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 RAIA00206169Connector5290-RIC- DURING TAKE OFF GOT TAKEOFF CONFIGURATION BRAKE WARNING. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BRAKE PRESSURE SWITCH CONNECTOR.SDR RAIA00205167Filter Element · clogged5281-PIT- #2 ENGINE WILL NOT START. MAINTENANCE REMOVED AND REPLACED THE #2 ENGINE START VALVE FILTER.SDR RAIA00205165Computer · overheated5261-ITH- RECEIVED #2 ATTITUDE HEADING REFERENCE SYSTEM WARNING . MAINTENANCE REMOVED AND REPLACED THE #2 AHRS COMPUTER.SDR 000163Tire · wornLEFT O/B TIRE WORN AND FUEL SMELL IN CABIN. REMOVED AND REPLACED TIRE. GROUND RUN, NO FUEL SMELL NOTICED.SDR 000162A/C Pack · malfunctionedNR 2 PACK OVERLOAD ON EICAS FOLLOWED BY SMOKE IN CABIN. DEFERRED NR 2 PACK.SDR RAIA00206188Strap · corrodedBLK CK TASK 3 532300220804A00 FOUND CORROSION ON STRAP AT FRAME 14 Y479. REMOVED AND REPLACED STRAP AT FRAME 14 Y479 IAW EMB-145 SRM 51-40-02.SDR RAIA00206187Strap · corrodedBLK CK TASK 3 532300220804A00 FOUND CORROSION ON STRAP AT FRAME 17 BETWEEN Y0 AND Y479. REMOVED AND REPLACED STRAP AT FRAME 17 BETWEEN Y0 AND Y479 IAW EMB-145 SRM 51-40-02.SDR RAIA00206186Support · corrodedBLK CK TASK 3 532300220804A00 FOUND CORROSION AT LEFT DIGITAL BETWEEN FRAMES 20&23. REMOVED AND REPLACED LEFT DIGITAL BETWEEN FRAMES 20&23 IAW EMB-145 SRM 51-40-02.SDR RAIA00206185Support · corrodedBLK CK TASK 3 532300220804A00 FOUND CORROSION AT RAMP SUPPORT FRAME 20 Y0. REMOVED AND REPLACED RAMP SUPPORT FRAME 20 Y0 IAW EMB-145 SRM 51-40-02.SDR RAIA00206184Sill · corrodedBLK CK TASK 3 532300220804A00 FOUND CORROSION AT LEFT SILL BETWEEN FRAME 14&20 AT 16L. REMOVED AND REPLACED LEFT SILL BETWEEN FRAMES 14&20 AT 16L IAW EMB-145 SRM 51-40-02.SDR RAIA00206183Gusset · corrodedBLK CK TASK 3 532300220804A00 FOUND CORROSION ON GUSSET AT FRAME 23-Y0 REMOVED AND REPLACED GUSSET AT FRAME 23 Y0 IAW EMB 145 SRM 51-40-02SDR RAIA00206182Fitting · corrodedBLK CK-TASK# 532100210805A00 FOUND "U" SHAPE LATERAL FITTING BENEATH PAX DOOR CORRODED. REMOVED AND REPLACED FITTING IAW EMB 145 SRM 51-40-02.SDR 000161Cooling Fan · obstructedCREW REPORTED PFD FAILURE AND POPPED C/B TO F30 ELECT BAY COOLING. CREW DECIDED TO RETURN TO FIELD. PFP OPS CHECK GOOD. CLEANED DEBRIS FROM COOLING FAN.SDR RAIA00205164Transducer · leaking5258-PIT- #1 HYDRAULIC SYSTEM FAILED. MAINTENANCE REMOVED AND REPLACED LEAKING PRESSURE TRANSDUCER.SDR RAIA00205161Filter5283-PIT- LEFT ENGINE WILL NOT START. MAINTENANCE REMOVED AND REPLACED THE STARTER CONTROL VALVE FILTER.SDR SIMA200215119Switch · failedAMA - FLT 3861 - FLIGHT CREW REPORTED ENGINE NR 2 THRUST REVERSER HAD FAILED INDICATION ON EICAS DURING APPROACH. REPLACED LOWER