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 C2XA02SH080Butt Strap · corrodedDURING C CHECK INSPECTION, CORROSION AND PITTING WAS FOUND AROUND RIVETS ON BUTTSTRAP BETWEEN FRAMES 59 AND 61. MAITENANCE REMOVED AND REPLACED AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH079Floorbeam · corrodedSHV-DURING C CHECK INSPECTION, LT LATERAL FLOORBEAM AROUND NUTPLATE HOLES WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND PERFORMED A FLOORBEAM REPAIR IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH077Floorbeam · corrodedSHV-DURING C CHECK INSPECTION DOUBLER ON RT LATERAL FLOORBEAM AT FRAME 20 WAS FOUND WITH CORROSION. MAINTENANCE REMOVED AND REPLACED DAMAGED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH078Floorbeam · corrodedSHV-DURING C CHECK INSPECTION NUTPLATE WAS FOUND WITH CORROSION ON CENTER FLOORBEAM AT FRAME 22. MAINTENANCE REMOVED DAMAGE AND REPLACED FLOORBEAM BETWEEN FRAMES 16 AND 24 IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH076Floorbeam · corrodedDURING C CHECK INSPECTION NUTPLATE WAS FOUND CORRODED ON CENTER FLOORBEAM AT FRAME 18. MAINTENANCE REMOVED AND REPLACED FLOORBEAM BETWEEN FRAMES 16 AND 24 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN SERVICE.SDR C2XA02SH074Angle · crackedDURING C CHECK INSPECTION SPLICED ANGLE AT LT FLOORBEAM BETWEEN FRAMES 16 AND 17 WAS FOUND CRACKED. MAINTENANCE REMOVED DAMAGE AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH075Floorbeam · corrodedSHV-DURING C CHECK FLOORBEAM DOUBLER AT FWD CARGO PARTITION WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED DAMAGED DOUBLER IAW EMB 145 SRM 51-20-03 AND SRM 51-04-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH073Floorbeam · corrodedDURING C CHECK INSPECTION BUTTSRAP ON CENTER FLOORBEAM WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 18 AND 23. MAINTENANCE REMOVED AND REPLACED CENTER FLOORBEAM BETWEEN FRAMES 18 AND 23 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH072Floorbeam · corrodedSHV- DURING C CHECK THE CENTER FLOORBEAM WAS FOUND TO HAVE CORROSION AT GALLEY MOUNT HOLES BETWEEN FRAMES 18 AND 23. MAINTENANCE REMOVED AND REPLACED CENTER FLOORBEAM BETWEEN FRAMES 18 AND 23 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SSDR C2XA02SH071Sill · corrodedDURING C CHECK INSPECTION CORROSION WAS FOUND ON NUTPLATE AT LT SILL BETWEEN FRAMES 20 AND 23. MAINTENANCE REMOVED AND REPLACED LT SILL BETWEEN FRAMES 18 AND 23 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02IA211Sign · inoperativeDURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY EXIT SIGN ON THE CEILING ADJACENT TO THE GALLEY FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EXIT SIGN, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND THE SDR C2XA02BT058Control Unit · faultyCREW REPORTED, "GEAR NOT RETRACTING." MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT AND LANDING GEAR CONTROL LEVER IAW EMB145 AMM 32-32-01 AND 32-32-02. OPERATIONAL CHECKED SYSTEM GOOD. AIRCRAFT RELEASED FOR SERVICE.SDR C2XA02CL188Sensor · defectiveCLE FLIGHT#3397 THE CREW REPORTED #2 ENGINE EXCEEDED THE LIMITS FOR OIL TEMPERATURE WHILE CLIMBING THRU 5000'.POWER WAS REDUCED AND THE TEMPERATURE RETURNED TO