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 RAIA00312315Proximity Sensor · dirtySTL- WINDSHIELD HEAT NR 2 FAIL, AIR GROUND FAIL, RUDDER NR 1 AND NR 2 FAIL. MAINTENANCE CLEANED CONNECTOR ON AIR GROUND PROXIMITY SENSOR.SDR RAIA00312313Motor · inoperativeSTL- CAPTAIN'S WINDSHIELD WIPER INOP. MAINTENANCE REMOVED AND REPLACED CAPTAIN'S WINDSHIELD WIPER MOTOR.SDR RAIAOO312311Proximity Switch · malfunctionedRIC- AIR GROUND FAIL MESSAGE. MAINTENANCE REMOVED AND REPLACED LEFT FORWARD AND RIGHT AFT PROX SWITCHES.SDR C2XA03BT116Connector · disconnectedCREW REPORTED, EMERGENCY LIGHT INOPERATIVE ON SIDE WALL OF CABIN. MAINTENANCE RESECURED CONNECTOR TO THE EMERGENCY LIGHT AND OPS CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE.SDR C2XA03TY207Inverter · looseON CREW PREFLIGHT, REPORTED THAT THE EMERGENCY SIDE WALL LIGHT WAS OUT. MAINTENANCE FOUND THE CANNON PLUG LOOSE TO AN INVERTER, RESECURED THE CANNON PLUG ON THE INVERTER ASSY LOCATED LEFT SIDE, JUST AFT OF ST14513.6, OPERATIONAL CHECKED GOOD. AIRCRAFT RELEASSDR C2XA03TY205Bearing · wornDURING A SCHEDULED INSPECTION BOTH HORIZONTAL STABILIZER SPHERICAL BEARING WERE FOUND TO BE WORN BEYOND SERVICE LIMITS. MAINTENANCE REMOVED AND REPLACED THE SPHERICAL BEARINGS IAW EMB MM 55-37-00 AND EC 5510-01070. AIRCRAFT RELEASED FOR SERVICE.SDR C2XA03CL197Fan · seizedCLE FLIGHT NR 2123) THE CREW REPORTED A VERY STRONG SMELL OF SMOKE FROM CABIN ON APPROACH. TURNED OFF NR 2 PACK AND SMELL DISSIPATED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED SYSTEM AND FOUND THE NR 2 RECIRCULATION FAN WAS SEIZED. MAISDR RAIA00312301Access Door · unsecureSTL- LOUD RATTLING NOISES COMING FROM LEFT FWD NOSE SECTION. MAINTENANCE SECURED GPU ACCESS DOOR.SDR C2XA03CL196Odor · detectedTHE CREW REPORTED ON APPROACH AFTER STARTING THE APU HAD A BURNING ODOR IN THE COCKPIT AND CABIN. ALSO REPORTED THE BURNING ODOR AT THE GATE WITH THE APU OFF. MAINTENANCE INSPECTED THE CABIN AND COCKPIT LIGHTING SYSTEM, THE RADIO EQUIPMENT FANS AND AVIONICSSDR C2XA03CL194Smoke · detectedCLE) FLIGHT NR 3230, THE CREW REPORTED THE COCKPIT AND CABIN FILLED WITH SMOKE ON DESCENT INTO CLEVELAND.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE NR 1 AND NR 2 BLEED AIR SYSTEM,THE NR 1 AND NR 2 ENGINES AND APU. NO DEFECTS WERESDR RAIA00311295Pressure Switch · leakingBGM- HYDRAULIC SYSTEM 1 FAILURE. MAINTENANCE REMOVED AND REPLACED BRAKE PRESSURE SWITCH.SDR C2XA03TY197Fitting · damagedTYS AFTER REAMING THE RT VERTICAL STAB SPHERICAL BEARING CASTING, THE HORIZ STAB FAIL THE DIHEDRAL CHECK. REMOVED AND REPLACED THE RT VERTICAL HINGE FITTING IAW EC 5510-01067 C/W BACKLASH CHECK IAW EMB 145 AMM27-40-00; C/W INCIDENCE AND DIHEDRAL CHECKS IAW EMSDR C2XA03TY196Gusset · corrodedDURING A SCHEDULED 3C INSPECTION THE GUSSET ON THE RT FLOORBEAM FOR PANEL 247AF WAS CORRODED. MAINT REMOVED OLD GUSSET AND FAB A NEW GUSSETT. ALODINED, PRIMED AND INSTALL NEW FAB GUSSET IAW EMB 135/145 SRM 51-40-04 AND 51-40-06, CPM 51-21-04-05-06 AND SRM 51SDR RAIA00311285Actuator · out of adjust5321-PIT- THRUST REVERSER DISAGREE RT SIDE. MAINTENANCE DEFERRED NR 2 THRUST REVERSER PER MEL 78-30-00. SUBSEQUENTLY CLEARED DMI BY ADJUSTING UPPER AND LOWER DOOR ACTUATOR READING.SDR C2XA03BT106Charger · faultyEWR---DURING PREFLIGHT INSPECTION, FOUND RIGHT FRONT EXTERIOR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 2 BATTERY CHARGER ASSY IAW EMB145 MM 33-50-04 AND EXTERNAL EMERGENCY LIGHT ASSY (PART NUMBER 1317) IAW EMB145 MM 33-50-10. OPSDR RAIA00311281Warning System · activated5291-BGM- SERVICE