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 C2XA04SH375Firewall · crackedSHV-DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RIGHT APU MOUNT. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13, STEP 4 FIGURE 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04IA074Odor · detectedIAH - FLIGHT 2197, THE CREW REPORTED A STRONG FUEL ODOR WHEN THE APU WAS STARTED AFTER LANDING. MAINTENANCE OPERATIONALLY CHECKED THE APU WITH NO DISCREPANCIES NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR RAIA00406017O-Ring · leaking3515 - PIT- DURING TAXI NR 2 LEAD LEAK INDICATION. MAINTENANCE REMOVED AND REPLACED DUCT O-RING IN DISTRIBUTION DUCT AFT AVIONICS BAY.SDR C2XA04SH364Crossbeam · corrodedSHV - DURING C-CHECK THE CROSSBEAM AT FRAME 22 FROM THE RIGHT SILL TO THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH363Floorbeam · corrodedSHV - DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25 WHERE THE CARBON FIBER CROSSMEMBER ATTACHES. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-22-10. THE AIRCRAFT WAS APPROVED FSDR C2XA04SH362Plate · corrodedDURING C-CHECK THE SHELL PLATE ON THE CENTER FLOORBEAM AT FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SHELL PLATE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH361Buttstrap · gougedSHV - DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 22 AND 23 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH360Buttstrap · corrodedSHV - DURING C-CHECK THE RIGHT BUTTSTRAP BETWEEN FRAMES 59 AND 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 C2XA04IA067Odor · detectedDURING PRE-FLIGHT INSPECTION, THE CREW REPORTED A SMOKE ODOR IN THE COCKPIT. MAINTENANCE INSPECTED THE AIRCRAFT WITH NO DEFICIENCIES NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04IA068Adc · burned outDURING PRE-FLIGHT INSPECTION, THE CREW REPORTED A SMOKE ODOR IN THE COCKPIT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE AIR DATA COMPUTER TO BE THE SOURCE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED COMPUTER, AND THE AIRCRAFT WAS APPROVED FOR RETURNSDR C2XA04SH359Beam · corrodedSHV - DURING C-CHECK THE CARGO DOOR LOWER CUTOUT BEAM 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 C2XA04SH358Floorbeam · corrodedDURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 23. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC 5320-01124. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH357Floorbeam · corrodedDURING C-CHECK THE LEFT FLOORBEAM 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 202, SHEET 1. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH356Floorbeam · corrodedDURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOORBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH355Angle · corrodedDURING C-CHECK, THE CENTER RAMP ANGLE WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH354Floorbeam · corrodedDURING C-CHECK THE LEFT CROSSBEAM AT FRAME 19 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 C2XA04SH349Firewall · crackedDURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RIGHT HAND MOUNTING BRACKET. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 53-32-13 FIGURE 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH348Buttstrap · corrodedSHV - DURING C-CHECK THE CENTER FORWARD FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH347Skin · dentedDURING C-CHECK THE EXTERNAL FUSELAGE SKIN WAS FOUND TO BE DENTED BETWEEN FRAMES 20 AND 21, AND BETWEEN STRINGERS 12L AND 13L. MAINTENANCE PERFORMED A PATCH REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 53-21-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04BT064Inverter · faultyDURING SERVICE CHECK MAINTENANCE FOUND THE AFT CABIN CEILING EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED NR 6 EMERGENCY EXIT SIGN LIGHT INVERTER IAW EMB145 AMM 33-50-01. OPS CHECKED SYSTEM GOOD.SDR CA040602003Shaft · failed(CAN) IN CLIMB AT 8000 FT A LOUD BANG WAS HEARD AND UNCOMMANDED ENGINE SHUTDOWN AND AIR RETURN AND UNEVENTFUL LANDING OCCURRED. DISASSEMBLY OF THE ENGINE AT RRC REVEALED THAT NR 6 BEARING BEVEL DRIVING GEAR SYSTEM THAT DRIVE MODULE 05 ACCESSORY GEARBOX HAS FSDR RAIA00406007Heater · defectiveDEN - PITOT ONE HEAT INOP INDICATION. MAINTENANCE DEFERRED NR 1 PITOT HEAT PER MEL. SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING THE NR 1 PITOT TUBE.SDR RAIA00405022Duct · looseERI - BLEED AIR LEAK