NORMAL.THE OIL TEMPERATURE EXCEEDED LIMITS AGAIN A FEW MINUTES LATER AND THE ENGINE WAS SHUTDOWN FORSDR C2XA02BT053Switch · faultyEWR---CO4131, CREW REPORTED, "ON TAKEOFF GOT LND GEAR AIR/GND FAIL. THEREFORE AIRRETURNED." MAINTENANCE REMOVED AND REPLACED LEFT HAND PROXIMITY SWITCH ON SHOCKABSORBER IAW EMB145 MM #32-63-01. EXTENDED AND RETRACTED LANDING GEAR OPS.CHECKED GOOD IAW EMB145 MMSDR C2XA02BT052Control Unit · faultyEWR---CO3537, CREW REPORTED, AIR GROUND SENSOR FAILED AFTER TAKEOFF. AIR RETURN TO EWR. MAINTENANCE TROUBLESHOT PROBLEM, REMOVED AND REPLACED LANDING GEAR ELECTRONIC UNIT IAW EMB145 AMM 32-32-01. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.SDR C2XA02SH058Floorbeam · corrodedSHV- DURING C CHECK INSPECTION, THE RT FLOORBEAM AT FRAME 22 WAS FOUND TO HAVE CORROSION. MAITENANCE REPAIRED AFFECTED AREA OF FLOORBEAM AND REMOVED AND REPLACED A DOUBLER IAW EC 5320-01073. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH059Floorbeam · crackedSHV- DURING C CHECK, SPLICE ANGLE WAS FOUND CRACKED AT LT FLOORBEAM BETWEEN FRAMES 16 AND 17. MAINTENANCE REMOVED AFFECTED AREA AND PERFORMED A SPLICE REPAIR ON LT FLOORBEAM BETWEEN FRAMES 16 AND 17. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH055Floorbeam · corrodedSHV - DURING C-CHECK, CENTER OMEGA BEAM AT AFT GALLEY MOUNTS NUT PLATE HOLES HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED AFFECTED OMEGA BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02CL179Sign · inoperativeCLE FLT 3292 CREW REPORTED THAT THE EMERGENCY EXIT IDENTIFIER SIGN IN THE CENTER CABIN CEILING IS INOP.SDR C2XA02SH061Floorbeam · corrodedDURING C CHECK INSPECTION, LT FLOORBEAM WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 19 AND 21. MAINTENANCE REMOVED AFFECTED PARTS AND REPAIRED LT FLOORBEAM IAW EMB SRM 53-21-10. THE AIRCRAFT WAS RETURN TO MAINTENANCESDR CX2A02SH60Butt StrapSHV DURING C CHECK LEFT HAND LATERAL FLOOR BEAM STRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 15 AND 19. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A SPLICE REPAIR IAW CONTINENTAL EXPRESS EC 5320-01074.THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH051Sill · corrodedSHV- DURING C-CHECK INSPECTION THE RIGHT SILLS FORWARD AND AFT OF SERVICE DOOR WERE FOUND TO HAVE SURFACE CORROSION. MAINTENANCE REMOVED AND REPLACED RIGHT SILLS FORWARD AND AFT OF SERVICE DOOR IAW EMB 145 SRM 51-20-01, SRM 51-40-02, SRM 51-20-03. THE AIRCRASDR C2XA02SH050Butt Strap · corrodedSHV- DURING C-CHECK INSPECTION CORRODED NUT PLATE HOLES WERE FOUND ON CENTER FLOORBEAM BUTT STRAP AT FRAME 18. MAINTENANCE REMOVED AND REPLACED BUTT STRAP BETWEEN FRAMES 17 AND 19 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH048Doubler · corrodedSHV- DURING C-CHECK INSPECTION, CORROSION WAS FOUND ON NUT PLATE HOLES ON DOUBLER AT FRAME 20. MAINTENANCE REMOVED AND REPLACED CORRODED DOUBLER AT FRAME 20 IN ACCORDANCE WITH EMB 145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA02SH057Floor Support · corrodedSHV- DURING C-CHECK, CENTER FLOOR SUPPORT BETWEEN FRAMES 20 AND 23 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH056Floor Support · corrodedSHV- DURING C-CHECK, CENTER FLOOR SUPPORT BETWEEN FRAMES 18 AND 20 