DOOR OPEN INDICATION. MAINTENANCE DEFERRED PER MEL 52-70-00. SUBSEQUENTLY, CLEARED DMI, OPS CHECK SERVICE DOOR WARNING SYSTEM, OPS CHECK OKAY.SDR C2XA03TY189Sill · corrodedTYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CARGO DOOR SILL. MAINTENANCE REMOVED AND REPLACED THE CARGO DOOR SILL IAW EMB SRM 51-20-03 AND 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.SDR C2XA03TY188Doubler · corrodedTYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE RIGHT HAND GALLEY FLOORBEAM DOUBLER AT FRAME 20 AND 22. MAINTENANCE REMOVED AND REPLACED THE DOUBLER IAW EMB SRM 51-30-01, 51-40-02 AND CPM 51-21-04, 05, 06. THE AIRCRAFT WILL BE RELEASED UPON COMSDR RAIA00310273Pitot Tube · inoperative5304-RDU- PITOT NR 2 INOP MESSAGE. MAINTENANCE REMOVED AND REPLACED NR 2 PITOT TUBE.SDR RAIA00310275Anti-Ice Valve · defective5723-CID- ENGINE NR 1 AIR INLET ANTI-ICE INDICATION. MAINTENANCE DEFERRED NR 1 ENGINE ANTI-ICE VALVE PER MEL 30-21-01. SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING NR 1 ENGINE ANTI-ICE VALVE.SDR C2XA03SH421Battery · dischargedSHV-DURING C-CHECK THE NR 2 EMERGENCY LIGHT BATTERY WAS FOUND TO HAVE NO OUTPUT. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY IAW EMB 145 AMM 33-50-04. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH420Wire · damagedSHV-DURING C-CHECK THE AFT AISLE EMERGENCY PROXIMITY LIGHT STRIP WOULD NOT ILLUMINATE. MAINTENANCE REPAIRED THE LIGHT STRIP WIRING IAW EMB 145 AMM 33-50-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH413Floorbeam · corrodedSHV-DURING C-CHECK THE LT CENTER OMEGA BEAM WAS FOUND TO BE CORRODED FROM FRAME 22-23 AND FRAME 24-25. MAINTENANCE REMOVED DAMAGED AREAS AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03BT103Ballast · defectiveCREW REPORTED ON TAXI, ELECTRICAL BURNING SMELL IN (THE VICINITY OF) ROW FOUR IN THE CABIN. MAINTENANCE REMOVED AND REPLACED LIGHT BALLAST AND WIRING FOR SEAT 4A AND 5A SIDEWALL LIGHTS. OPS CHECKED GOOD, NO BURNING SMELL NOTED IAW EMB145 MM NR 3321-00. AIRCSDR C2XA03SH409Buttstrap · corrodedSHV- DURING C-CHECK THE FORWARD DIGITAL BUTTSTRAP BETWEEN FRAMES 25 AND 16 WAS FOUND TO BE CORRODED. 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 RAIA00310271Bleed Valve · failed5693-STL- APU BLEED FAIL MESSAGE. MAINTENANCE REMOVED AND REPLACED APU BLEED VALVE.SDR C2XA03SH408Floorbeam · corrodedSHV- DURING C-CHECK THE CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-22-10 FIGURE 203 SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH406Buttstrap · corrodedSHV- DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 18 AND 23 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 C2XA03SH405Angle · corrodedSHV- DURING C-CHECK THE CENTER RAMP ANGLE AT FRAME 20 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 C2XA03SH404Buttstrap · corrodedSHV- DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 23 AND 29 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 SIMA200329703Floorbeam · corrodedDURING AN MBV INSPECTION, FOUND CORROSION ON LEFT FLOORBEAM, PREV REPAIR, AT FRAME 20. REMOVED PREVIOUS REPAIR, CORROSION LIMITED TO UPPER DOUBLER ANGLE OF PREVIOUS REPAIR. FABRICATED A DOUBLER ANGLE. REPAIR DONE IAW EMB 145, SRM 145/1142 REV 23, CHAPTER 53-SDR SIMA200329704Sill · corrodedDURING MBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED SERVICE CENTER DOOR SILL. INSTALLED NEW SILL IAW EMB SRM, SRM EMB 145-1142 REV 23, CHAPTERS 51-40-02, 04, 05, 06, 07, 51-20-01 AND 51-20-03. (M)SDR RAIA00310270Control Unit · malfunctioned5295-STL- BRAKE