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 C2XA00IA429Battery Pack · inoperativeIAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT CENTER FLOOR CABIN EMERGENCY LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CENTER FLOOR EMERGENCY LIGHT BATTERY PACK IAW EMB-145 AMM 33-50-04. THE AIRCRAFT WAS APPROVED FOR RETURN SDR RAIA0012001Probe · failed6315-BOS- LEFT TAT HEAT FAIL INDICATION ILLUMINATED. MAINTENANCE INSPECTED AND REPLACED LEFT TAT PROBE.SDR C2XA00IA426Gusset · corrodedDURING C CHECK INSPECTION THE CENTER FLOORBEAM GUSSET STRAP UNDER THE LAV MODULE, FRAME 57 TO 60, WAS FOUND TO BE CORRODED. MX REMOVED/REPLACED THE DAMAGED GUSSET IAW EMB145 SRM 51-40-02. A/C APPROVED FOR RETURN TO SERVICE.SDR C2XA00IA424Frame · chafedDURING C CHECK INSPECTION, FRAME 65 RIGHT SIDE FLANGE WAS FOUND TO BE CHAFED BY A CARGO LINER FASTENER. MX REPAIRED THE FRAME AND REPOSITIONED THE CARGO LINER FASTENER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5310-01146SDR C2XA00IA423Angle · crackedDURING C-CHECK INSPECTION, REAR SECTION II, STRINGER #16 RIGHT AT APU FIREWALL. THE SUPPORT ANGLE WAS FOUND TO BE CRACKED. MX REMOVED/REPLACED THE CRACKED ANGLE WITH A FABRICATED PART IAW EMB145 SRM 51-40-02 AND 51-30-01. A/C WAS APPROVED FOR RETURN FOR SERVICSDR C2XA00IA422Strap · corrodedDURING C-CHECK INSPECTION, RIGHT SIDE FLOORBEAM BUTT-STRAP BETWEEN FRAMES 59 TO 61 WAS FOUND TO BE CORRODED. MX REMOVED/REPLACED CORRODED SECTION OF FLOORBEAM IAW EMB145 SRM 51-40-02. A/C WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA00IA421Strap · corrodedDURING C-CHECK INSPECTION, THE CENTER FLOOR BEAM BUTT-STRAP BETWEEN FRAMES 60 TO 61 WAS FOUND TO BE CORRODED. MX REMOVED/REPLACED CORRODED SECTION OF THE FLOOR BEAM IAW EMB145 SRM 51-40-02. A/C WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA00BT095Control Unit · faultyEWR-CREW REPORTED AFTER TAKEOFF, GEAR WOULD NOT RETRACT. NOSE GEAR DISAGREED WITH MAIN GEAR INDICATION AIRCRAFT LANDED WITHOUT INCIDENT. MX TROUBLESHOT A/C AND FOUND FAULTY LANDING GEAR ELECTRONIC UNIT REMOVED AND REPLACED LGEU GEAR SWUNG AND OPS. CHECKED SYSTSDR C2XA00IA420Seat Track · wornDURING C-CHECK INSPECTION THE CAPTAINS AND FIRST OFFICERS SEAT TRACKS WERE FOUND TO BE WORN. MX REMOVED/REPLACED SEAT TRACKS IAW EMB145 AMM 53-01-05. A/C WAS APPROVED FOR RETURN TO SERVICE.SDR C2XAOOBT091Smoke Detector · faultyEWR-CREW REPORTED LAV SMOKE WARNING ON CLIMBOUT. NO SMOKE NOTED. MX REMOVED/REPLACED SMOKE DETECTOR IAW EMB145 MM 26-18-01 OPS CHECKED SATISFACTORY IAW EMB 145 MM 26-14-00. REFERENCE M-602 #313920 FOR WORK ACCOMPLISHED.SDR C2XA00IA415Computer · false indicationTHE FLIGHT CREW REPORTED A FALSE LAV SMOKE WARNING DURING CLIMB. MX RELEASED A/C IAW MEL 26-14-00, PLACARD #005807. EFD MX REMOVED/REPLACED #2 DAU (DATA ACQUISITION UNIT) IAW EMB145 AMM 31-41-01. A/C WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA00IA419Smoke Detector · false activationCREW REPORTED A LAV SMOKE WARNING DURING CLIMB. MX RELEASED A/C IAW MEL 26-14-00, PLACARD 005797. BNA MX REMOVED/REPLACED LAV SMOKE DETECTOR IAW 26-14-01 AND A/C WAS APPROVED FOR RETURN TO SERVICE.SDR C2XAOOBT092Bulb · inoperativeBTV-DURING 1A INSPECTION MAINTENANCE