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED AFFECTED BUTT STRAP BETWEEN FRAMES 18 AND 20 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH054Angle · corrodedSHV - DURING C-CHECK CENTER FLOORBEAM REINFORCEMENT ANGLE WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 18 AND 20. MAINTENANCE REMOVED AND REPLACED AFFECTED ANGLE IAW EMB -145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH052Doubler · corrodedSHV- DURING C-CHECK DOUBLER AT FRAME 22 WAS FOUND TO HAVE CORROSION IN NUT PLATE HOLES. MAINTENANCE REMOVED AND REPLACED DOUBLER AT FRAME 22 IAW IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH053Butt Strap · corrodedSHV DURING C-CHECK INSPECTION CENTER FLOORBEAM STRAP AT FRAME 18 WAS FOUND TO HAVE CORROSION IN NUT PLATES HOLES. MAINTENANCE REMOVED AND REPLACED AFFECTED BUTT STRAP IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH049Floorbeam · corrodedSHV- DURING C-CHECK INSPECTION, CENTER FLOORBEAM STRAP FOUND TO HAVE NUT PLATES CORRODED AND SURFACE CORROSION FROM FRAME 15 TO 17. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS IAW EMB 145 SRM 53-21-10 PG 210 ITEM 4 FIG 203, INSTALLED REPAIR PARTSDR C2XA02SH047Sill · corrodedSHV- DURING C-CHECK INSPECTION, THE RIGHT SILL AFT OF THE SERVICE DOOR HAD CORRODED NUT PLATE HOLES. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND SILL AFT OF THE SERVICE DOOR IN ACCORDANCE WITH EMB 145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURNSDR C2XA02SH046Sill · corrodedSHV- DURING C-CHECK INSPECTION, THE LEFT SILL HAD CORROSION AROUND THE NUT PLATE HOLES BETWEEN FRAMES 60 AND 61. MAINTENANCE REMOVED AND REPLACED THE LEFT SILL BETWEEN FRAMES 60 AND 61 IN ACCORDANCE WITH EMB 145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FORSDR C2XA02SH045Butt Strap · corrodedSHV-DURING C-CHECK INSPECTION, THE RIGHT HAND LATERAL FLOOR BEAM WAS FOUND TO HAVE CORROSION AROUND THE NUTPLATE HOLES BETWEEN FRAMES 59 AND 61.MIANTENANCE REMOVED AND REPLACED THE RIGHT HAND BUTT STRAP BETWEEN FRAMES 59 AND 61 IN ACCORDANCE WITH EMB 145 SRM 5SDR C2XA02SH044Butt Strap · corrodedSHV-DURING C-CHECK INSPECTION, THE LEFT LATERAL BEAM AND CENTER FLOOR BEAM NUTPLATE HOLES WERE FOUND TO BE CORRODED AT BETWEEN FRAMES 59 AND 61.MAINTENANCE REMOVED AND REPLACED BOTH THE LEFT HAND AND CENTER BUTT STRAP'S BETWEEN FRAMES 59 AND 61 IN ACCORDANCE WSDR C2XA02BT046Light · blownBTV---DURING SERVICE/ROUTINE OVERNIGHT CHECK MAINTENANCE FOUND AISLE OVERHEAD EMERGENCY LIGHT AT EMERGENCY EXIT ROW TO BE INOPERATIVE. REMOVED AND REPLACED LIGHT BULB AT EMERGENCY EXIT OVERHEAD LIGHT IAW EMB145 AMM 33-50-00. OPS. CHECKED LIGHT GOOD.SDR C2XA02SH062Skin · dentedDURING C CHECK INSPECTION, THE MAIN DOOR STRUCTURE WAS FOUND TO HAVE A DENT AFT OF ACTUATING LEVER. MAINTENANCE REMOVED AND REPAIRED DAMAGED AREA IAW EMB 145 SRM 52-10-01. PERFORMED LEAK TEST. LEAK TEST GOOD. IAW EMB 145 MM 21-31-00-700-808-A. THE AIRCRAFT SDR C2XA02BT048Ballast · defectiveEWR---CO3869, ON POSTFLIGHT INSPECTION, CREW REPORTED SMOKE IN THE GALLEY. BAD GALLEY BALLAST. MAINTENANCE REMOVED AND REPLACED BALLAST FOR GALLEY LIGHT. AIRCRAFT RELEASED FOR SERVICE.SDR C2XA02BT041Lamp · faultyBTV---CO3398, DURING SERVICE CHECK