Embraer EMB-145ER
Service difficulty reports · 1,266
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 = 'EMB145ER' 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 = 'EMB145ER' 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 C2XA04SH411Sill · corrodedSHV - DURING C-CHECK THE LEFT SILL WAS FOUND TO BE CORRODED FROM FRAME 42 TO 47. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH410Sill · corrodedSHV - DURING C-CHECK THE RIGHT SILL WAS FOUND TO BE CORRODED FROM FRAME 42 TO 47. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH409Strap · corrodedSHV - DURING C-CHECK THE FORWARD DIGITAL WAS FOUND TO BE CORRODED FROM FRAME 17 TO 18. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10, STEP 4, FIG 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH408Strap · corrodedSHV - DURING C-CHECK THE FORWARD DIGITAL A FRAME 14 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10, STEP 4, FIG 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH407Shear Tie · crackedSHV - DURING C-CHECK THE SHEAR TIE WAS FOUND TO BE CRACKED AT FRAME 68 AND STRINGERS 6R-7R. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SHEAR TIE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH406Buttstrap · corrodedSHV - DURING C-CHECK THE LEFT HAND OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 24 TO FRAME 36. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH405Sill · corrodedSHV - DURING C-CHECK THE RIGHT HAND FLOOR SILL WAS FOUND TO BE CORRODED FROM FRAME 36 TO FRAME 41. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH404Sill · corrodedSVH - DURING C-CHECK THE RIGHT HAND FLOOR SILL WAS FOUND TO BE CORRODED FROM FRAME 24 TO FRAME 29. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH403Buttstrap · corrodedSHV - DURING C-CHECK THE RIGHT HAND OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 61 IN THE LAV. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH452Spar · crackedDURING C-CHECK EDDY CURRENT INSPECTION USING EDDY CURRENT PROBE TEST BLOCK TB-M030B AS A STANDARD, LT WING SPAR 3 UPPER O/B HOLE FOR TORQUE BOX 1 ATTACH REVEALED A CRACK. MX REAMED HOLE TO 8.382MM(.330) AND REINSPECTED. CRACK WAS NOT REMOVED. HOLE WAS REAMESDR C2XA04SH434Floorbeam · corrodedSHV - DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10, STEP 2, FIG 201 SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH424Rib · chafedSHV - DURING C-CHECK THE NR 2 ENGINE LOWER COWLING AFT EDGEMEMBER 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 C2XA04SH402Doubler · corrodedSHV - DURING C-CHECK THE CARGO FORWARD PARTITION FRAME DOUBLER WAS FOUND TO BE CORRODED AT FRAME 61 BETWEEN STRINGERS 16L AND 17L. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICESDR C2XA04SH401Sill · corrodedSHV - DURING C-CHECK THE LEFT HAND FORWARD CARGO FLOOR SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 61 AND 65. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH400Floorbeam · corrodedSHV - DURING C-CHECK THE RIGHT HAND OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 19. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 207. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH451Doubler · crackedSHV - DURING C-CHECK THE DOUBLER ON FRAME 61 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH416Rib · chafedSHV - DURING C-CHECK THE NR 2 ENGINE UPPER COWLING AFT EDGEMEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGEMEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH448Buttstrap · corrodedSHV - DURING C-CHECK THE LEFT BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WILL BE APPROVED FOR RETURN TO SERVICE UPON COMPLETION OF C-CHECK.SDR C2XA04SH447Buttstrap · corrodedSHV - DURING C-CHECK THE LEFT BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WILL BE APPROVED FOR RETURN TO SERVICE UPON COMPLETION OF C-CHECK.SDR C2XA04SH440Buttstrap · corrodedSHV - DURING C-CHECK THE CENTER OMEGA BEAM 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 C2XA04SH428Buttstrap · corrodedSHV - DURING C-CHECK THE LEFT OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 29-37. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH427Buttstrap · corrodedSHV - DURING C-CHECK THE CENTER OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 29-37. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH4426Buttstrap · corrodedSHV - DURING C-CHECK THE CENTER OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 39-45. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH425Buttstrap · corrodedSHV - DURING C-CHECK THE LEFT OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 53-58. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04BT071Battery Pack · faultyCREW REPORTED, ODOR OF WIRE INSULATION BURNING IN COCKPIT AND FLIGHT ATTENDANT JUMPSEAT, ALONG WITH CABIN AND CABIN EMERGENCY PUSHBUTTONS ILLUMINATING. MAINTENANCE FOUND EMERGENCY BATTERY NR 2 NOT INSTALLED CORRECTLY. REMOVED AND REPLACED NR 2 EMERGENCY BATTSDR C2XA04SH399Sill · corrodedSHV - DURING C-CHECK THE LEFT SILL WAS FOUND TO BE CORRODED FROM FRAME 53 TO 59. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH398Sill · corrodedSHV - DURING C-CHECK THE LEFT SILL WAS FOUND TO BE CORRODED FROM FRAME 36 TO 41. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04CL066Connector · looseCLE FLIGHT 3352, CREW REPORTED THAT THE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED SYSTEM AND FOUND A LOOSE CONNECTOR ON THE EMERGENCY LIGHT INVERTER. MAINTENANCE RESECURED THE CONNECTOR. SYSTEM OPERATIONALLY CHECKED GOOD.SDR C2XA04SH397Rib · chafedSHV - DURING C-CHECK THE NR 1 UPPER ENGINE COWLING FT EDGEMEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGEMEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH396Floorbeam · corrodedSHV - DURING C-CHECK THE AFT DIGITAL WAS FOUND TO BE CORRODED AT FRAME 19. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH431Bracket · corrodedSHV - DURING C-CHECK THE MAIN DOOR FORWARD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH430Bracket · corrodedSHV - DURING C-CHECK THE MAIN DOOR AFT U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04IA078Proximity Sensor · inoperativeIAH - FLIGHT 2891 DURING CLIMBOUT OF LCH THE CREW REPORTED THAT THE LANDING GEAR DID NOT RETRACT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NLG WEIGHT ON WHEELS PROXIMITY SWITCH, OPERATIONAL CHECKED GOOD, AND THE ASDR C2XA04SH393Sill · corrodedSHV - DURING C-CHECK THE LEFT SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 TO 29. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH395Doubler · corrodedSHV - DURING C-CHECK THE DOUBLER AT FRAME 20 WAS FOUND TO BE CORRODED AROUND THE NUT PLATES. MAINTENANCE REMOVED AND REPLACED THE DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH394Buttstrap · corrodedSHV - DURING C-CHECK THE CENTER BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH389Sill · corrodedSHV - DURING C-CHECK THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC5320-01089. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04BT070Bulb · burned outCREW REPORTED, STRONG ODOR OF BURNED ELECTRICAL COMPONENTS IN CABIN ROW 7 AREA. MAINTENANCE REMOVED AND REPLACED SIDEWALL LIGHT ASSEMBLY AT ROW 5 AND 6 AREA IAW EMB 145 MM 33-21-06, OPS CHECKED LIGHTS GOOD.SDR C2XA04SH388Sill · corrodedSHV - DURING C-CHECK THE LEFT HAND FLOOR SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 19 AND 24. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH446Angle · corrodedSHV - DURING C-CHECK THE CENTER RAMP ANGLE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE AFFECTED RAMP ANGLE IAW EMB 145 SRM 51-40-02 AND WILL REPLACE THE AFFECTED ANGLE WHEN THE PART BECOMES AVAILABLE. THE AIRCRAFT WILL BE APPROVED FOR RETURN TO SERVICESDR C2XA04SH445Buttstrap · corrodedSHV - DURING C-CHECK THE CENTER BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 19 TO 23. MAINTENANCE REMOVED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. MAINTENANCE WILL REPLACE THE AFFECTED BUTTSTRAP WHEN PART BECOMES AVAILABLE. THE AIRCRAFT WILL BE APSDR C2XA04IA075Light · looseIAH - FLIGHT 2551, DURING PREFLIGHT INSPECTION THE LOWER FORWARD SERVICE DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE LOOSE. MAINTENANCE RESECURED THE AFFECTED EMERGENCY LIGHT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04IA080Seal · dryEWR - FLIGHT 2311, THE CREW REPORTED THAT THE MAIN CABIN DOOR JAMS WHEN OPENING, AND IS VERY DIFFICULT TO OPEN. MAINTENANCE LUBED THE PASSENGER DOOR, OPERATIONALLY CHECKED GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04IA069Wire · looseIAH - DURING AIRCRAFT MODIFICATION SEVERAL EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND GROUND WIRE GS85008DC TO BE LOOSE. MAINTENANCE RESECURED THE GROUND WIRE, OPERATIONALLY CHECKED THE EMERGENCY LIGHTING SYSTEM WITH NO DEFICIENCIESDR C2XA04IA062Lamp · burned outIAH- FLIGHT 2673, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE GALLEY EMERGENCY LIGHT, AND FLOOR PROXIMITY LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE GALLEY EMERGENCY LIGHT BULB, RESET THE EMERGENCY LIGHT SYSTEM, ANSDR RAIA00406029Light · inoperative3548 - PIT - LAST FLOOR EMERGENCY STRIP LIGHT PARTIALLY INOPERATIVE. MAINTENANCE DEFERRED STRIP LIGHT PER MEL 33-50-00-2. SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING STRIP LIGHT.SDR C2XA04IA079Control Panel · contaminatedDURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE MIDDLE EMERGENCY LIGHTS ON THE FLOOR WOULD NOT ILLUMINATE. MAINTENANCE CLEANED THE CONNECTION AT THE FLIGHT ATTENDANTS LIGHTING CONTROL PANEL, OPERATIONALLY TESTED THE SYSTEM AND CLEARED THE DISCREPANCY.SDR C2XA04BT063Light · inoperativeCREW REPORTED PASSENGER DOOR EMERGENCY EXIT LIGHT IS INOPERATIVE. RESET EMERGENCY EXIT LIGHT SYSTEM, SYSTEM OPS CHECKED GOOD. AFTER ARRIVING IN EWR, DURING PREFLIGHT FOUND EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE INSPECTED SYSTEM, OPERATIONALLY TESTED SDR C2XA04CL059Inverter · inoperativeTHE CREW REPORTED THE EMERGENCY EXIT SIGN WAS INOPERATIVE WHEN TESTED. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.SDR C2XA04CL058Sign · inoperativeTHE CREW REPORTED THE EMERGENCY EXIT SIGN ABOVE THE FLIGHT ATTENDANT JUMPSEAT WAS INOPERATIVE. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE EMERGENCY LIGHT SYSTEM. OPERATIONAL CHECKS WERE GOOD. NO DEFECTS WERE FOUND. THE AIRCRAFT RELEASED FOR SERVICE.
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