FOUND EMERGENCY LIGHTS, RT OVERHEAD LIGHT BY ESCAPE HATCH INOPERATIVE. RELAMPED RT, OVERHEAD EMERGENCY LIGHT BY ESCAPE HATCH. OPS. CHECKED GOOD. IAW EMB145 MM 33-50-00.SDR RAIA0011006Tube · failed6317-BOS- STABILIZER ANTI ICE FAIL EICAS MESSAGE ILLUMINATED DURING TAXI. MAINTENANCE INSPECTED AND REPLACED ANTI ICE TUBE ASSEMBLY.SDR C2XA00IA414Uplock · inoperativeIAH - FLT 3925 - AFTER TAKEOFF FROM SAV, ON GEAR RETRACTINO, THE CREW REPORTED A LEFT GEAR UNSAFE LIGHT AND A LANDING GEAR LEVER DISAGREE MESSAGE, THE CREW CYCLED THE GEAR AND ALL WARNINGS WENT AWAY. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDSDR C2XA00IA413Detector · inoperativeIAH - FLT 4095 - THE CREW REPORTED A LAVATORY SMOKE WARNING ON CLIMB-OUT THROUGH 6000 FEET WITH NO SMOKE NOTED. THE AIRCRAFT LANDED AT MEM WITHOUT INCIDENT WHERE THE LAVATORY SMOKE DETECTOR WAS PLACED ON MEL 26-14-00 CONTROL NR 005501, AND THE AIRCRAFT WAS APSDR RAIA0011003Strut · failed7615-STL- NOSE WHEEL ON RIGHT SIDE SEPARATED FROM AXLE, SEPARATION OCCURRED AT THE GATE BEFORE TAXI. MAINTENANCE INSPECTED AND REPLACED NOSE GEAR LOWER SLIDING TUBE ASSEMBLY.SDR C2XAOOIA400Battery Pack · dischargedIAH-DURING A CHECK INSPECTION, THE AISLE PATH EMERGENCY LIGHT STRIP FROM SEAT 7 TO SEAT 12 WAS FOUND TO BE INOPERATIVE. MX REMOVED/REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK AND THE A/C WAS APPROVED FOR RETURN TO SERVICE.SDR C2XAOOIA401Floorbeam · corrodedIAH-DURING C-CHECK INSPECTION, THE CENTER FLOOR BEAM WAS FOUND TO BE CORRODED FROM FRAME 60-61. MX REMOVED/REPLACED AFFECTED FLOOR BEAM IN ACCORDANCE WITH EMB145 SRM 51-40-02 AND A/C WAS APPROVED FOR RETURN TO SERVICE.SDR C2XAOOIA402Floorbeam · corrodedIAH-DURING C-CHECK INSPECTION, RH FLOOR BEAM WAS FOUND TO BE CORRODED FROM FRAME 59-61. MX REMOVED/REPLACED THE AFFECTED FLOOR BEAM IN ACCORDANCE WITH EMB145 SRM 51-40-02, AND THE A/C WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA3091Bulb · inoperativeORD - FLT 4275 - ONE OF THE CEILING EMERGENCY LTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULB. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR C2XAOOBT086Hose · cutPVD REPORTED LOSS OF SYSTEM ONE HYDRAULIC QUANTITY IN CRUISE FLIGHT, DECLARED EMERGENCY AND DIVERTED INTO EWR.. A/C LANDED UNEVENTFULLY. MX FOUND A CUT HYDRAULIC HOSE ON LEFT ENGINE DRIVEN PUMP..REMOVED/REPLACED HYDRAULIC HOSE ON LT. EDP IAW EM145 MM29-20-04. SDR C2XAOOIA395Contactor · burnedIAH-CREW REPORTED SMOKE IN COCKPIT AFTER ATTEMPTING TO START THE APU, A/C LANDED AT IAH WITHOUT INCIDENT. MX INSPECTED THE A/C AND FOUND THE APU START CONTACTOR TO HAVE A MELTED LUG AND HEAT DAMAGE TO THE BUSS BAR AND LINE CONTACTOR. MX REMOVED/REPLACED THE AFSDR RAIA0010046Sensor · failed6257-BOS- STALL PROTECTION SYSTEM 2 INOP WARNING ILLUMINATED ON TAKEOFF ROLL. MAINTENANCE INSPECTED AND REPLACED RIGHT AOA STALL VANE.SDR C2XAOOIA399Smoke Detector · inoperativeIAH-CREW REPORTED A FALSE BAGGAGE SMOKE WARNING DUEING TAKEOFF ROLL. TAKEOFF WAS ABORTED WITHOUT INCIDENT, AND A/C RETURNED TO THE GATE WHERE MX REMOVED AND REPLACED THE AFFECTED SMOKE DETECTOR AND THE A/C WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA00IA469Blade · failedAMA - FLT 4210 - THE CREW