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 C2XA99IA186Power Supply · inoperativeIAH - FLT 4215 - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE FORWARD EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED POWER SUPPLY IAW EMB145 MM 33-50-11, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)SDR CA990430056Pin · loose(CAN) DURING LANDING ROLLOUT, WHILE IN REVERSE, THE NR 1 ENGINE FLAMED OUT. ATTEMPTS TO RESTART THE ENGINE AT THE GATE RESULTED IN A HUNG START. BORESCOPE OF THE ENGINE REVEALED SEVERE HP TURBINE DAMAGE, BLADES REDUCED TO STUBS. ENGINE STRIP CONFIRMED HP1SDR C2XA99IA178Bulb · failedIAH - DURING AIRCRAFT MODIFICATION, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA99CL023Engine · failedPIT - FLT 4131 - CREW REPORTED THAT THE LEFT ENGINE FLAMED OUT ON LANDING ROLL WITH REVERSER ON, THE ENGINE WOULD NOT RESTART ON EITHER FADEC USING THE APU OR CROSS BLEED. MAINTENANCE INSPECTED THE AIRCRAFT SYSTEMS AND FOUND THAT THE LEFT ENGINE HAD EXCEEDED MSDR C2XA99CL027Air Dist · odorCLE - FLT 4059 - CREW REPORTED THAT AFTER SETTING TAKEOFF POWER THEY RECEIVED A SMOKE SMELL IN THE COCKPIT. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE AIRCRAFT AND RELEASED IT IAW MEL 21-51-00 CONTROL NR 173359. ON 3/24/99 MAINTENANCE PERFORMESDR C2XA99IA177Angle · crackedIAH - DURING C-CHECK INSPECTIONI, THE RIGHT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND TO BE CRACKED AT THE FORWARD END. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW EMB145 SST 0391/99, AND THE AIRCRAFT WAS APPROVED FOR RESDR C2XA99IA176Angle · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND TO BE CRACKED AT THE FORWARD END. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW EMB 145 SST 0391/99, AND THE AIRCRAFT WAS APPROVED FOR RETSDR C2XA99IA155Bulb · failedIAH - FLT 4206 - CREW INFORMED MAINTENANCE THE LEFT OVERWING FORWARD EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB AS REQUIRED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)SDR SIMA990512Air Dist · odorSHV - FLT 4109 - WITH TEMPERATURE CONTROL IN AUTO, THE FLIGHT ATTENDANT REPORTED A SMELL AND SMOKE IN THE CABIN. AFTER SWITCHING TEMPERATURE CONTROL TO MANUAL, THE SMELL CLEARED. INSPECTED NR 2 AIR CONDITIONING PACK AREA AT WING ROOT AND AUTO. NO DEFECTS WERESDR C2XA99CL019Lt Pack · odorCLE - FLT 4011 - CREW REPORTED THE LEFT PACK FILLED THE COCKPIT WITH SMOKE, AFTER THE PACK WAS TURNED OFF THE SMOKE CLEARED. AIRCRAFT WAS RELEASED IAW MEL 21-51-00 NR 173666. THE NEXT DAY MAINTENANCE INSPECTED THE NR 1 PACK ASSOCIATED COMPONENTS AND PERFORMED SDR C2XA99CL016Valve · failedCLE - FLT 4099 - CREW REPORTED THAT DURING CRUISE, THE HORIZONTAL STABILIZER ANTI-ICE SYSTEM FAILED. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER ANTI-ICE VALVE IAW EMB-145 MM 30-12-01, OSDR C2XA99BT005Connector · dirtyFLT 4084 - CREW REPORTED 'UNABLE TO RAISE GEAR'. MAINTENANCE CLEANED LGEU CANNON PLUGS. PERFORMED SEVERAL GEAR RETRACTIONS AND EXTENSIONS OPERATIONAL, TESTED SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 1,862.1 HOURS. ACFT CYCLES: 1,787. (X)SDR C2XA99CL013Heater · inoperableCLW - FLT 4091 - CREW REPORTED THAT DURING TAXI, THE NR 1 TAT HEAT WAS INOPERATIVE. AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED THE NR 1 TAT PROBE IAW EMB-145 MM 34-15-03. OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE.SDR C2XA99IA077Bulb · failedIAH - DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE LEFT HAND OVERWING EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BULB AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)SDR RAIA990135Probe · failedFLT 5783 - SBN - NR 2 TAT HEAT FAILED. MAINTENANCE REPLACED NR 2 TAT PROBE. (M)SDR SIMA990251Switch · leakingCLE - FLT 4387 - NR 1 HYDRAULIC SYSTEM FAILED. LANDING GEAR HAD TO BE MANUALLY EXTENDED. REMOVED AND REPLACED LEAKING HYDRAULIC PRESSURE SWITCH. SERVICED SYSTEM AND PERFORMED