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 RAIA00403006Power Supply · inoperativeEMERGENCY FLOOR PATH LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED NR 2 POWER SUPPLY.SDR C2XA04SH136Stiffener · gougedSHV- DURING C-CHECK THE T-REINFORCEMENT ON STRINGER 19 LEFT WAS FOUND TO BE GOUGED BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMBRAER IC 2004-145/0718. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04BT027Proximity Switch · faultyCREW REPORTED, EXPERIENCED SEVERAL UNUSUAL THUMPS WHILE INFLIGHT. NOISES SEEM TO BE COMING FROM THE NOSE OF THE AIRCRAFT. MAINTENANCE TROUBLESHOT AND FOUND RIGHT HAND LANDING GEAR UPLOCK CHANNEL-B FAULTY. REMOVED AND REPLACED LANDING GEAR PROXIMITY SWITCH-BSDR C2XA04CL016Inverter · intermittentCVG FLIGHT 2931 THE CREW REPORTED THE OVERWING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE WHEN TESTED. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL TEST AND NO DEFECTS WERE FOUND. WHEN AIRCRAFT GOT TO IAH THE CREW REPORTED THE OVERWING EMERGENCY EXIT LIGHTSDR C2XA04BT026Odor · detectedCREW REPORTED, STRONG ODOR OF FUEL/OIL IN COCKPIT AND CABIN AFTER EVERY APU START. MAINTENANCE INSPECTED, PERFORMED SEVERAL APU STARTS IAW EMB145 AMM 49-00-00. OPS AND LEAKED CHECKED GOOD. NO SMELL NOTED. AIRCRAFT RETURNED TO SERVICE.SDR C2XA04SH129Buttstrap · corrodedSHV- DURING C-CHECK THE LEFT BUTTSTRAP AT FRAME 65 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 RAIA00402028Socket · burnedFUMES IN MAIN CABIN WITH SMOKE COMING FROM SEAT 1A CEILING LIGHT AREA. MAINTENANCE FOUND WINDOW WASH LIGHT HOLDER AT 1A BURNED AND DEFERRED SYSTEM IAW MEL. SUBSEQUENTLY CLEARED DMI REMOVING AND REPLACING WINDOW WASH LIGHT HOLDER.SDR C2XA04CL015Filter · dirtyCLE FLIGHT 3231 THE CREW REPORTED A ENGINE NR 2 FUEL IMPENDING BYPASS WARNING. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE NR 2 ENGINE AND REPLACED THE FUEL FILTER AND IMPENDING BYPASS INDICATOR. OPERATISDR C2XA04IA018Connector · dirtyDURING PREFLIGHT INSPECTION THE EMERGENCY LIGHT ABOVE THE FLIGHT ATTENDANTS JUMPSEAT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED THE FORWARD INVERTER, CLEANED THE CONNECTOR, AND RE-INSTALLED THE SAME UNIT. THE EMERGENCY LIGHTING SYSTEM OPERATIONALLY CHESDR C2XA04SH112Floorbeam · corrodedDURING C CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A SHIM/FILLER REPAIR IAW EMB 145 SRM 53-21-10, FIG 201, SHEET 1. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH111Floorbeam · corrodedDURING C CHECK THE GALLEY CENTER FLOORBEAM FROM FRAME 16-24 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH110Angle · corrodedDURING C CHECK THE CENTER RAMP ANGLE FROM FRAME 18-20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RAMP ANGLE IAW SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH109Floorbeam · corrodedDURING C CHECK THE CENTER FLOORBEAM FROM FRAME 18 TO FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR RAIA00402029Solenoid · defectiveGUST LOCK WILL NOT DISENGAGE. MAINTENANCE DEFERRED SYSTEM IAW MEL. SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING THE RUDDER GUST LOCK SOLENOID.SDR C2XA04SH101Intake · gougedSHV- DURING C-CHECK THE NR 2 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH100Intake · gougedSHV- DURING C-CHECK THE NR 1 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH099Stiffener · chafedSHV- DURING C-CHECK THE RIGHT HAND ENGINE UPPER COWLING AFT INTERNAL STIFFENER WAS FOUND TO BE CHAFED AND EXCEEDED BLEND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICESDR C2XA04SH098Sill · corrodedSHV- DURING C-CHECK THE RIGHT HAND FORWARD FLOOR SILL BETWEEN FRAMES 18 AND 20 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 C2XA04SH097Sill · corrodedSHV- DURING C-CHECK THE LEFT HAND FLOOR SILL BETWEEN FRAMES 18 AND 22 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 C2XA04SH096Door Frame · corrodedSHV- DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LOWER BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH095Sill · corrodedSHV- DURING C-CHECK THE SERVICE DOOR SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 21 AND 22. MAINTENANCE BLENDED OUT THE AFFECTED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH094Buttstrap · corrodedSHV- DURING C-CHECK THE CENTER FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE BLENDED OUT THE AFFECTED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH093Stringer · gougedSHV-DURING C-CHECK EXTERIOR STRINGER 19 RIGHT WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH092Channel · crackedSHV- DURING C-CHECK THE RIGHT WING UPPER NUT PLATE CHANNEL ON SPAR 1 WAS FOUND TO BE CRACKED AND BENT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CHANNEL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH091Sill · corrodedSHV- DURING C-CHECK THE LEFT FORWARD SILL IN THE CARGO COMPARTMENT WAS FOUND TO BE CORRODED AROUND THE NUT PLATES. