Embraer EMB-145
Service difficulty reports · 3,003
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 = 'EMB145' 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 = 'EMB145' 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 C2XA04SH276Floorbeam · corrodedSHV-DURING C CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH275Bracket · corrodedSHV-DURING C CHECK THE MAIN DOOR SILL FORWARD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH274Rib · chafedSHV-DURING C CHECK THE LEFT UPPER ENGINE COWLING AFT RIB WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RIB IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH273Firewall · crackedSHV-DURING C CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED IN TWO PLACES AT THE RIGHT UPPER APU MOUNT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FIREWALL IAW EMB 145 SRM 51-40-02 AND EA 5340-01016 REV A. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH271Buttstrap · corrodedSHV-DURING C CHECK THE FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED JUST UNDER THE COCKPIT STEP PANEL. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5320-01115. THE AIRCRAFT WAS APPROVED FOR RETURN TO SESDR C2XA04SH270Sill · corrodedSHV-DURING C CHECK THE LEFT HAND AFT CARGO FLOOR SILL WAS FOUND TO BE CORRODED FROM FRAME 68 TO FRAME 71. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH269Sill · corrodedSHV-DURING C CHECK THE LEFT HAND FORWARD CARGO FLOOR SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH268Sill · corrodedSHV-DURING C CHECK THE RIGHT HAND CENTER CARGO FLOOR SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH267Sill · corrodedSHV-DURING C CHECK THE CARGO DOOR LOWER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR RAIA00405002Wire · disconnectedEMERGENCY EGRESS LIGHT AT ROW 8 INOP. MAINTENANCE REPAIRED WIRE AT LIGHT ASSY.SDR C2XA04SH261Switch · dirtySHV-DURING C CHECK THE LEFT EMERGENCY EXIT FAILED THE WARNING MESSAGE OPERATIONAL CHECK. MAINTENANCE CLEANED DIRT AND DEBRIS FROM THE EMERGENCY EXIT MICRO SWITCH. MAINTENANCE PERFORMED THE OPERATIONAL CHECK IAW EMB 145 AMM 52-21-00-700-801-A AGAIN. THE OPERSDR SIMA200412002Odor · detectedGSO - FLT 3625 - CREW REPORTED A MILD IRRITANT ODOR IN CABIN. SMELLS LIKE EUCALYPTUS OIL OR VICKS VAPOR RUB. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. GROUND RAN AIRCRAFT WITH CREW TO ISOLATE ANY ODORS. NO ODORS NOTED FROM EITHER PACK OR BLEED SYSTEM. SDR RAIA00404016Switch · inoperativeUNABLE TO CROSS START - CROSS BLEED VALVE WOULD NOT OPEN. MAINTENANCE REMOVED AND REPLACED NR 2 BLEED PUSH BUTTON SWITCH.SDR RAIA00404019Wire · shorted5621 - STL - BRAKE 2 OVERHEAT INDICATION. MAINTENANCE DEFERRED NR 2 BRAKE HEAT INDICATION PER MEL 32-40-01. SUBSEQUENTLY CLEARED DMI BY REPAIRING SHORTED WIRE AT PIN A CANNON PLUG P 1090.SDR RAIA00404014Battery · overheatedBAT 1 OVHT MESSAGE ON EICAS. MAINTENANCE REMOVED AND REPLACED NR 1 BATTERY.SDR C2XA04IA051Heater · smokeDURING DESCENT THE CREW REPORTED THAT THE WINDSHIELDS FOGGED UP WITH A BURNING ODOR. THE AIRCRAFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE DEFERRED THE WINDSHIELD HEATING SYSTEM. THE FIRST OFFICER'S WINDSHIELD WAS LATER REMOVED AND REPLACED AND THE DEFERRALSDR