OUTBOARD STOW SWITCHES AND BOTH UPPER STOW SWITCHES S/N'S 2374, 2370. (M)SDR 000160Smoke Detector · false indicationPILOT INITIATED FIRE EXTINGUISHER FOR THE BAGGAGE COMPARTMENT AFTER EICAS BAGGAGE SMOKE INDICATION IN FLIGHT. REMOVED AND REPLACED THE BAGGAGE COMPARTMENT SMOKE DETECTOR ASSEMBLIES.SDR 000159Fire Loop · faultyE-2 FIRE DETECTION MSG. REMOVED AND REPLACED ENGINE FIRE LOOP.SDR C2XA02IA114Computer · faultyIAH- FLIGHT 3668, ON CLIMB THE CREW NOTED THAT THE CABIN ALTITUDE AND RATE WERE MISSING, AND THE CREW WAS UNABLE TO CONTROL THE CABIN ALTITUDE. THE CREW RETURNED THE AIRCRAFT TO IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 IC600 COMPUTER,SDR C2XA02IA113Computer · faultyIAH- FLIGHT 3668, ON CLIMB THE CREW NOTED THAT THE PITCH TRIM MAIN SYSTEM WAS INOPERATIVE AND NO TRIM INDICATION. THE CREW RETURNED THE AIRCRAFT TO IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 IC600 COMPUTER, PERFORMED OPERATIONAL CHECKS SDR RAIA00205155Computer · overheated5285-PIT- OVERHEAT INDICATION #2 AHRS. MAINTENANCE REMOVED AND REPLACED #2 AHRS COMPUTER.SDR 000157Sense Line · malfunctionedLT ENGINE HIGH ITT AT TAKEOFF. REMOVED AND REPLACED BLEED SENSE LINE.SDR RAIA00206181Support · corrodedBLK CK - TASK# 53Z241214001A00 - CORROSION ON FLOOR SUPPORT AT CBL AND JUST AFT OF FRAME 19. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-02.SDR RAIA00206180Doubler · corrodedBLK CK - TASK# 53Z241214001A00 - CORROSION ON DOUBLER AT CBL FRAME 19. REMOVED AND REPLACED DOUBLER IAW SRM 51-40-02.SDR RAIA00206179Sill · corrodedBLK CK - TASK# 53Z241214001A00 - SURFACE CORROSION ON WEB SILL PLATE AT BL 18R AT FRAME 19. REMOVED AND REPLACED SILL PLATE IAW SRM 51-40-02.SDR RAIA00206178Fitting · corrodedBLK CK - CORROSION ON FLOORBOARD STRINGER AT CBL BETWEEN FRAMES 15 AND 18. REMOVED AND REPLACED T-SHAPE IAW SRM 51-40-02.SDR RAIA00206177Floor Support · corrodedCORROSION ON FLOORBOARD GUSSET AT CBL AT FRAME 18 AT FLOORBOARD HOLE. REMOVED AND REPLACED GUSSET IAW SRM 51-40-02.SDR RAIA00206176Gusset · corrodedBLK CK - TASK# 53Z241214001A00 - CORROSION ON FLOORBOARD STRINGER AT BL 18L THRU CBL AT FRAME 18. REMOVED AND REPLACED GUSSET IAW SRM 51-40-02.SDR C2XA02TY092Wire · brokenTYS, DURING A SCHEDULED INSPECTION, THE EMERGENCY PROXIMITY FLOOR LIGHT STRIP HAS A WIRE BROKEN. MAINTENANCE REMOVED AND REPLACED THE LIGHT STRIP, OPERATIONAL CHECKED GOOD IAW EMB-145-AMM-33-50-12. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASESDR C2XA02TY091Floorbeam · corrodedTYS, DURING A SCHEDULED INSPECTION, CORROSION WAS FOUND ON THA LEFT OMEGA BEAM AT FRAME 20. MAINTENANCE CUT OUT THE CORRODED AREA, FABRICATED ANGLES, SHIMS AND FILLER, THEN INSTALLED. IAW EMB-145-SRM-53-21-10 AND 51-40-02. THE REPAIR WAS SATISFACTORY AND THESDR C2XA02TY090Plate · corrodedTYS, During a scheduled inspection, minor corrosion was found on tha aft digital plate at frames 16 and 17. Maintenance removed the corrosion and replaced the corroded rivits. I/A/W-EMB-145-SRM-51-10-02, 51-40-02 and 51-21-04/05 & 06. The repair was satisfactoSDR C2XA02TY089Floorbeam · corrodedTYS DURING A SCHEDULED 1C/2C INSPECTION THE TOP CAP AT FRAME 17-18 WAS CORRODED. MAINTENANCE REMOVED THE CORROSION AND BLENDED THE AREA, REPLACED THREE RIVET'S, ALODINE, PRIMED AND PAINTED IAW EMB 145 SRM 51-40-02, 51-10-02, 51-21-04-05-06. ALL WORK WAS ACCSDR C2XA02TY088Angle · corrodedTYS DURING A SCHEDULED 1C/2C INSPECTION THE LEFT AFT AISLE RAMP ANGLE AT FR. 20 WAS CORRODED. MAINTENANCE REMOVED AND FAB.A NEW ANGLE AND SHIM AND INSTALL ,ALLODINE,PRIMED AND PAINTED IAW EMB51-30-01 AND 51-21-04,05,06. ALL WORK WAS ACCOMPLISH AND WILL BE RELSDR C2XA02TY087Angle · corrodedTYS DURING A SCHEDULED 1C/2C INSPECTION CORROSION WAS FOUND ON THE RAMP ANGLE AT FRAME 20. MAINTENANCE REMOVED AND REPLACED RT RAMP ANGLE AT FRAME 20 IAW EMB 145 SRM 51-40-02. THE WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.SDR C2XA02TY086Battery · dischargedTYS DURING A SCHEDULED 1C/2C INSPECTION THE BACK-UP BATTERY FAIL THE FUNCTIONAL CHECK. MAINTENANCE REMOVED AND REPLACED THE BACK-UP BATTERY IAW EMB-145 AMM 24-35-01 AND THE FUNCTIONAL CHECK WAS GOOD IAW EMB 145 AMM 24-35-01-700-801 A. ALL WORK WAS ACCOMPLISSDR C2XA02TY085Skin · nickedTYS During a scheduled inspection the L/H #1 passenger window frame was found to be nicked. Maintenance accomplished a blend out repair which included a NDT inspection IAW EMB GST#1393/02, EMB-145 M.M. 56-20-00, CPM 51-21-04, 51-21-05, and 51-21-06. The reSDR C2XA02TY084Skin · nickedTYS During a scheduled inspection the #1 right hand passenger window frame was found to be damaged (nicked). Maintenance accomplished a blend out repair which included a NDT inspection IAW EMB GST#1392/02, EMB-145 M.M. 56-20-00, CPM 51-21-04, 51-21-05 and 5SDR C2XA02TY083Skin · corrodedTYS DURING A SCHEDULED INSPECTION THE SERVICE DOOR CUTOUT SKIN WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW EMB GST 1395/02, EMB145 CPM 51-21-04, 51-21-05 AND 51-21-06, THE REPAIR WAS SATISFACTORY. THE AIRCRSDR C2XA02TY082Structure · dentedTYS DURING A SCHEDULED 1C-2C INSPECTION THE PAX DOOR LOWER AFT CORNER WAS DENTED. DENT MEASUREMENT'S WERE 1.25 INCH L BY .1875 INCH. MAINTENANCE RESTORED THE PROFILE, INSPECTED FOR CRACKS, NONE NOTED. ALL WORK WAS ACCOMPLISH AND WILL BE RELEASED UPON COMPSDR C2XA02TY081Structure · crackedTYS DURING A 1C/2C INSPECTION, THE