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 SIMA20180608001Connector · missingNUMBER 1 EMERGENCY LIGHT STRIP WIRE MISSING END CONNECTOR. REPLACED MISSING LIGHT STRIP WIRE CONNECTOR IAW SWPM 20-21-00, PERFORMED OPS CHECK IAW AMM 33-50-00, OPS CHECK GOOD. CONNECTOR PIN P/N M39029/31-228.SDR SIMA20180608005Fitting · crackedCRACK IN SHEAR CLIP AT FRAME 62 BETWEEN STRINGERS 4 R AND 5 R. INSTALLED EWIS PROTECTION IAW SWPM 21-20-00 REMOVED CARGO DOOR FWD TORSION BAR SUPPORT AND CARGO DOOR LIFTING CABLE TO FOM IAW AMM 52-32-00. REMOVED TORSION BAR SUPPORT FITTING BETWEEN FRAMES 61 ANSDR SIMA20180608002Fitting · crackedCRACK IN SHEAR CLIP FRAME 79 BETWEEN STRINGER 7L AND 8L. REMOVED SHEAR CLIP IAW SRM 51-40-02. LOCATED, DRILLED AND ALODINED FASTENER HOLES IAW SRM 51-20-03,AND CPM 51-21-04.INSTALLED NEW SHEAR CLIP IAW SRM 51-40-02.SDR SIMA20180608004Channel · corrodedCORROSION IN SERVICE DOOR THRESHOLD BEAM BETWEEN FRAMES 20 AND 22. INSTALLED EWIS PROTECTION IAW SWPM 20-21-00. REMOVED SERVICE DOOR THRESHOLD TRIM AND DISPLACED DOOR SEAL IAW AMM 20-10-01AND 53-21-11.REMOVED CROSSBEAM, 2EA LOWER ANGLES AND SCUFF PLATE TO FOM SDR SIMA20180608007Fitting · crackedCRACK IN SHEAR CLIP AT FRAME 61 BETWEEN STRINGERS 6L AND 7L. REMOVED SHEAR CLIP AT FRAME 61 IAW SRM 51-40-02. LOCATED, DRILLED AND ALODINED FASTENER HOLES ON NEW SHEAR CLIP IAW SRM 51-20-03 AND CPM 51-21-04. INSTALLED NEW SHEAR CLIP IAW SRM 51-40-02, RESTORED SDR SIMA20180608006Fitting · crackedCRACK IN SHEAR CLIP AT FRAME 71 BETWEEN STRINGERS 16L AND 17L. INSTALLED EWIS PROTECTION IAW SWPM 20-21-00. REMOVED CRACKED SHEAR CLIP IAW SRM 51-40-02. LOCATED, DRILLED ALODINED AND PRIMED FASTENER HOLES IN NEW SHEAR CLIP IAW SRM 51-20-03, AND CPM 51-21-04 ANSDR FJTA201806129191Warning Message · activatedCLIMBING THRU FL180, IN ICING CONDITIONS, THE ANTI ICE CAME ON THEN THE NR 2 OIL TEMP WENT TO 147C, BROUGHT THRUST LEVER BACK TO IDLE AND TEMP WENT TO 156 C. STARTED DECENT BACK TO DEPARTURE, LEFT ICING CONDITIONS. THE ANTI TURNED OFF AND THE RIGHT OIL TEMSDR SIMA20180607001Windshield · failedON TAXI OUT CA WINDSHIELD SHATTERED, RETURNED TO GATE "TRANSFERRED TO NRWC 661-ORD-03688". INSTALLED LT WINDSHIELD IAW AMM 56-10-01. LEAK CHECK AND PRESSURIZATION GOOD. RE-TORQUE AFTER PRESSURIZATION COMPLETED.SDR HNAA2018060800119Controller · malfunctionedDURING CLIMB, THE FIRST OFFICER NOTICED THE CABIN PRESSURE CLIMBING, SWITCHED TO MANUAL CONTROL, AND LEVELED OFF AT FL 228. STARTED QRH MEMORY ITEMS FOR RAPID DEPRESSURE, NO EICAS MESSAGES NOTED. INITIATED RAPID DEPRESSURE PROCEEDURE, DUE TO PUTTING CONTROLSDR HNAA2018060800118Oil System · lowNR 1 ENGINE AT MIN DISPATCH. SERVICED THE NR 1 ENGINE WITH 2 QTS OF OIL IAW AMM 12-12-01-03.SDR HNAA2018060800117Warning Message · illuminatedAFTER THE NR 1 ENGINE