEMENT WIRES BURNED. THE NR 3 PITOT HEAD WILL NOT HEAT. R & R PITOT STATIC SENSOR IAW AMM 34-13-02. OPS AND LEAK CHECKED GOOD IAW AMM 30-31-00. REPAIRED WIRING IAW SWPM 20-21-00.SDR SIMA20180201002Controller · failedCABIN ALTITUDE WARNING AT FL 250. TROUBLESHOT AND FOUND THE AUTO PRESSURIZATION DIGITAL CONTROLLER DISPLAY ELEVATION SWITCH TO BE STICKING. SUSPECT DIGITAL CONTROLLER IS BAD. REPLACED DIGITAL CONTROLLER IAW AMM 21-31-01-000-801-A, & 21-31-01-400-801-A. PERSDR SIMA20180201004Sign · inoperativeDURING A CHECK, FOUND EMERGENCY EXIT SIGN IN THE FRONT OF SEAT 3B TO BE INOPERATIVE. REMOVED AND REPLACED THE SIGN IAW AMM 33-50-13. OPS CHECKED IAW AMM 33-50-00, CHECKED GOOD. NO DEFECTS NOTED.SDR HNAA2018020200023Pressure Switch · faultedNO TAKEOFF CONFIG EICAS MESSAGE DUE TO PARKING BRAKE ON LIGHT REMAINED ILLUMINATED WITH PARKING BRAKE OFF. TAKEOFF CONFIG BUTTON STILL SAYS OK WHEN PRESSED. EICAS MESSAGE APPEARS WHEN POWER LEVERS ARE AVANCED. INSPECTED THE EMERGENCY BRAKE SYS IAW FIM 32-44SDR SIMA20180201001Lamp · inoperativeLEFT AFT EXTERIOR OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS. OPS CHECKED GOOD IAW AMM 33-50-10.SDR RAIA201801310002Clamp · looseBLEED 2 LEAK ON CLIMB OUT FOUND HIGH STAGE VLV CLAMP LOOSE AND TIGHTENED. FOUND BLEED VALVE NR 2 CLAMP LOOSE AND TIGHTENED. RAN THE LEAK CHECK AT 90%. NO LEAKS NOTED AT THIS
TIME.SDR RAIA201801310001Valve · defectiveUNABLE TO PRESSURIZE AIRCRAFT AFTER TAKE OFF. R&R GROUND CONNECTION VALVE PERFORMED OPS CHECK OF PRESSURIZATION, OPS CHECK GOOD.SDR HNAA2018020100018Relay · failedNO TAKEOFF CONFIGURATION EICAS MESSAGE DUE TO PARKING BRAKE ON LIGHT REMAINED ILLUMINATED WITH PARKING BRAKE OFF. OPS CHECK OF THE EMERGENCY PARKING BRAKE HANDLE RELAY K0212, MADE A FEW CLICKING NOISES WITH IN A SECOND WITH BRAKE LIGHT COMING ON ASDR HNAA2018020100016Switch · out of rigNR 2 ENGINE THRUST REVERSER DISAGREE MESSAGE DISPLAYED DURING TAKE OFF ROLL, ABORTED TAKEOFF. ENGAGED THE NR 2 THRUST REVERSER SYSTEM & OPS CHECKED. DISCREPANCY REMAINS. INSPECTED, & FOUND THE NR 2 THRUST REVERSER SWITCHES ON THE THRUST LEVER OUT OF RIG. ASDR SIMA20180130009Structure · corrodedLEFT OTBD FLAP, OTBD ROLLER BUSHING BORE IS CORRODED. REMOVED AND REPLACED THE LT OTBD FLAP ASSY IAW AMM 27-50-00.SDR HNAA2018020100021Relay · failedPARKING BRAKE ON LIGHT ILLUMINATED. R & R THE PARKING BRAKE RELAY K0212. OPS CHECKED OK.SDR RAIA201801300002Sensor · looseNR 2 BLEED LEAK IN FLT, WHILE CLIMBING THROUGH 13,000 FEET. QRH PERFORMED, NO CHANGE. SECURED A LOOSE TEMP SENSOR ON THE DUCT FORWARD OF THE NR 2 PRE COOLER. OPS CHECKED GOOD.SDR SIMA20180130006Unknown · malfunctionedRUDDER PEDALS LOCKED UP. INSPECTED STEERING SYSTEM, PERFORMED OPS TEST OF STEERING SYSTEM AND TAXI RUN WITH CREW IAW AMM 32-50-0, OPS CHECK GOOD.SDR SIMA20180130005Unknown · malfunctionedON SHORT FINAL MASTER WARNING ON EICAS PTRIM MAIN INOP AND PTRIM BACKUP INOP. STAYED ON A COUPLE SECONDS THEN WENT AWAY. FOUND MSG CTRL WHEEL TRIM SW FAIL 3 OCCURENCES. PERFORMED A/C RESET AND STAB ELECTRONIC OPS CHECK IAW AMM 27-40-00. OPS CHECK GOOD. FOUND T
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