INDICATION NR 1 ENGINE. MAINTENANCE RE-SECURED BLEED AIR DUCT.SDR RAIA00405035Valve · inoperativeEVV - LEFT ENGINE ANTI ICE FAIL MESSAGE. MAINTENANCE DEFERRED NR 1 ENGINE ANTI ICE PER MEL. SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING NR 1 ENGINE ANTI ICE VALVE.SDR RAIA00405020Warning Light · illuminatedSERVICE DOOR WARNING ON TAKEOFF ROLL. MAINTENANCE DEFERRED DOOR WARNING PER MEL.SDR RAIA00405019Warning Light · illuminatedPIT - MAIN DOOR OPEN MESSAGE ON TAKEOFF ROLL. MAINTENANCE PLACED DOOR INDICATING ON DEFERRAL PER MEL.SDR RAIA00405018Start Valve · inoperativeSTL - RIGHT ENGINE NO ROTATION ON START. MAINTENANCE REMOVED AND REPLACED NR 2 AIR START VALVE.SDR C2XA05IA074Light · intermittentPREFLIGHT INSP FOUND EXIT LIGHTS WERE INOP. MX RESET SYSTEM. OPS CHECKED EXIT LIGHTS WITH NO DEFECTS NOTED. ACFT RETURNED TO SERVICE.SDR C2XA04SH309Cowling · chafedDURING C-CHECK THE NR 1 ENGINE LOWER COWLING WAS FOUND TO BE CHAFED ON THE INNER SKIN. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH296Beam · corrodedSHV - DURING C-CHECK THE CARGO DOOR CUTOUT LOWER 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 C2XA04SH295Stiffener · chafedSHV - DURING C-CHECK THE NUMBER 2 ENGINE LOWER 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 C2XA04SH294Skin · dentedDURING C CHECK THE NR 2 ENGINE INTAKE PERFORATED SKIN WAS FOUND TO BE DENTED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 54-20-01, SECTION 7, (FIGURE 207). THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH293Buttstrap · corrodedSHV - DURING C-CHECK THE LEFT OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 20 AND 21. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH292Floorbeam · corrodedDURING C CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 20 AND 23. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 AND EC 5310-01270. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR RAIA00405030Actuator · malfunctionedBOS - ENGINE NR 1 T/R DISAGREE. MAINTENANCE DEFERRED NR 1 T/R PER MEL. SUBSEQUENTLY CLEARED DMI BY ADJUSTING NR 1 T/R BOTTOM ACTUATOR.SDR C2XA04SH291Doubler · corrodedSHV - DURING C-CHECK THE RIGHT FLOORBEAM DOUBLER AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH290Floorbeam · corrodedDURING 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. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH289Angle · corrodedSHV - DURING C-CHECK THE LOWER ANGLE ON THE CROSSBEAM BETWEEN THE SERVICE DOOR AFT SILL AND THE CENTER FLOORBEAM AT FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FORSDR C2XA04SH288Floorbeam · corrodedDURING C-CHECK THE RIGHT HAND FLOORBEAM DOUBLER AT FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH287Sill · corrodedDURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH286Sill · corrodedDURING C-CHECK THE SERVICE DOOR FORWARD 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 C2XA04SH285Firewall · crackedSHV-DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE TOP END OF THE RIGHT HAND VERTICAL STIFFENER. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 53-32-13 FIGURE 204. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH284Sill · corrodedSHV-DURING C-CHECK THE LEFT HAND SILL FROM FRAME 18 TO FRAME 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 C2XA04SH283Sill · corrodedSHV-DURING 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 C2XA04SH282Floorbeam · corrodedSHV-DURING C CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 22. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH281Buttstrap · corrodedSHV-DURING C CHECK THE CENTER OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 18 TO 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 RAIA00405009Control Unit · defective5701-STL- BRAKE DEGRADE MESSAGE. MAINTENANCE REMOVED AND REPLACED BRAKE CONTROL UNIT.SDR C2XAO4SH279Frame · crackedDURING C-CHECK FRAME 22 WAS FOUND TO BE CRACKED BETWEEN STRINGER 21 LT AND 21 RT. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SPLICE REPAIR IAW EMB 145 SRM 53-00-04, PG. 205, FIG. 206. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH278Rib · chafedSHV-DURING C CHECK THE RIGHT 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 C2XA04SH277Angle · corrodedSHV-DURING C CHECK THE RAMP ANGLE ON THE CENTER OMEGA BEAM 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.
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