REPORTED THAT THE NR 2 ENGINE SHUTDOWN FOLLOWING A LOUD BANG. THE AIRCRAFT LANDED AT AMA WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE DEFECTIVE ENGINE SDR C2XAOOIA387Engine · failedAMA-CREW REPORTED THAT NR 2 ENGINE SHUTDOWN FOLLOWING A LOUD BANG. A/C LANDED AT AMA WITHOUT INCIDENT. MX REMOVED AND REPLACED NR 2 ENGINE AND A/C WAS APPROVED FOR RETURN TO SERVICE.SDR C2XAOOIA391Bearing · corrodedIAH-DURING C-CHECK INSPECTION, THE RIGHT HAND VERTICAL STABILIZER SPHERICAL BEARING WAS FOUND TO BE CORRODED. MX REMOVED AND REPLACED THE AFFECTED BEARING IN ACCORDANCE WITH EMB145 MM55-37-00-400-801-A, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XAOOIA390Bushing · corrodedIAH-DURING C-CHECK INSPECTION, THE LEFT HAND HORIZONTAL STABILIZER TO VERTICAL STABILIZER OUTBOARD BUSHING WAS FOUND TO BE CORRODED. MX REMOVED/REPLACED AFFECTED BUSHING, AND A/C WAS APPROVED FOR RETURN TO SERVICE.SDR C2XAOOIA389Pin · corrodedIAH-DURING C-CHECK INSPECTION, THE LEFT HAND HORIZONTAL STABILIZER HINGE PIN WAS FOUND TO BE CORRODED. MX REMOVED AND REPLACED THE AFFECTED PIN IN ACCORDANCE WITH EMB145 MM 55-10-00-400-801-A AND A/C WAS APPROVED FOR RETURN TO SERVICE.SDR C2XAOOIA388Bearing · corrodedIAH-DURING C-CHECK INSPECTION, THE LEFT HAND VERTICAL STABILIZER SHERICAL BEARING WAS FOUND TO BE CORRODED. MX REMOVED/REPLACED THE AFFECTED BEARING IN ACCORDANCE WITH EMB145 MM 55-37-00-400-801-A AND THE A/C WAS APPROVED FOR RETURN TO SERVICE.SDR C2XAOOIA392Bushing · corrodedDURING C-CHECK INSPECTION, RT HORIZONTAL STABILIZER TO VERTICAL STABILIZER OUTBOARD BUSHING WAS FOUND TO BE CORRODED. MX REMOVED/REPLACED THE AFFECTED BUSHING AND A/C WAS APPROVED FOR RETURN TO SERVICE.SDR C2XAOOIA394Skin · crackedREFERENCE OPEN SDR C2XAOOIA383 DURING C-CHECK INSPECTION, THE LEFT HAND SKIN ON THE VERTICAL STABLILIZER WAS FOUND TO BE CRACKED. MX PERFORMED AN INSERTION REPAIR IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING CHANMGE EC5530-01045, AND A/C WAS APPROVED FORSDR C2XAOOIA393Frame · damagedREFERENCE OPEN SDR C2XAOOIA384 IAH-DURING C-CHECK INSPECTION, FRAME 64 RIGHT WAS FOUND TO HAVE A HOLE WORN IN IT. MX PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING CHANGE EC5310-01144, AND THE A/C WAS APPROVED FOR RETURN TO SERVISDR C2XA00IA393Frame · damagedREFERENCE OPEN SDR C2XA00IA384 DURING C-CHECK INSPECTION, FRAME 64 RIGHT WAS FOUND TO HAVE A HOLE WORN IN IT. MX PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING CHANGE EC5310-001144, AND THE A/C WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA00IA384Frame · damagedDURING C-CHECK INSPECTION, FRAME 64 RIGHT WAS FOUND TO HAVE A HOLE WORN IN IT.SDR C2XA00IA394Skin · crackedREFERENCE OPER SDR C2XA00IA383-DURING C-CHECK INSPECTION, THE LEFT HAND SKIN ON THE VERTICAL STABILIZER WAS FOUND TO BE CRACKED. MX PERFORMED INSERTION REPAIR IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING EC5530-01045, AND A/C WAS APPROVED FOR RETURN TO SSDR C2XA00IA383Skin · crackedDURING C-CHECK INSPECTION THE LEFT HAND SKIN ON THE VERTICLE STABILIZER WAS FOUND TO BE CRACKED. THIS SDR FILED OPEN AWAITING FINAL CORRECTIVE ACTION.