NR 1 LOWER COWLING AFT EDGE MEMBER WAS CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFT EDGE MEMBER. ALL WORK WAS ACCOMPLISHED IAW EMB 135/145 SRM 51-20-03, CPM 51-21-04-05-06 AND SRM 51-40-02. ALL WORK WAS ACCOMPLISHED ASDR C2XA02TY080Hinge Fitting · wornTYS DURING A SCHEDULED 1C/2C INSPECTION THE HORIZ. STAB HINGE PIN LOCKING BRACKETS ON THE LT. AND RT. SIDE HAD WEAR STEPS IN THEM. MAINT. BLENDED THE WEAR STRIPS,PERFORMED NDT INSPECTION,ALLODINED,PRIMED AND PAINTED IAW WITH GST#1391/02-EMB 135/145 CPM 51-21SDR C2XA02TY079Cap · corrodedTYS DURING A SCHEDULED 1C/2C INSPECTION, BOTH LT AND RT BEARING CAPS HAD CORROSION ON THE MLG. MAINTENANCE REMOVED AND REPLACED BOTH FWD AND AFT LOWER BEARING CAPS IAW AMM 32-10-01, WHICH WAS ACCOMPLISH AND WILL BE RELEASED UPON COMPLETION OF ALL C-CHECK INSDR C2XA02TY078Doubler · corrodedTYS DURING A SCHEDULED 1C/2C INSPECTION, THE OMEGA BEAM DOUBLERS AT FRAMES 20 AND 22 WERE FOUND CORRODED. MAINTENANCE FABRICATED A NEW OMEGA BEAM DOUBLER'S AND REPLACED IAW EMB 145-SRM-53-21-10. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETIOSDR C2XA02RI004Strut · faultyRIC FLT 3576-CREW REPORTED AIR/GROUND FAIL MESSAGE IN FLIGHT. THE CREW RETURNED TO RIC WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE NOSE LANDING GEAR CENTERING UNIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR STRUT ASSEMBLY, AND PSDR C2XA02TY077Line · chafedTYS, DURING A SCHEDULED INSPECTION THE FIRE EXTINGUISHING DISCHARGE LINE WAS FOUND CHAFED ON THE LEFT ENGINE. MAINTENANCE REMOVED AND REPLACED THE LINE IAW EMB-145-AMM-26-21-06.SDR C2XA02TY076Bulkhead · gougedTYS, During a schedule inspection the forward pressure bulkhead was found gouged under the windshield wiper moter. Maintenance blended out the damage, performed dye penetrant inspection, alodined and primed I/A/W-EMB-135/145-CPM-51-21-04,51-21-05 and GST-1423/SDR C2XA02CL107Liner · missingCLE FLIGHT 3595 THE CREW REPORTED ON LANDING RECEIVED A APU FIRE INDICATION. THE APU WAS SHUT DOWN AND THE INDICATION CLEARED. MAINTENANCE INSPECTED AND FOUND THE EXHAUST SILENCER LINER ASSEMBLY WAS MISSING. THE EXHAUST SILENCER ASSEMBLY WAS REPLACED AND OPSDR C2XA02IA096Module · inoperativeIAH- DURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY LIGHTS FAILED TO ARM. IAH- MAINTENANCE REMOVED AND REPLACED THE CABIN CONTROL MODULE FOR LIGHTS, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS SDR 000156Battery · dischargedNR 3 AND 4 EMERGENCY LIGHT BATTERIES DEAD. INSTALLED NR 3 AND 4 EMERGENCY LIGHT BATTERIESSDR 000155Battery · dischargedNR 1 AND 2 EMERGENCY LIGHT BATTERIES DEAD. INSTALLED NR 1 AND 2 EMERGENCY LIGHT BATTERIES.
Back to Embraer EMB-145