OPERATIONAL CHECK WITH NO FURTHER DEFECTS NOTED. (X)SDR RAIA990128Valve · failedORD - FLT 5776 - WING ANTI-ICE FAILED. MAINTENANCE REPLACED LEFT WING ANTI-ICE VALVE. (X)SDR C2XA99CL008Duct · chaffedCLE - FLT 4119 - CREW REPORTED THAT DURING CRUISE THEY RECEIVED A LEFT ENGINE BLEED LEAK LIGHT, THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT BLEED DUCT LOCATED IN FUSELAGE ABOVE THE LEFT WING IAW EMB-1SDR RAIA990117Gcu · failedFLT 5776 - ORD - NR 1 GENERATOR FELL OFF LINE. MAINTENANCE REPLACED NR 1 GENERATOR CONTROL UNIT. (M)SDR C2XA99CL006Blade · damagedCLE - DURING A SCHEDULED BORESCOPE INSPECTION THE LEFT ENGINE TURBINE BLADES WERE FOUND TO HAVE DAMAGE BEYOND MANUFACTURES LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE IAW CONTINENTAL EXPRESS TASK CARD NR 6271001, OPERATIONAL AND LEAK CHECKS WERE SDR C2XA99CL005Connector · malfunctionedCLE - FLT 4019 - CREW REPORTED THAT DURING CRUISE THE LEFT ENGINE OIL TEMPERATURE PEGGED OUT (135 DEGREES CELSIUS) AND WOULD NOT DECREASE WITH A THRUST DECREASE, A PRECAUTIONARY ENGINE SHUT DOWN WAS PERFORMED. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDESDR C2XA99IA019Control Module · inoperativeIAH - DURING CONFORMITY CHECK WHILE PERFORMING EMERGENCY LIGHT FUNCTIONAL CHECK, FOUND THE EICAS INDICATED 'EMERGENCY LIGHTS NOT ARMED' WITH THE LIGHTS PLACED IN THE ARMED POSITION. MAINTENANCE REMOVED AND REPLACED THE CABIN LIGHT CONTROL MODULE IAW EMB-145 MSDR RAIA990106Apu · contaminatedORD - FLT 5788 - SMOKE IN COCKPIT AND CABIN. SMOKE WENT AWAY WITH APU OFF. MAINTENANCE RAN APU AND PERFORMED OPS CHECK OF ECS SYSTEM, DETERMINED TO BE GLYCOL IN APU INLET. (X)SDR C2XA99IA001Apu · failedIAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED SMOKE COMING FROM THE LEFT PACK. MAINTENANCE REMOVED AND REPLACED THE AUXILLARY POWER UNIT AND THE AIRCRFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98BT086Skin · crackedSMALL CRACK IN SECTION OF FUSELAGE BEHIND PASSENGER DOOR. REPAIRED DAMAGED SECTION OF FUSELAGE IAW SRM. PRESSURE CHECKED GOOD. (M)SDR RAIA981221Adc · failedJFK/RED - FLT 6705 - RED WARNING. NO TAKEOFF DATA ILLUMINATED. MAINTENANCE REPLACED NR 1 AIR DATA COMPUTER. (X)SDR C2XA98CL082Bleed Valve · failedCLE - FLT 4052 - THE CREW REPORTED THAT THEY RECEIVED A LEFT BLEED LEAK WARNING AFTER TAKEOFF. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE LEFT BLEED SHUTOFF VALVE IAW EMB-145 SDR C2XA98IA495Light · inoperativeIAH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE RIGHT EXTERNAL EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE CLEANED THE AFFECTED LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA494Power Supply · inoperativeIAH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THE EMERGENCY EXIT LIGHT ON THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED POWER SUPPLY IAW EMB145 MM 33-50-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERSDR C2XA98IA493Wire · brokenIAH - DURNIG POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT AT EXIT ROW 2 RIGHT SIDE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON THE AFFECTED LIGHT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA485Support · corrodedIAH - DURING C-CHECK INSPECTION, THE RAMP SUPPORT WAS FOUND TO BE CORRODED AT FRAME 20 RIGHT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT AND THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA484Fitting · corrodedIAH - DURING C-CHECK INSPECTION, THE AFT GALLEY INBOARD AFT FITTING WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FITTING, AND THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA483Fitting · corrodedIAH - DURING C-CHECK INSPECTION, THE AFT GALLEY INBOARD FORWARD FITTING WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FITTING, AND THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA482Angle · crackedIAH - DURING C-CHECK INSPECTION, THE VERTICLE STABILIZER RIGHT DRAG ANGLE