C2XA04CL039Light · malfunctionedCLE FLIGHT 2114 THE CREW REPORTED THE EMERGENCY LIGHTS WOULD NOT GO OUT AFTER TESTING. MAINTENANCE PERFORMED A RESET OF THE SYSTEM AND OPERATIONAL CHECKS WERE GOOD.SDR RAIA00404010Rod · out of adjustLOUD SQUEAL COMING FROM PAX DOOR. MAINTENANCE FOUND EXTERNAL DOOR ROD OUT OF RIG AND ADJUSTED ROD. GROUND RAN AND DID CABIN PRESSURE CK.SDR RAIA00404008Odor · detectedLAV SMOKE MESSAGE. MAINTENANCE CHECKED LAV IN CABIN FOR EVIDENCE OR ODOR, RAN LT AND RT PACKS IN AUTO AND MANUAL, UNABLE TO DUPLICATE.SDR C2XA04CL036Proximity Switch · crackedCLE FLIGHT 2826, THE CREW REPORTED THE NOSE GEAR DOORS WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR UPLOCK PROXIMITY SWITCH. OPERATIONAL CHECKS WERESDR SIMA200311204Window Post · corrodedWHILE CHANGING THE CO-PILOTS WINDSHIELD TWO FASTENER HOLES IN THE LOWER AFT CORNER OF THE AIRFRAME OPENING WERE FOUND TO BE CORRODED. ONE OF THE FASTENER HOLES REMAINED WITHIN MANUFACTURERS LIMITS AFTER REMOVAL OF CORROSION. APPLIED ALODINE AND EPOXY PRIMER SDR C2XA04IA047Buss · burnedDURING CRUISE THE PILOT REPORTED A SMOKE ODOR IN THE COCKPIT. THE AIRCRAFT DIVERTED TO MGM WHERE MAINTENANCE COULD NOT DUPLICATE THE SMOKE ODOR. THE AIRCRAFT WAS REPOSITIONED TO IAH WHERE MAINTENANCE FOUND THE CAPTAINS WINDSHIELD BUSS BLOCK TO HAVE EVIDENCE SDR AIA00404002Computer · malfunctioned3512 - LGA - DURING R/O ROLL GOT SPOILERS FAIL MESSAGE. MAINTENANCE RESET STALL PROTECTION COMPUTER AND OPS CHECKED OK.SDR C2XA04IA046Switch · malfunctionedDURING PREFLIGHT INSPECTION THE EMERGENCY LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESET THE EMERGENCY LIGHT ARMING SWITCH AND THE LIGHTING SYSTEM OPERATIONALLY CHECKED GOOD. THE DISCREPANCY WAS THEN CLEARED.SDR SIMA200409701Pressure Switch · malfunctionedRUDDER 1/2 INOP EICAS. FOLLOWED CHECKLIST, MECHNICAL CONTROL NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED NR 2 RUDDER PRESSURE SWITCH IAW AMM. AIRCRAFT RETURNED TO SERVICE. (M)SDR C2XA04BT043Battery · faultyCREW REPORTED DURING PREFLIGHT INSPECTION, EMERGENCY EXIT LIGHT BY PASSENGER DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CHECKED GOOD IAW EMB145 MM 33-50-00.SDR RAIA00403029Transducer · defectiveWING ANTI-ICE TEST FAILED. MAINTENANCE REMOVED AND REPLACED BURST TRANSDUCER.SDR C2XA04CL030Windshield · shortedDTW FLIGHT 2136, THE CREW REPORTED SMOKE IN THE COCKPIT WHEN WINDSHIELD HEAT TURNED ON. MAINTENANCE INSPECTED AND REPLACED THE CAPTAINS WINDSHIELD. OPERATIONAL CHECKS WERE GOOD.SDR RAIA00403031Filter · dirty5717 - STL - BLEED 2 OVER-TEMP MESSAGE. MAINTENANCE CLEANED FAN AIR VALVE FILTER.SDR C2XA04CL027Connector · looseCLE FLIGHT 2031, THE CREW REPORTED THE EMERGENCY EXIT SIGN NEXT TO MAIN CABIN DOOR WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EXIT SIGN AND RESECURED THE INVERTER CONNECTOR. OPERATIONAL CHECKS WERE GOOD.SDR RAIA00403021Switch · dirty3538 - PIT - "SPD BRK LVR DISAGREE" MESSAGE. MAINTENANCE CLEANED THRUST LEVER SWITCHES. HIGH SPEED TAXI CHECKS OK.SDR RAIA00403020Control Unit · malfunctioned3563 - PWM - WHEN THRUST LEVERS ARE ADVANCED SPEED BRAKE LEVER DISAGREE MESSAGE IS DISPLAYED. MAINTENANCE REMOVED AND REPLACED SPOILER CONTROL UNIT.SDR 2XA04SH171Strap · corrodedSHV - DURING C-CHECK THE LEFT FORWARD DIGITAL STRAP FROM FRAME 15 TO FRAME 16.5 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH161Floorbeam · crackedSHV - DURING C-CHECK THE CENTER FLOORBEAM RAMP ANGLE WAS FOUND TO BE CRACKED AT FRAME 21. MAINTENANCE REMOVED AND REPLACED THE CRACKED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR RAIA00403010Starter · inoperativeLT ENGINE WILL NOT START. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE AIR TURBINE STARTER.SDR C2XA04SH160Strap · corrodedSHV - DURING C-CHECK THE AFT LEFT CENTER DIGITAL STRAP WAS FOUND TO BE CORRODED AT FRAME 16 TO FRAME 18. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DIGITAL STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH159Buttstrap · gougedSHV - DURING C-CHECK THE CENTER OMEGA BEAM BUTTSTRAP WAS FOUND TO BE GOUGED AT FRAME 21. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH158Buttstrap · corrodedSHV - DURING C-CHECK, THE LEFT BUTTSTRAP AT FRAME 65 TO FRAME 68 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH157Floorbeam · corrodedSHV - DURING C-CHECK, THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A SHIM FILLER REPAIR IAW EMB 245 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH156Rib · chafedSHV - DURING C-CHECK, THE AFT EDGE MEMBER OF THE NR 2 ENGINE UPPER COWLING WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH155Sill · corrodedSHV - DURING C-CHECK, THE LOWER CARGO DOOR CUTOUT SILL WAS FOUND TO BE CORRODED FROM FRAME 65 TO 68. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH154Structure · corrodedSHV - DURING C-CHECK, THE CROSS MEMBER AT FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH153Stringer · gougedSHV - DURING C-CHECK EXTERNAL STRINGER 19L WAS FOUND TO BE GOUGED BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A REINFORCING ANGLE IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH150Firewall · crackedSHV - DURING C-CHECK, THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RIGHT HAND APU MOUNT. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH149Stiffener · chafedSHV - DURING C-CHECK, THE RIGHT HAND ENGINE LOWER COWLING AFT STIFFENER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH148Floorbeam · corrodedSHV - DURING C-CHECK, THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH147Floorbeam · corrodedSHV - DURING C-CHECK, THE LEFT HAND FLOORBEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE AFFECTED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH146Floorbeam · corrodedSHV - DURING C-CHECK, THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE AFFECTED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04IA030Light · inoperativeDURING SCHEDULED MAINTENANCE THE EMERGENCY LIGHT STRIP AT THE EXIT ROW WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRIP, OPERATIONALLY TESTED THE LIGHTING, AND CLEARED THE DISCREPANCY.SDR C2XA04IA025Connector · looseDURING SCHEDULED MAINTENANCE THE LEFT OVERWING EMERGENCY LIGHT FAILED TO ILLUMINATE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE EMERGENCY LIGHT ASSEMBLY CANNON PLUG LOOSE. THE CONNECTOR WAS RESET, THE LIGHT OPERATIONALLY TESTED AND THE DISCREPANCY CLEA
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