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH090Buttstrap · corrodedSHV- DURING C-CHECK THE LAVATORY CENTER BUTTSTRAP 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 C2XA04SH089Structure · chafedSHV- DURING C-CHECK THE LEFT LOWER COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFT EDGE MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04BT022Wire Harness · faultyCREW REPORTED, SIDEWALL LAMP FLICKERING AND SMELL OF SMOKE IN SEAT 1A. MAINTENANCE REMOVED THE BULB AIRCRAFT RELEASED IAW MEL 33-20-00/1 CATEGORY-C ITEM CONTROL NUMBER 038985. AIRCRAFT ARRIVED EWR, MAINTENANCE REMOVED AND REPLACED HARNESS FOR LAMP INSERT SEASDR C2XA04IA013Engine · defectiveLCH-FLIGHT 970, THE CREW REPORTED SMOKE IN THE CABIN, THE CREW SHUT DOWN THE NR 2 ENGINE, AND DIVERTED TO LCH WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVISDR C2XA04IA012Light · malfunctionedDURING PREFLIGHT INSPECTION, THE EMERGENCY LIGHT ABOVE THE COCKPIT DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESET THE POWER TO THE SYSTEM AND COULD NOT DUPLICATE THE PROBLEM.SDR RAIA00402016Proximity Switch · malfunctionedRIC - DURING LANDING AT BOS RIGHT MAIN GEAR INDICATED NOT LOCKED, RECYCLED AND GOT THREE GREEN INDICATIONS. MAINTENANCE REMOVED AND REPLACED DOWNLOCK PROX SWITCH AND PERFORMED GEAR SWING, CHECK OK.SDR RAIA00402012Proximity Sensor · false indicationSTL- SPOILER OPEN INDICATION DURING TAXI. MAINTENANCE REMOVED AND REPLACED LEFT AFT SPOILER PROX SENSOR.SDR RAIA00402008Pressure Switch · inoperativeCLT - LEFT ENGINE ANTI-ICE VALVE FAILED TO OPEN ON TEST. MAINTENANCE DEFERRED NR 1 ENGINE ANTI-ICE PER MEL SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING NR 1 ENGINE ANTI-ICE PRESSURE SWITCH.SDR C2XA04SH047Sill · corrodedSHV-DURING C-CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED AROUND THE NUT PLATES. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH048Buttstrap · corrodedSHV - DURING C-CHECK THE CENTER FLOORBEAM BUTTSTRAP 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 C2XA04SH046Buttstrap · corrodedSHV - DURING C-CHECK THE RT FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 22. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH045Floorbeam · 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 C2XA04SH044Floorbeam · corrodedSHV- DURING C-CHECK THE RIGHT RAMP SUPPORT ANGLE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH043Buttstrap · corrodedSHV- DURING C-CHECK THE CENTER FLOORBEAM BUTTSTRAP 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 C2XA04SH042Buttstrap · corrodedSHV- DURING C-CHECK THE RIGHT OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE RIGHT FLOORBEAM BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH041Buttstrap · corrodedSHV- DURING C-CHECK THE LEFT HAND MIDDLE FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED IN THE CARGO AREA FROM FRAME 65 TO FRAME 68. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVISDR C2XA04SH040Sill · corrodedSHV- DURING C-CHECK THE CARGO DOOR 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 C2XA04SH039Buttstrap · corrodedSHV- DURING C-CHECK THE LEFT HAND FLOORBEAM BUTTSTRAP BETWEEN FRAMES 59-61 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 C2XA04SH038Firewall · crackedSHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE LEFT HAND AND RIGHT HAND SUPPORT ROD BRACKETS. MAINTENANCE PERORMED A DOUBLER REPAIR TO THE AFFECTED AREAS IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04TY029Sill · corrodedTYS, DURING A SCHEDULED INSPECTION THE CARGO DOOR CUT OUT LOWER SILL WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE CARGO DOOR SILL IAW EMB-135/145 SRM-51-20-03, 51-40-02 AND CMP-51-21-04/05/06.SDR C2XA04TY028Floorbeam · corrodedTYS, DURING A SCHEDULED INSPECTION THE CENTER TOP CAP IN THE GALLEY WAS FOUND CORRODED. MAINTENANCE CLEANED AND BLENDED THE CORRODED AREA, ALODINED, PRIMED AND PAINTED IAW EMB-IC2004-145/0302.SDR C2XA04TY027Sill · corrodedTYS, DURING A SCHEDULED INSPECTION THE PAX DOOR LOWER ENTRANCE SILL WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE PAX DOOR SILL IAW EMB-135/145 SRM-51-40-02.SDR C2XA04TY026Sill · corrodedTYS, DURING A SCHEDULED INSPECTION, THE FORWARD PARTITION ON LEFT SIDE UNDER THE CABIN FIBER BEAM WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SILL IAW EMB-135/145 SRM 51-40-02/03 AND CMP51-21-04.SDR C2XA04TY025Sill · gougedTYS, DURING A SCHEDULED INSPECTION THE LEFT OUTBOARD FLOOR SUPPORT BETWEEN FRAMES 61 AND 64 WAS FOUND DAMAGED. MAINTENANCE REMOVED THE FLOOR SUPPORT, FABRICATED NEW PARTS, ALODINED, PRIMED AND INSTALLED IAW EMB-135/145 SRM 51-40-02/03 AND CMP-51-21-04.SDR C2XA04TY024Sill · gougedTYS, DURING A SCHEDULED INSPECTION THE LEFT OUTBOARD FLOOR SUPPORT AT FRAME 68 WAS FOUND GOUGED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT IAW EMB-135/145-SRM-51-40-02 / CMP-51-21-04/06.
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