Embraer EMB-145LR
Service difficulty reports · 36,799
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 CHQA20121106406Light · inoperativeCREW REPORTED THAT THE RIGHT OVERWING EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE DEFERRED THE EMERGENCY LIGHT. THE DEFERRAL WAS CLEARED ON 11/7/2012 BY REPLACING THE RIGHT OVERWING EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOSDR SIMA20121106004Sensor · failedON FLIGHT 4271 THE CREW REPORTED AT FLIGHT LEVEL 370 THE NR 1 ENGINE OIL WENT FROM 10 QUARTS TO AMBER AT 1 QUART. THERE WAS NO EICAS MESSAGE NOTED. THE CREW CONTACTED MAINTENANCE AND DIVERTED TO CVG. THE CREW DECLARED AN EMERGENCY AS A PRECAUTIONARY MEASURESDR SIMA20121106003Flashlight · inoperativeON FLIGHT 2723 THE FLIGHT ATTENDANT REPORTED THE FORWARD FLASHLIGHT DID NOT WORK. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FLASHLIGHT IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVSDR SIMA20121106002Bracket · looseON FLIGHT 2977 THE CREW REPORTED THE COCKPIT FLASHLIGHT BRACKET WAS LOOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. SECURED COCKPIT FLASHLIGHT BRACKET IAW EMB-145 MM 25-60-00. OK FOR SERVICE. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20121106001Light · inoperativeDURING B INSPECTION FOUND THE EMERGENCY EXIT LIGHT ON THE MAIN DOOR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP AT MAIN DOOR EMERGENCY LIGHT PER EMB AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. THE OPERATIONAL CHECK WASDR SIMA20121105012Shear Tie · corrodedCARGO DOOR CUTOUT SHEAR TIE CORRODED AT FR 68. REPAIRED CARGO DOOR CUTOUT SHEAR CLIP AT FR 68 IAW EO EM-53MR-1129, PART B.SDR SIMA20121105011Channel · corrodedGALLEY RT HAT CHANNEL CORRODED AT FRAME 23. REPAIRED GALLEY RT HAT CHANNEL AT FR 23 IAW EO-EM-53MR-2036, PART A.SDR SIMA20121105010Shear Tie · corrodedCARGO DOOR CUTOUT SHEAR TIE CORRODED AT FR 65. REPAIRED CARGO DOOR CUTOUT SHEAR TIE AT FR 65 IAW EO EM-53MR-1129, PART A.SDR SIMA20121105009Sill · corrodedDURING MAINTENANCE INSPECTION FOUND THE SERVICE DOOR AFT SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR AFT SILL IAW EMB SRM 51-40-02 AND 51-20-03. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20121105008Angle · crackedDURING MAINTENANCE INSPECTION FOUND THE CARGO DOOR SILL L ANGLES AT FRAME 66 AND 67 CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CARGO DOOR SILL L ANGLES AT FRAME 66 AND 67 IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVISDR SIMA20121105007Sill · corrodedDURING MAINTENANCE INSPECTION FOUND THE CARGO DOOR CENTER SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CARGO DOOR CENTER SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR RAIA201211050002Pressure Switch · malfunctionedDURING DESCENT THE FLIGHT CREW GOT AN A/P FAIL/RUDDER SYS 1-2 INOP AND YAW DAMP FAIL EICAS MESSAGE. FLIGHT CREW MADE AN EMERGENCY LANDING. MAINTENANCE INSPECTED AND REMOVED AND REPLACED RUDDER SYSTEM 2 PRESSURE SWITCH. SYSTEMS OPS CHECKED GOOD.SDR RAIA201211050001Smoke Detector · faultyDURING CRUISE FLIGHT THE FLIGHT CREW GOT A BAGGAGE COMPARTMENT SMOKE INDICATION. THE FLIGHT CREW DISCHARGED THE BAGGAGE COMPARTMENT FIRE EXTINGUISHER AND MADE AN EMERGENCY LANDING. MAINTENANCE INSPECTED THE BAGGAGE COMPARTMENT AND FOUND NO INDICATION OF SMOKSDR SIMA20121105005Light · inoperativeDURING B INSPECTION FOUND THE 2ND FROM FRONT CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP AT LOCATION INDICATED PER EMB AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. THE OPERATIONAL CHECK WAS GOODSDR SIMA20121105004Connector · looseDURING B INSPECTION FOUND THE FORWARD BULKHEAD EMERGENCY "EXIT" SIGN WILL NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND LOOSE CONNECTOR ON LIGHT SECURED AS REQUIRED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20121105003Roller · dirtyON FLIGHT 2795 THE CREW REPORTED THE MAIN CABIN PASSENGER DOOR WAS VERY DIFFICULT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEAN AND LUBE FRAME ROLLS OPEN AND CLOSE. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 52-18-00. THE AIRCRAFT WAS RETURNED SDR CHQA20121103405Sign · inoperativeDURING INSPECTION, THE EMERGENCY EXIT SIGN ABOVE SEAT 12F WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY EXIT SIGN AT ROW 12, OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR SIMA20121103003Light · inoperativeDURING B INSPECTION FOUND THE RIGHT EMERGENCY LIGHT AT WING/FUSELAGE FAIRING FRONT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT EMERGENCY LAMP AT WING/FUSELAGE FAIRING FRONT IAW EMB 145 AMM 33-50-10. THE OPERATIONAL CHECSDR SIMA20121102011Beam · corrodedRT BEAM IN GALLEY AREA HAS CORROSION AT FR 23. REPAIRED BEAM IAW EO EM-53MR-2035.SDR SIMA20121102010Door Frame · damagedCARGO DOOR CUTOUT FRAME 65 LATERAL "L" SHAPE CORRODED JUST ABOVE THE CENTER SILL. REPAIRED CARGO DOOR CUTOUT FRAME 65 "L" SHAPE (SHEAR CLIP) ABOVE CENTER SILL WITH ACCOMPLISHMENT OF AEA EO EM-53MR-1129 PART ASDR SIMA20121102009Gusset · corrodedDURING B INSPECTION FOUND THE GALLEY AFT DIAMOND GUSSET HAS CORROSION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE GALLEY AFT DIAMOND GUSSET IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20121102008Sill · corrodedDURING B INSPECTION FOUND THE LAV RIGHT FLOOR SILL CORRODED JUST FORWARD OF THE CARBON BEAM. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAV RIGHT FLOOR SILL JUST FORWARD OF THE CARBON BEAM IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNEDSDR SIMA20121102007Sill · corrodedDURING B INSPECTION FOUND THE LEFT NR 1 FLOOR SILL CORRODED BETWEEN FRAMES 19-20. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT NR 1 FLOOR SILL IAW EMB SRM 51-40-02 AND 51-20-03. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20121102006Sill · corrodedDURING B INSPECTION FOUND THE CARGO DOOR CENTER SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CARGO DOOR CENTER SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR ASOA20121102100Lamp · inoperativeDURING 5A CHECK INSPECTION, ROW 12 CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX R & R ROW 12 CEILING EMERGENCY LIGHT BULB WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20121102099Coffeemaker · odorF/A REPORTED ELECTRIC BURNING ODOR WITH VISIBLE SMOKE IN GALLEY ON CLIMBOUT. F/A PULLED COFFEEMAKER BREAKERS AND ODOR AND SMOKE CLEARED. MX INSPECTED BOTH COFFEEMAKERS FOR BURN MARKS. NONE FOUND. CLEANED BOTH HOT PLATES OF COFFEE STAINS AND LIQUID. BREWEDSDR SIMA20121102003Light · inoperativeDURING B INSPECTION FOUND THE MAIN DOOR OVERHEAD EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR OVERHEAD EMERGENCY LIGHT BULB IN REFERENCE WITH 33-26-04-000-801-A AND 33-26-04-400-801-A. THE OPERATIONALSDR SIMA20121102001Unknown · odorON FLIGHT 4302 THE CREW REPORTED AN OVERPOWERING TUNA FISH ODOR. MAINTENANCE ACCEPTED THE AIRCRAFT TO FIND AN OVERPOWERING TUNA FISH ODOR IN THE FLIGHT DECK. SPRAYED AIR FRESHENER FOR FLIGHT CONTINUOUSLY BUT AIRCRAFT STILL SMELLED LIKE A DEAD FISH BAKING IN SDR SIMA20121101006Stringer · crackedFOUND 2 CRACKS APPROX 3/8 " LONG EA ON STRINGER 2L JUST AFT OF FR 75. REPAIRED STRINGER 2L AT FRAME 75 IAW SRM 53-00-03 FIG. 202 AND ETA-EM-5300-2534. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20121101004Battery · dischargedDURING B INSPECTION FOUND THE AFT EMERGENCY LIGHTS ABOVE WINGS BOTH SIDES INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 & 4 EMERGENCY BATTERY AND POWER SUPPLY IAW W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFSDR SIMA20121101001Pdu · failedON FLIGHT 4350 THE CREW REPORTED THAT ON APPORACH THE FLAPS FAILED IN THE ZERO POSITION. THE CREW COULD NOT OBTAIN ANY FLAPS ON LANDING. THE CREW DECLARED AN EMERGENCY AND RAN THE APPROPRIATE CHECKLIST. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WASDR SIMA20121031003Seal · peelingON FLIGHT 2807 THE CREW REPORTED THAT ON TAKEOFF ACCELERATING TO 180 KNOTS THE CREW NOTICED A COCKPIT NOISE RESEMBLING STATIC OR CRACKING EMINATING FROM THE OVERHEAD PANEL ON THE CAPTAIN’S SIDE. THE CREW DECLARED AN EMERGENCY AND RETURNED TO DFW. THE AIRCRAFSDR CHQA20121031420Seat Track · corrodedDURING INSPECTION, THE LEFT SIDE WALL SEAT TRACK FROM FRAME 30 THROUGH FRAME 33 WAS FOUND TO BE CORRODED. THE LEFT SIDE WALL SEAT TRACK FROM FRAME 30 THROUGH 33 WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.SDR CHQA20121031419Attach Bracket · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE AFT FLOOR ATTACH BRACKET AT THE PASSENGER DOOR THRESHOLD. THE AFT FLOOR ATTACH BRACKET AT THE PASSENGER DOOR THRESHOLD WAS REPLACED IN ACCORDANCE WITH 51-40-02.SDR CHQA20121031418Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT SIDE WALL SEAT TRACK FROM FRAME 41 THROUGH FRAME 47. THE LEFT SIDE WALL SEAT TRACK FROM FRAME 41 THROUGH FRAME 47 WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.SDR CHQA20121031417Gusset · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CENTER OMEGA BEAM DIGITAL FROM FRAME 20 THROUGH FRAME 23. THE CENTER OMEGA BEAM GUSSET WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20121031416Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT SIDE WALL SEAT TRACK FROM FRAME 47 THROUGH FRAME 51. THE LEFT SIDE WALL SEAT TRACK FROM FRAME 47 THROUGH FRAME 51 WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.SDR CHQA20121031415Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OMEGA BEAM SEAT TRACK FROM FRAME 25 THROUGH FRAME 28. THE LEFT OMEGA BEAM SEAT TRACK FROM FRAME 25 THROUGH FRAME 28 WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.SDR CHQA20121031414Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT SIDE WALL SEAT TRACK SUPPORT AT FRAME 42 THROUGH FRAME 50. THE LEFT SIDE WALL SEAT TRACK SUPPORT FROM FRAME 42 THROUGH FRAME 50 WAS REPAIRED IN ACCORDANCE WITH SRM 51-30-03, 51-20-03, AND 51-40-02.SDR CHQA20121031413Seat Track · corrodedDURING INSPECTION, THE LEFT CENTER OMEGA BEAM SEAT TRACK AT FRAME 31 WAS FOUND TO BE CORRODED. THE LEFT-HAND CENTER OMEGA BEAM SEAT TRACK AT FRAME 31 WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.SDR CHQA20121031412Seat Track · corrodedDURING INSPECTION, THE CENTER OMEGA BEAM SEAT TRACK WAS FOUND TO BE CORRODED FROM FRAME 41 THROUGH FRAME 47. THE CENTER OMEGA BEAM SEAT TRACK FROM FRAME 41 THROUGH FRAME 47 WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.SDR CHQA20121031411Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT SIDE WALL SEAT TRACK FROM FRAME 54 THROUGH FRAME 59. THE LEFT SIDE WALL SEAT TRACK FROM FRAME 54 THROUGH FRAME 59 WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.SDR CHQA20121031410Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT SIDE WALL SEAT TRACK FROM FRAME 47 THROUGH FRAME 52. THE RIGHT SIDE WALL SEAT TRACK FROM FRAME 47 THROUGH FRAME 52 WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.SDR CHQA20121131409Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT WALL SEAT TRACK FROM FRAME 53 THROUGH FRAME 57. THE RIGHT SIDE WALL SEAT TRACK FROM FRAME 53 THROUGH FRAME 57 WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.SDR SIMA20121029004Angle · corrodedDURING IMBV INSPECTION FOUND CARGO DOOR AFT ANGLE AT FRAME 68 CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLETED INSTALLATION OF FRAME 68 SHEAR CLIP IAW EO EM-53MR-1129. THE AIRCRAFT WAS RETUNRED TO SERVICE.SDR CHQA20121031397Control Module · faultyCREW REPORTED AN ELECTRICAL BURNING ODOR FROM THE FRONT OF THE CABIN DURING FLIGHT. MAINTENANCE REPLACED THE CABIN LIGHTING CONTROL MODULE. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR SIMA20121031002Light · inoperativeDURING B INSPECTION FOUND THE EMERGENCY LIGHT AT MID-CABIN LEFT SIDE EMERGENCY EXIT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP AT THE LEFT EMERGENCY EXIT PER EMB AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. THE OPERATSDR SIMA20121031001Light · inoperativeDURING B INSPECTION FOUND THE 3RD AFT EMERGENCY CEILING LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP AT CEILING LIGHT INDICATED PER EMB AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. THE OPERATIONAL CHECK WAS GOOD. SDR SIMA20121030004Stringer · crackedFOUND 2 CRACKS APPROX 3/8 " LONG EA ON STRINGER 2R JUST AFT OF FR 75. REPAIRED STRINGER 2R AT FRAME 75 IAW SRM 53-00-03 AND ETA-EM-5300-2534. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR CHQA20121030396Thermostat · faultyCREW REPORTED THAT UPON TAKEOFF, RECEIVED A BLEED 1 OVERHEAT MESSAGE. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FAN AIR CONTROL THERMOSTAT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
Back to Embraer EMB-145LR