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 C2XA09SH418Bushing · migratedSHV - DURING C-CHECK RT SPRING TAB OTBD PANEL ATTACH BRACKET INBD HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED RT SPRING TAB OTBD PANEL ATTACH BRACKET IAW AMM 20-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA200931304Skin · crackedDURING MAINTENANCE BASE VISIT INSPECTION MULTIPLE CRACK LIKE INDICATIONS WERE NOTED ON THE EXTERIOR SKIN AROUND RIVET HEADS AT FRAMES 77, 78 AND 79 BETWEEN STRINGERS 3L AND 7L AND BETWEEN 3R AND 7R. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED FASTENERS ANSDR C2XA09SH404Frame · crackedSHV - DURING C-CHECK LT FRM 10 UNDER DV WINDOW CUTOUT IS CRACKED. MAINTENANCE REMOVED AND REPLACED FUSELAGE FRAME 10 LT SIDE IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH395Bushing · migratedSHV - DURING C-CHECK LT GROUND SPOILER I/B HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED LT GROUND SPOILER I/B HAT BUSHING IAW EC5740-01152 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA200930003Sill · corrodedDURING INSPECTION FOUND THE CARGO DOOR SILL CORRODED AT FRAME 66. AIRCRAFT REMOVED FROM SERVICE. REPLACED CARGO DOOR SILL IN ACCORDANCE WITH EMBRAER SRM 51-40-02. THE AIRCRAFT RETURNED TO SERVICE.SDR SIMA200930101Web · crackedDURING INSPECTION FOUND THE NOSE LANDING GEAR SUPPORT WEB TO BE CHAFED, FOUND IT ALSO TO HAVE A CRACK 3.5 MM LONG. THE AIRCRAFT HAS BEEN REMOVED FROM SERVICE. REPAIRED THE NOSE LANDING GEAR BAY SUPPORT IAW EO EM-5300-1470. THE AIRCRAFT WAS RETURNED TO SERVISDR SIMA200924301SUPBattery · inoperativeDURING MAINTENANCE INSPECTION, ROWS NUMBERED 1-3 EMERGENCY LIGHTS AND SERVICE DOOR OVERHEAD LIGHT WERE FOUND TO BE INOPERABLE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NUMBER 2 BATTERY AND CHARGER IAW 33-700-19 MANUAL. OPERATIONAL CHECK GOOD.SDR SIMA200928904Skin · crackedDURING MAINTENANCE INSPECTION, FOUND MULTIPLE CRACK LIKE INDICATIONS ON EXTERIOR SKIN AROUND RIVET HEADS AT FRAMES 77, 78 AND 79 BETWEEN STRINGERS 3L AND 7L AND 3R AND 7R. AIRCRAFT REMOVED FROM SERVICE. REMOVED FASTENERS & REAMED HOLES TO REMOVED SKIN CRACKSSDR C2XA09RI169Door · stuckFLIGHT 2504 - JAX - FLIGHT CREW REPORTED PAX DOOR WILL NOT OPEN FROM INSIDE. MX VERIFIED DOOR OPERATION AND COULD NOT DUPLICATE THE PROBLEM ACFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA09TY242Roller · faultyPAX DOOR HARD TO CLOSE. REMOVED AND REPLACED AFT PAX DOOR ROLLER IAW EMB 145 AMM 53-21-02 AND RIGGED DOOR IAW AMM 52-18-00. OPS CHECK GOOD.SDR SIMA200925301Drive Unit · malfunctionedON FLIGHT 3962 DURING CRUISE A FLAP FAIL MESSAGE APPEARED AND REMAINED ON EICAS. THE FLAPS FAILED AT 0 DEGREES. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. THE AIRCRAFT WAS INSPECTED TO THE EXTENT NECESSARY FOSDR C2XA09SH295Fitting · wornSHV - DURING C-CHECK LT SPEED BRAKE CENTER HINGE POINT I/B HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED LT SPEED BRAKE CENTER FITTING IAW EMB145 SRM 51-40-02 AND LT SPEED BRAKE ACTUATOR IAW EMB145 AMM 27-62-02. THE AIRCRAFT WAS APPROVED FOR RETURN SDR CHQA200900194Warning System · activatedON TAKEOFF FROM IAD THE CREW RECEIVED A MASTER WARNING OF "TAKEOFF TRIM". THE TAKEOFF WAS ABORTED WITHIN 5 KTS OF V1. AFTER CLEARING THE RUNWAY AND COMPLETING THE CHECKLISTS THE "BRAKES OVERTEMP" MESSAGE APPEARED. TAXI CONTINUED SLOWLY UNTIL TAXIWAY "Y" WASSDR C2XA09SH202Frame · corrodedDURING C-CHECK SERVICE DOOR CUT-OUT LWR NUT PLATE HOLE AT FRAME 22 HAS CORROSION. MX REPAIRED SERVICE DOOR CUT-OUT LOWER NUT PLATE HOLE AT FRAME 22 IAW EC5310-01373. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH201Mount · crackedDURING C-CHECK ENG NR 2 FWD YOKE LWR MOUNT CRACKED. MX PERFORMED AND COMPLETED REPAIR OF NR 2 FWD YOKE LWR MOUNT IAW EC5450-01027. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH200Skin · damagedDURING C-CHECK 4 WORKING RIVETS, FRAME 75 STRINGER 1L-2L. MX REPAIRED 2 REAMED RIVET HOLES IAW EC5330-01938 AND INSTALLED 2 RIVETS IAW SRM 51-40-02 AND PREPPED, PRIMED AND RESTORED ORIGINAL FINISH IAW CPM 51-21-06 AT FRAME 75, STRINGER 1L-2L. THE ACFT WAS APSDR C2XA09SH199Skin · crackedDURING C-CHECK CRACK AROUND RIVETS FRAME 75 STRINGER 1R (EXTERNAL FUSELAGE). MX REPAIRED 2 REAMED RIVET HOLES IAW EC5330-01938 AND INSTALLED RIVETS AT FRAME 75 STRINGER 1R IAW SRM 51-40-02 AND PREPPED, PRIMED AND RESTORED ORIGINAL FINISH IAW CPM 51-21-06. THSDR C2XA09SH198Bushing · migratedDURING C-CHECK RT GROUND SPOILER OTBD ATTACH BRACKET INBD HAT BUSHING IS MIGRATED. MX COMPLETED REPAIR OF RT GROUND SPOILER OTBD ATTACH BRACKET INBD HAT BUSHING IAW EC5740-01152 REV B. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH197Bushing · migratedDURING C-CHECK RT SPEED BRAKE ACTUATOR ATTACH BRACKET ON SPEED BRAKE INBD HAT BUSHING IS MIGRATED. MX COMPLETED REPAIR OF RT SPEED BRAKE ACTUATOR ATTACH BRACKET ON SPEED BRAKE INBD HAT BUSHING IAW EC5740-01152 REV B. THE ACFT WAS APPROVED FOR RETURN TO SERVISDR C2XA09SH196Bushing · migratedDURING C-CHECK RT GROUND SPOILER INBD ATTACH BRACKET OTBD HAT BUSHING IS MIGRATED. MX COMPLETED REPAIR OF RT GROUND SPOILER INBD ATTACH BRACKET OTBD HAT BUSHING IAW EC5740-01152 REV B. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH195Bushing · migratedDURING C-CHECK RT GROUND SPOILER ACTUATOR ATTACHMENT BRACKET ON GROUND SPOILER INBD HAT BUSHING WAS MIGRATED. MX COMPLETED REPAIR OF RT GROUND SPOILER ACTUATOR ATTACH BRACKET ON GROUND SPOILER INBD HAT BUSHING IAW EC5740-01152 REV. B. THE ACFT WAS APPROVED TSDR C2XA09CL098Sign · inoperativeDURING ROUTINE MX LT EMERGENCY EXIT SIDEWALL SIGN WAS FOUND INOPERATIVE. MX REPLACED EXIT SIGN AND OPS CHECKS WERE GOOD .SDR C2XA09RI123Seal · dirtyFLIGHT 2893 - EWR - FLIGHT CREW REPORTED MAIN CABIN DOOR HARD TO OPEN AND CLOSE. EWR MX CLEANED CABIN DOOR SEAL AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.SDR SIMA200914503SUPEngine · leakingON FLIGHT 3987, DURING ROTATION DETECTED ELECTRICAL SMOKE THEN AT 500 FEET CREW RECEIVED A LAV SMOKE WARN. ODOR LINGERED UNTIL CREW WAS BACK AT THE GATE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT ENGINE. DEFECTS NOTED. OPS CHECK GOOD. AIRCSDR SIMA200914503Engine · odorON FLIGHT 3987, DURING ROTATION SMELLED ELECTRICAL SMOKE THEN AT 500 FEET CREW RECEIVED A LAV SMOKE WARN. ODOR LINGERED UNTIL CREW WAS BACK AT THE GATE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT ENGINE. DEFECTS NOTED. OPS CHECK GOOD. AIRCRSDR C2XA09SH144Floor Support · corrodedSHV-DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FRAME 29. MAINTENANCE REMOVED CORROSION IAW EMB-145 SRM 53-22-10 AND INSTALLED FABRICATED REPAIR AT FRAME 29 IAW EMB-145 SRM 53-00-10 AND CPM 51-21-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09RI084Control Panel · corrodedFLIGHT 2548 - EWR - FLIGHT CREW REPORTED EMERGENCY LIGHTS INTERMITTENT. EWR MX CLEANED OFF CORROSION FROM F/A CONTROL PANEL AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA09RI085Valve · defectiveFLIGHT 2812 - AMA - FLIGHT CREW REPORTED THAT TOWER NOTIFIED THAT ACFT WAS LEAKING FUEL FROM LEFT WING. CREW PROCEEDED WITH AIR RETURN AND LANDED ACFT UNEVENTFULLY. MX REMOVED AND REPLACED FLAP VALVE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APSDR C2XA09IA109Flapper Valve · leakingAMA - FLIGHT 2812, DURING TAKEOFF THE CREW REPORTED A SUSPECTED FUEL LEAK FROM THE LT WING. THE AIRCRAFT RETURNED TO AMA WHERE IT LANDED WITHOUT INCIDENT. CONTRACT MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE LEFT FLAPPER VALVE, OPERATIONASDR RAIA2009042700005Uplock · malfunctionedFLT 5571 - STL - RIGHT MLG WOULD NOT RETRACT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MLG UPLOCK BOX. OPERATIONAL CHECK OF THE EXTENSION AND RETRACTION SYSTEM CHECKED GOOD.SDR RAIA2009042700003Proximity Switch · false activationFLT 5535 - STL - CREW RECEIVED A RIGHT MAIN LANDING GEAR UNSAFE INDICATION SHORTLY AFTER TAKEOFF. MAINTENANCE REMOVED AND REPLACED THE RIGHT MLG DOWNLOCK PROXIMITY SWITCH. LANDING GEAR EXTENSION AND RETRACTION SYSTEM OPS CHECKED GOOD.SDR C2XA09TY063AConnector · looseSEAT 12BC SIDEWALL AFT EMERGENCY LIGHT INOP. FOUND CONNECTOR LOOSE. TIGHTENED CONNECTOR AND OPS CHECKED GOOD. IAW EMB 145 AMM 33-50-14SDR RAIA2009042000004Inverter · inoperativePRE FLT 5540 - STL - EMERGENCY LIGHT IN CABIN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT INVERTER. SYSTEM OPS CHECKED GOOD.SDR RAIA2009041600004Light · malfunctionedPRE FLT 5540 - STL - CABIN EMERGENCY LIGHT INOPERATIVE. MAINTENANCE RESET THE AIRCRAFT POWER AND CYCLED THE EMERGENCY LIGHT SWITCH. LIGHT OPS CHECKED GOOD. NO DEFECTS NOTED.SDR C2XA09SH114Floor Support · corrodedSHV-DURING C-CHECK CENTER OMEGA BEAM (FR 25-29) HAS PITTING ON I/B FLANGE. MAINTENANCE REMOVED PITTING CORROSION, ALODINED, PRIMED AND PAINTED BLENDED AREA ON CENTER OMEGA BEAM FR 25-29 ON I/B FLANGE IAW CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SDR C2XA09SH113Floor Support · corrodedSHV-DURING C-CHECK (FR 26) LT OMEGA BEAM I/B FLANGE HAS CORROSION AT NUTPLATE. MAINTENANCE REMOVED AND REPLACED NUTPLATE AT FR 26 LT OMEGA BEAM I/B FLANGE IAW EC5320-01137 AND ALODINED, PRIMED AND PAINTED BLENDED AREA ON LT OMEGA BEAM I/B FLANGE NUTPLATE FR 2SDR C2XA09SH112Floor Support · corrodedSHV-DURING C-CHECK LT OMEGA BEAM I/B FLANGE HAS PITTING (FR 30-31). MAINTENANCE REMOVED CORROSION AND ALODINED, PRIMED AND PAINTED BLENDED AREA ON LT OMEGA BEAM I/B FLANGE FR 30-31 IAW EMB-145 CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH111Floor Support · corrodedSHV-DURING C-CHECK CENTER OMEGA BEAM AT FR 25 HAS CORROSION AT NUTPLATE. MAINTENANCE REMOVED CORROSION AND CLEANED, ALODINED, PREPPED, PRIMED AND TOPCOATED CENTER OMEGA BEAM AT FR 23-26 IAW