INBOARD INOP MESSAGE. MAINTENANCE REMOVED AND REPLACED BRAKE CONTROL UNIT.SDR C2XA03TY186Stringer Clip · corrodedDURING A SCHEDULED INSPECTION SEVERAL SIGNS OF CORROSION WERE FOUND ON THE STRINGER CLIP BETWEEN FRAME 60 AND 61. MAINTENANCE REMOVED AND REPLACED THE STRINGER CLIP AT FRAME 60 BETWEEN STRINGERS 20L AND 21L IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASEDSDR C2XA03TY185Floorbeam · corrodedDURING A SCHEDULED INSPECTION THE CENTER FLOORBEAM CAP AT FRAME 61 WAS FOUND TO BE CORRODED AROUND SEVERAL NUT PLATES. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM CAP IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.SDR C2XA03TY184Sill · corrodedDURING A SCHEDULED INSPECTION THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED IN SEVERAL AREAS. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW EMB SRM 53-21-60 AND CPM 51-21-04, 51-21-05 AND 51-21-06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF SDR C2XA03TY183Floorbeam · corrodedDURING A SCHEDULED INSPECTION THE LEFT HAND FLOORBEAM AT FRAME 18 WAS FOUND TO BE CORRODED IN SEVERAL AREAS. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW EMB SRM 53-21-10 AND CPM 51-21-04, 05 AND 06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECSDR C2XA03TY182Sill · corrodedDURING A SCHEDULED INSPECTION THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW EMB SRM 51-10-02, 53-21-10 AND CPM 51-21-05,06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.SDR C2XA03TY181Channel · corrodedDURING A SCHEDULED INSPECTION SEVERAL AREAS OF CORROSION WERE FOUND ON THE SERVICE DOOR CUTOUT SILL. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW EMB SRM 53-21-10 AND CPM 51-21-04, 05, 06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF THE INSPECTION.SDR C2XA03SH401Sill · corrodedDURING C-CHECK THE LT SILL AT FR 18 TO FR 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH400Sill · corrodedDURING C-CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03BT097Control Lever · faultyEWR---CO3418, CREW REPORTED, LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. EICAS MESSAGE LDG GEAR DISAGREE. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL LEVER IAW EMB145 MM 32-32-00, AND PERFORMED SEVERAL LANDING GEAR EXTENSIONS AND RETRACTIONS IAW SDR C2XA03SH399Rib · dentedDURING C-CHECK THE NR 1 ENGINE LOWER COWLING AFT RIB WAS FOUND TO BE DENTED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RIB IAW EMB 145 SRM 54-10-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH398Floorbeam · corrodedDURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CENTER FLOORBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH397Sill · corrodedDURING C-CHECK THE SERVICE DOOR AFT 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 C2XA03SH395Rib · gougedSHV- DURING C-CHECK THE NR 1 LOWER ENGINE COWLING AFT RIB WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH394Structure · gougedSHV- DURING C-CHECK THE NR 2 LOWER COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH393Longeron · gougedDURING C-CHECK THE NR 2 LOWER ENGINE COWLING INBOARD LONGERON WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH392Crossbeam · corrodedSHV- DURING C-CHECK THE UPPER CROSS BEAM AT FR 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE UPPER CROSS BEAM AT FR 23 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH391Structure · chafedSHV-DURING C-CHECK THE NR 2 LOWER ENGINE COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
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