START, E1-2 SHORT DISPATCH MESSAGE DISPLAYED.SDR SIMA20180606014Fitting · crackedNR 1-2-3-5 LT ISLE FLOOR LIGHT EXTRUSION CRACKED. REMOVED AND REPLACED NR 1,2,3, AND 5 LT ISLE FLOOR LIGHT EXTRUSIONS IAW AMM 33-50-12.SDR SIMA20180606012Skin · crackedRT AFT FUSELAGE HAS A SKIN CRACK AT FRAME 75 ABOVE STRINGER 2R. RAI SERVICEABLE DOUBLER FOR SKIN REPAIR AT FR 75R IAW SRM 53-31-01.SDR SIMA20180606015Battery · dischargedNR 2 EMERGENCY LIGHT BATTERY INOP. REMOVED AND REPLACED NR 2 EMERGENCY LIGHT BATTERY AND CHARGER IAW WC 33-700-19. OP CHECK GOOD.SDR SIMA20180606010Yoke · crackedLT PYLON ENGINE FORWARD LOWER YOKE CRACKED. (BEHIND LOWER FWD ENG MOUNT). REMOVED UNSERVICEABLE AND INSTALLED NEW LT PYLON ENGINE FORWARD LOWER YOKE IAW EO EM-54MR-386.SDR SIMA20180606009Yoke · crackedRT PYLON ENGINE FORWARD LOWER YOKE CRACKED. (BEHIND LOWER FWD ENG MOUNT). REMOVED AND REPLACED RT PYLON ENGINE FORWARD LOWER YOKE IAW EO EM-54MR-386.SDR SIMA20180606011Stringer · corrodedFR22 AND STR15R HAS CORROSION. PERFORMED FR22 STR15 REPAIR IAW ERS-EM-53MR-3332.SDR ASOA201806065152Battery Pack · inoperativeDURING AN INSPECTION, THE FORWARD EMERGENCY LIGHT STRIP WOULD NOT ILLUMINATE. R & R THE BATTERY AND CHARGER, OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA201806076006Control Unit · failedSPOILERS FAILED ON APPROACH, AT APPROXIMATELY 800 FT AGL. COMPLIED WITH QRH PROCEDURES. TROUBLESHOT THE GROUND SPOILER AIR/GROUND CKT FAULT IAW FIM 27-63-00-810-811-A. REMOVED AND REPLACED THE SPOILER CONTROL UNIT IAW AMM 27-63-02. OPS CHECKED IAW AMM 27-63SDR 4VAA201806076002Switch · failedRETURNED DUE TO A LOSS OF CABIN PRESSURIZATION AT FL330, CAPTAIN NOTED RISING CABIN ALTITUDE. DONNED OXYGEN MASKS, DESCENDED TO 10,000. CABIN ALTITUDE REACHED 11,000 WITH ASSOCIATED WARNINGS BEFORE FINALLY STARTING TO GO DOWN.
MAINTENANCE PERFORMED FIM 2SDR SIMA20180606005Floor Support · corrodedCORROSION ON THE CENTER OMEGA BEAM FROM FRAME 52 TO 62 -C/A-REMOVED CORROSION FROM CENTER OMEGA AT FRAME 59 AND FRAME 60 IAW EMB 145 SRM 51-10-03, DAMAGE AT FRAM E 60 FOUND TO BE OUT OF SRM 53-24-10 LIMITS.CUT OUT CORROSION DAMAGE AT FRAME 60 IAW EMB SRM 53-24SDR SIMA20180606002Floor Support · corrodedCORROSION ON THE RT OMEGA BEAM BETWEEN FRAMES 52 AND 62. BLENDED CORROSION IAW SRM 51-10-03, FOUND TO BE CRACKED ON THE INBD SIDE. 0.25 IN LENGTH.DETERMINED TO BE OUT OF LIMITS PER EMB 145 SRM 53-24-10.CUT OUT CRACK IAW EMB 145 SRM 53-24-10, PERFORMED HFEC SDR SIMA20180606003Floor Support · corrodedCORROSION ON THE CENTER OMEGA AT CARBON CROSSMEMBER, FRAME 29. BLENDED THE CORROSION IAW SRM 51-10-03, FOUND TO BE OUT OF LIMITS IAW SRM 53-22-10. CUT OUT THE DAMAGE IAW SRM 53-22-10. PERFORMED HFEC INSPECTION OF CUT OUT AND BLENDED AREAS IAW NDTM 51-00-0SDR SIMA20180606001Bracket · crackedCRACKED BRACKET AT