EMB-145 CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICSDR C2XA09SH110Beam · corrodedSHV-DURING C-CHECK BAGGAGE DOOR CUT-OUT LOWER BEAM HAS CORROSION. MAINTENANCE REMOVED AND INSTALLED NEW BAGGAGE DOOR CUTOUT LWR BEAM IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH109Frame · corrodedSHV-DURING C-CHECK CORROSION AROUND RIVETS AT FR 61 STR 16L-15L. MAINTENANCE REMOVED CORROSION IAW EMB-145 CPM 51-21-04 AND CPM 51-21-05. MAINTENACE COMPLETED INSTALLATION OF CARBON SUPPORT DOUBLER AT FR 61 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVESDR RAIA2009040700002Wire · brokenPRE FLT 5540-STL - FLOOR PROXIMITY LIGHT IN THE AFT CABIN INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT THE LIGHT. OPS CHECKED GOOD.SDR C2XA09SH108Valve · unknownSHV - AIRCRAFT N15980 WAS GIVEN A FERRY FLIGHT RELEASE PERMIT FROM DFW TO SHV BECAUSE PACK VALVE 1 CLOSED, COULD NOT RESET. CABIN ALT RAISED PASSED 8,000FT UP TO 14,000FT AT 14:00. EMERGENCY DESCENT WAS PERFORMED. ALSO, O2 MASKS DEPLOYED COMING OUT OF OKC. SDR C2XA09SH107Relay · inoperativeSHV - AIRCRAFT N15980 WAS GIVEN A FERRY FLIGHT RELEASE PERMIT FROM DFW TO SHV BECAUSE OF AN AIR GROUND SENSOR FAIL ON T/O OUT OF OKC AND WAS UNABLE TO RETRACT THE LANDING GEAR, THEN IT WENT AWAY AND GEAR RETRACTED (CAME UP). MAINTENANCE IN SHV REMOVED AND REPSDR C2XA09SH106Skin · corrodedSHV - DURING C-CHECK HORIZONTAL STAB RT LEADING EDGE HAS CORROSION AROUND RIVET HEADS AT UPPER & LOWER SURFACE. MAINTENANCE REMOVED CORROSION AROUND RIVET HEADS AT UPPER & LOWER SURFACE ON HORIZONTAL STABILIZER RT LEADING EDGE WITH POLISHING PROCEDURE IAW EC5SDR C2XA09SH105Skin · corrodedSHV - DURING C-CHECK HORIZONTAL STAB LT LEADING EDGE HAS CORROSION AROUND RIVET HEADS AT UPPER & LOWER SURFACE. MAINTENANCE REMOVED CORROSION AROUND RIVETS AND COMPLETED POLISHING PROCEDURES ON LT LEADING HORIZONTAL EDGE IAW EMB-145 EC5530-01116 REV D - 80 PESDR C2XA09TY056Fitting · wornRT AILERON OUTBOARD PCA ROD BRACKET OUTBOARD BUSHING HOLE IS OUT OF LIMITS. REMOVED AND REPLACED PCA FITTING IAW EC 5750-01177. AIRCRAFT IS STILL IN C-CHECK.SDR RAIA2009040200002Wire · brokenPRE FLT 5540 - STL - EMERGENCY PATH LIGHT AT THE REAR OF THE AIRCRAFT INOPERATIVE. MAINTENANCE RESECURED THE WIRING TO THE EMERGENCY LIGHT STRIP. OPERATIONAL CHECK OF THE LIGHT PROVED GOOD FIX.SDR C2XA09SH085Skin · corrodedSHV - DURING C-CHECK CORROSION FOUND ON INTERNAL SKIN AT STR 19L JUST FWD OF FR 61. MAINTENANCE REMOVED CORROSION IAW EMB 135/145 SRM 51-40-02 AND SRM 51-10-03. PREPPED, ALODINED AND PRIMED INTERNAL SKIN IAW EMB 135/145 CPM 51-21-04 AND CPM 51-21-05. INSTALSDR SIMA200908502Duct · meltedON FLIGHT 9800 CREW REPORTED ON CRUISE A SLIGHT BURNING SMELL IN COCKPIT. SMELL WAS NOT NOTICED IN CABIN. CREW SELECTED A COOLER TEMP ON LEFT PACK SMELL DISSIPATED. SELECTED WARMER ON LEFT PACK SMELL RETURNED. TURNED LEFT PACK OFF SMELL WENT AWAY. KEPT PASDR C2XA09SH081Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT CARBON CROSSBEAM ATTACHMENT POINT, FR 49. MAINTENANCE REPAIRED CORRODED AREA ON LT OMEGA BEAM (CORRODED AREA) AT FRM 49 IAW IC2009-145/00816. ALODINED, PRIMED AND PAINTED IAW EMB-145 CPM 51-21-06. THE AIRC
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