(CLOSED BY C2XA00IA394)SDR 20001120SH009Armature · failedARMATURE MICA FAILED PREMATURELY. MICA MISSING BETWEEN BARS FOUR TIMES IN DIFFERENT SEGMENTS AND RISER BARS SEPARATING WHERE WELDED TOGETHER. POOR DESIGN OF ARMATURE/MICA AND INSULATION BREAKING DOWN PREMATURELY. (X)SDR C2XA00CL082Smoke Detector · intermittentCLE FLIGHT 3686-THE CREW REPORTED A INTERMITTENT BAGGAGE SMOKE WARNING IN FLIGHT. THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT.MAINTENANCE REMOVED AND REPLACED BAG SMOKE DETECTOR I/A/W EMB 145 MAINTENANCE MANUAL 26-15-01. PERFORMED DETECTOR OPERATSDR 20001101SH013Bearing · failed(APU) STARTER/GENERATOR DRIVE END BEARING FAILED PREMATURELY CAUSING EXCESS DAMAGE TO UNIT: ARMATURE RUBBED STATOR LAMINATIONS, SPUR GEAR RUBBED PICK UP. ALL (BER) BRUSHES WORN 75 PERCENT. NOTE: BEARING FAILURE CAUSED EXCESS DAMAGE TO UNIT.SDR 20001101SH012Bearing · failed(APU) STARTER/GENERATOR ANTI-DRIVE END BEARING FAILED PREMATURELY CAUSING EXCESS DAMAGE TO UNIT. ARMATURE RUBBED STATOR LAMINATIONS. PICK UP SHORTED. (ALL (BER). NOTE: BEARING FAILURE CAUSED EXCESS DAMAGE TO UNIT. (X)SDR C2XA00BT078Smoke Detector · faultyBTV - FLT 4218 - CREW REPORTED, LAV SMOKE INDICATION ON CLIMB-OUT. MAINTENANCE MEL AIRCRAFT AND RELEASED IAW MEL 26-14-00 CATEGORY C CONTROL NR 002376. ON 10-13-00 MAINTENANCE REMOVED AND REPLACED THE LAV SMOKE DETECTOR IAW EMB145 MM 26-14-01. OPS CHECKED GSDR C2XA00IA373Strap · corrodedIAH-DURING C-CHECK INSPECTION, THE CENTER FLOORBEAM BUTTSTRAP WAS FOUND TO BE CHAFED FROM FRAME 18 TO FRAME 23. MAINTENANCE REMOVED AND REPLACED THE AFFECTED GUSSET IN ACCORDANCE WITH EMB145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA00IA372Strap · corrodedIAH-DURING C-CHECK INSPECTION, THE CENTER BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 15 TO FRAME 18. MAINTENANCE REMOVED THE CORRISION, AND PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING CHANGE EC5310-01141, AND THE AIRCRAFT WSDR C2XA00IA371Engine · odorIAH-FLIGHT 3876 FROM OKC TO IAH, THE CREW REPORTED AN EXTREMELY STRONG EXHAUST SMELL WHEN ANTI-ICE WAS ON IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, AND THE AIRCRAFT WAS APPROVED FOR RETSDR C2XA00BT072Sensor · faultyTYS CO3991 CREW REPORTED LAV SMOKE ECIAS INDICATION ON CLIMBOUT, NO SMOKE NOTED MAINTENANCE REMOVED AND REPLACED LAV SMOKE DETECTOR SENSOR IAW EMB 145 AMM 26-14-01. OPS. CHECK GOOD IAW EMB 26-14-00.SDR C2XA00IA367Nozzle · malfunctionedIAH-DURING FLIGHT 3884 THE CREW REPORTED EXTREMELY STRONG JET FUEL FLAMES WHEN THE ANTI-ICE SYSTEM WAS ACTIVATED. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE FUEL NOZZLES, AND THE AIRCRASDR C2XA00IA364Bushing · corrodedIAH-DURING C-CHECK INSPECTION, THE RIGHT HAND HORIZONTAL STABILIZER AFT ATTACHMENT INBOARD BUSHING WAS FOUND TO BE CORRODED AND PITTED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUSHING IN ACCORDANCE WITH EMB145 M/M 20-10-08, AND THE AIRCRAFT WAS APPROVED SDR C2XA00IA363Bushing · groovedIAH-DURING C-CHECK INSPECTION, THE RIGHT HAND HORIZONTAL STABILIZER AFT ATTACHMENT OUTBOARD BUSHING WAS FOUND TO BE PITTED AND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUSHING IN ACCORDANCE WITH EMB145 M/M 20-10-08, AND THE AIRCRAFT WAS APPROVED
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