WAS FOUND TO BE CRACKED AT THE FORWARD END. MAINTENANCE REMOVED AND REPLACED THE FORWARD SECTION OF DRAG ANGLE IAW EMB145 SRM 54-40-02, AND THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SDR C2XA98IA481Angle · crackedIAH - DURING C-CHECK INSPECTION, THE VERTICLE STABILIZER LEFT DRAG ANGLE WAS FOUND TO BE CRACKED AT THE FORWARD END. MAINTENANCE REMOVED AND REPLACED THE FORWARD SECTION OF DRAG ANGLE IAW EMB145 SRM 54-40-02, AND THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SSDR C2XA98IA480Beam · corrodedIAH - DURING C-CHECK INSPECTION, THE CENTER AISLE OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE CORRODED SECTION OF OMEGA BEAM AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5320SDR C2XA98IA479Beam · corrodedIAH - DURING C-CHECK INSPECTION, THE CENTER AISLE OMEGA BEAM WAS FOUND TO BE CORRODED JUST FORWARD OF FRAME 25. MAINTENANCE REMOVED THE CORRODED SECTION OF OMEGA BEAM AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS DRAWINGS COEX03TYY05/06 AND COEX03TYYSDR C2XA98IA478Beam · crackedIAH - DURING C-CHECK INSPECTION, THE FORWARD GUST LOCK MOUNT STRUCTURE CROSS BEAM WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED AN INTERIM REPAIR IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01098, AND THE AIRCRAFT WAS APPROVED SDR C2XA98IA477Battery Pack · dischargedIAH - DURING C-CHECK INSPECTION, THE EMERGENCY LIGHT BATTERY AT STATION 17540.8 WAS FOUND TO BE DISCHARGED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK IAW EMB145 AMM 33-50-04, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98BT084Control Unit · failedBRAKE FAIL MESSAGE, BRAKE INBOARD AND OUTBOARD INOPERATIVE. REMOVED AND REPLACED BRAKE CONTROL UNIT. OPS CHECKED GOOD. (M)SDR C2XA98IA476Valve · failedIAH - FLT 4240 - THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 HYDRAULIC SYSTEM PRIORITY VALVE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SSDR C2XA98IA491Power Supply · inoperativeIAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY LIGHT POWER SUPPLY IAW EMB145 MM 33-50-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA475Frame · chafedIAH - DURING C-CHECK INSPECTION, FRAME 68 WAS FOUND TO BE CUT BY THE LEFT OUTBOARD RUDDER CONTROL CABLE. MAINTENANCE REPAIRED THE FRAME IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5320-01028, AND THE AIRCRAFT WAS APPROVED FOR RETURN SDR C2XA98IA474Skin · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT THRUST REVERSER MODULE UPPER SKIN WAS FOUND TO BE CRACKED WITH SHEARED RIVETS ABOVE FORWARD OF PANEL 426SL. MAINTENANCE STOP DRILLED THE CRACK, INSTALLED A REPAIR DOUBLER, AND REPLACED THE SHEARED FASTENERS IAW EMB14SDR C2XA98IA473Beam · damagedIAH - DURING C-CHECK INSPECTION, FOUND CORROSION BETWEEN THE COMPOSITE FLOOR CROSS BEAMS AND OMEGA BEAMS AT FRAMES 20 AND 25. MAINTENANCE REPAIRED THE DAMAGED SECTIONS OF OMEGA BEAM IAW EMBRAER FAX SST-2125/98, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVSDR C2XA98IA472Strap · corrodedIAH - DURING C-CHECK INSPECTION, THE CENTER FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 13 TO FRAME 18. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA471Angle · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DRAG ANGLE IAW EMB145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA470Angle · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DRAG ANGLE IAW EMB145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR RAIA981104Electronic Unit · failedORD - FLT 5776 - LANDING GEAR WILL NOT RETRACT AND WING DEICE FAILED. MAINTENANCE REPLACED LANDING GEAR ELECTRONIC UNIT AND INSPECTED DEICE SYSTEM. FOUND TO WORK GOOD. (X)SDR C2XA98CL070Control Unit · failedHPN - FLIGHT 4053 - CREW REPORTED THAT DURING BEFORE TAKEOFF CHECKS THE TAKEOFF CONFIGURATION WARNING SOUNDED FOR 'TRIM'. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW E
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