FRAME 14, STRINGER 2L. REMOVED AND REPLACED THE BRACKET IAW SRM 51-40-02, SRM 51-20-03, CPM 51-21-04, AND 51-20-01.SDR SIMA20180605008Flashlight · out of adjustFA FLASHLIGHT INOP. C/A-COMPLETE:PERFORMED ADJUSTMENT OF THE FA FLASHLIGHT IAW AMM 33-51-01. FUNCTION CHECK GOOD.SDR SIMA201806075005Control Panel · malfunctionedFIRE DETECTOR TEST FAILED AT THE NR 2 FIRE HANDLE, LIGHT NOT COMING ON. REMOVED AND REPLACED FIRE DETECTION PANEL AND THE NR 2 FIRE HANDLE IAW AMM 26-00-01, AND 26-21-01. OPS CHECKED GOOD IAW AMM 26-10-00.SDR SIMA2018061404016Light · crackedNR 7 FLOOR EMERGENCY LIGHT STRIP WAS CRACKED. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12.SDR SIMA2018061304015Frame · crackedFRAME 66 IS CRACKED ON UPPER FLANGE BY THE CARGO DOOR SILL.-C/A-COMPLETED FRAME REPAIR OF FRAME 66 IAW SRM 53-00-04 AND 51-40-02.SDR SIMA20180604014Frame · crackedFRAME 67 WAS CRACKED ON THE UPPER FLANGE BY THE CARGO DOOR SILL. REPAIRED THE FRAME IAW SRM 53-00-04, AND 51-40-02.SDR SIMA2018061304013Door Sill · corrodedCARGO DOOR SILL WAS CORRODED, REPLACED THE CARGO DOOR SILL IAW SRM 51-40-02.SDR SIMA201806074011Shear Tie · crackedFRAME 68 SHEAR TIE HAD A ONE INCH CRACK AROUND A LOCK FASTERNER BETWEEN STRINGERS 6L AND 7L. REPAIRED THE SHEAR TIE IAW SRM 53-31-04, AND 51-20-03.SDR SIMA201806064010Inverter · inoperativeEMERGENCY LIGHT IN ROW 3 (B+C SIDE) DID NOT WORK. REMOVED AND REPLACED THE INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD. ACFT OK FOR SERVICE.SDR ASOA201806067098Skin · crackedFUSELAGE SKIN CRACKED AT FRAME 75, STRINGER 2L. CUTOUT THE DAMAGE SECTION, FABRICATED A FILLER, AND DOUBLER. INSTALLED THE REPAIR.SDR SIMA20180604006Fitting · crackedCRACK IN SHEAR CLIP AT FRAME 62 BETWEEN STRINGERS 6R AND 8R. C/A-INSTALLED EWIS PROTECTION IAW SWPM 20-21-00. REMOVED 4 EACH BONDING TABS ON SHEAR CLIP TO FOM IAW SWPM 20-13-05. REMOVED SHEAR CLIP IAW SRM 51-40-02. LOCATED, DRILLED AND ALODINED NEW SHEAR CLIP SDR SIMA201806054003Shear Tie · crackedSHEAR TIE AT FRAME 62, BETWEEN STRINGERS 6L AND 8L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-20-03, CPM 51-21-04, CPM 51-21-05, 51-21-06, AND ETN GN-51-017.SDR SIMA201806054004Shear Tie · crackedSHEAR TIE AT FRAME 67, BETWEEN STRINGERS 6L AND 7L WAS CRACKED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-40-10, FIG 1, SRM 51-20-03, CPM 51-21-04, 51-21-05. CPM 51-21-06, AND ETN GN-51-017.SDR SIMA201806054005Shear Tie · crackedSHEAR TIE AT FRAME 72, BETWEEN STRINGERS 17 L AND 18L WAS FOUND CRACKED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-20-03, CPM 51-21-04 AND 51-21-05.SDR SIMA201806054007Shear Tie · crackedSHEAR TIE AT FRAME 61, BETWEEN STRINGERS 6 R AND 7R WAS CRACKED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-20-03, AND CPM 51-20-04.SDR SIMA201806054008Shear Tie · crackedSHEAR TIE AT FRAME 26, BETWEEN STRINGERS 15R AND 16R WAS FOUND CRACKED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-20-03, CPM 51-21-04, AND 51-20-01.SDR SIMA201806054009Shear Tie · crackedSHEAR TIE AT FRAME 25 BETWEEN STRINGER 15R AND 16R WAS FOUND CRACKED. REMOVED THE SHEAR TIE IAW SRM 51-40-02. LOCATED, DRILLED, AND ALODINE A NEW SHEAR TIE IAW SRM 51-20-03, AND CPM 51-21-04. INSTALLED IAW SRM 51-40-02, AND 51-20-01.SDR SIMA20180604001Shear Tie · crackedCRACKED SHEAR TIE AT FRAME 24 BETWEEN STRINGERS 16R AND 17R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, SRM 51-20-03, CPM 51-21-04, AND 51-20-01.SDR SIMA20180604002Shear Tie · crackedCRACKD SHEAR TIE AT FRAME 24 BETWEEN STRINGERS 15R AND 16R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02. SRM 51-20-03, CPM 51-21-04, AND 51-20-01SDR RAIA201806030001O-Ring · damagedBLEED 2 LEAK IN FLIGHT. ON GROUND MESSAGE WENT AWAY. FOUND AIR LEAKING IN ZONE 270 IN CARGO COMPARTMENT. REPLACED O-RINGS AND RESECURED COUPLINGS 272CRW AND 272BF. NO MORE LEAKS DETECTED. OPS CHECK GOODSDR ASOA2018067035151Control Valve · failedPILOT REPORTED THE MAIN BRAKES WERE LESS EFFECTIVE THAN NORMAL, ALMOST FEELS LIKE THEY WERE OVERHEATED AND GLAZED ON THE DISCS. MX REMOVED AND REPLACED THE OTBD BRAKE CONTROL VALVE, OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA201806035150Control Module · failedPILOT REPORTED AN ODOR, CABIN LIGHT WAS GETTING TOO HOT. MX PERFORMED AN INSPECTION OF THE CABIN LIGHTING AND FOUND CABIN LIGHTING CONTROL MODULE AND 1A LIGHT BALLAST BAD. REMOVED AND REPLACED LIGHT CONTROL MODULE AND BALLAST, OPS CHECKED GOOD. ACFT WAS ASDR SIMA201806063003Smoke Detector · no testCARGO FIRE LIGHT INDICATOR NOT WORKING. DOES NOT TEST. REMOVED & REPLACED THE AFT CARGO AFT SMOKE DETECTOR IAW 26-15-01. OPS CHECKED GOOD. ACFT OK FOR SERVICE.SDR SIMA2018060403001Controller · failedLOST PRESSURIZATION DURING DESCENT, CABIN ALTITUDE 8000 FT AND INCREASING DESCENDED AS SOON AS POSSIBLE TO 10,000 FT, CABIN ALTITUDE REACHED 11,000 FT. CABIN REMAINED UNPRESSURIZED FOR REMAINDER OF FLIGHT. OXYGEN MASKS DID NOT DEPLOY. REMOVED AND REPLACED TSDR ASOA2018060625149Battery Pack · inoperativeDURING A MX INSPECTION, THE NR 2 EMERGENCY LIGHT BATTERY WAS INOPERATIVE. MX REMOVED AND REPLACED THE BATTERY. OPS CHECKED GOOD. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA2018060625148Control Module · failedFLIGHT ATTENDANT CONTROL PANEL, CABIN LIGHTS INOPERATIVE, SMELLED ELECTRICAL SMOKE. MX REMOVED AND REPLACED PSU LIGHT CONTROL MODULE, AND 1A BALLAST, OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA2018060420003Lamp · inoperativeSERVICE DOOR EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A, AND 33-50-10-000-801-A. OPS CHECKED GOOD.
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