MAINTENANCE FOUND THE AFT OVERHEAD AISLE EMERGENCY LIGHT TO BE INOPERATIVE.....REMOVED AND REPLACED THE LAMP IN THE AISLE OVERHEAD EMERGENCY LIGHT. OPS.CHECKED GOOD.SDR C2XA02IA172Engine · power lossFlight 3927 - Crew reported that the #1 engine lost power in flight. The crew shut the engine down and had experienced noticeable vibration after shutdown. The crew diverted to AUS and landed without incident. Maintenance removed and replaced the affected engiSDR C2XA02CL167Inverter · inoperativeCLE FLIGHT#2979 THE CREW REPORTED THE EMERGENCY EXIT SIGN WAS INOPERATIVE.MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT INVERTER.OPERATIONAL CHECKS WERE GOOD.Original Control number was incomplete. Corrected 9/4/02SDR C2XACL167Inverter · inoperativeCLE FLIGHT#2979 THE CREW REPORTED THE EMERGENCY EXIT SIGN WAS INOPERATIVE.MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT INVERTER.OPERATIONAL CHECKS WERE GOOD.SDR C2XA02CL163Sensor · defectiveCLE FLIGHT# 3033 THE CREW REPORTED #1 ENGINE OIL TEMPERATURE WAS HIGH DURING CLIMB.THE ENGINE WAS SHUT DOWN BY THE CREW AND THE AIRCRAFT LANDED IN CLE WITHOUT FURTHER INCIDENT.MAINTENANCE REPLACED THE #1 ENGINE OIL PRESSURE/TEMPERATURE SENSOR.OPERATIONAL CHECKSDR C2XA02CL160Control Unit · faultyCLE - FLIGHT 3218, THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT DURING CLIMB. THE AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFSDR C2XA02IA162Uplock · faultyIAH- DURING A OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM THE MECHANIC NOTED THAT THE RIGHT HAND MLG WAS NOT SHOWING THE CORRECT INDICATION UPON RETRACTION. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND MLG UPLOCK BOX, PERFORMED A OPERATIONAL CHECK OF THESDR C2XA02IA161Warning System · malfunctionedIAH- AFTER TAKEOFF THE LEFT MAIN LANDING GEAR, LANDING GEAR DISAGREE MESSAGE APPEARED, THE CREW RETURNED THE AIRCRAFT TO IAH WITHOUT INCIDENT. MAINTENANCE PERFORMED A OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED SDR C2XA02TY113Computer · malfunctionedTYS AIR RETURN, PILOT REPORTED AHRS DISPLAYED ERRONEOUS HEADING. MAINTENANCE OPERATIONAL CHECKED AHRS SYSTEM IAW-EMB-145-MM-34-21-00-700-801A, ALL SYSTEMS OPERATIONAL CHECKED GOOD. AIRCRAFT RELEASED TO SERVICE.SDR C2XA02IA154Light · inoperativeDURING PREFLIGHT THE CREW NOTED THAT THE CABIN DOOR AND ROW TWELVE (12) WINDOW EXIT EMERGENCY LIGHTING FAILED TO ILLUMINATE.SDR C2XA02IA152Connector · looseIAH - CREW REPORTED THAT ONE OF THE FLOOR PROXIMITY EMERGENCY LIGHT STRIPS DID NOT ILLUMINATE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NR 3 FLOOR STRIP CONNECTOR TO BE LOOSE. THE CONNECTOR WAS RESECURED, THE FLOOR STRIP OPERATIONALLY CHECKED GOOD, ASDR C2XA02IA153Light · malfunctionedMEM - CREW REPORTED THAT THE EMERGENCY LIGHTING STAYED ON WITH SWITCH SELECTED TO THE OFF POSITION. AN ELECTRICAL RESET OF THE SYSTEM WAS ACCOMPLISHED AND THE EMERGENCY LIGHTING SYSTEM OPERATIONALLY CHECKED GOOD.SDR C2XA02TY112Sill · corrodedTYS DURING A SCHEDULED INSPECTION THE FORWARD SERVICE DOOR SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE DOOR SILL IAW EMB-145 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.
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