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 SIMA200206708Floorbeam · corrodedABI - DURING INSPECTION OF AIRCRAFT, FOUND CORROSION ON THE GALLEY CENTER FLOORBEAM AT FRAME 20. REMOVED CORROSION BY BLENDING OUT. FABRICATED AND INSTALLED A 'U' CHANNEL DOUBLER IAW EMB GST-0130A/02 ITEM 6, GST-0276/02 AND STANDARD SRM PRACTICES. (M)SDR SIMA200206707Floorbeam · corrodedABI - DURING INSPECTION OF AIRCRAFT, FOUND CORROSION ON THE GALLEY FLOORBEAM 3 INCH AFT OF FRAME 22. REMOVED CORROSION BY BLENDING OUT. FABRICATED AND INSTALLED U-CHANNEL DOUBLER IAW EMB GST-0130A/02 ITEM 6, AND STANDARD SRM PRACTICES. (M)SDR RAIA00202075Gusset · corrodedMX-STL DURING 8000 HOUR INSPECTION FOUND CORROSION AT CENTER TOP CAP SKIN I/B OF SERVICE DOOR. REMOVED AND REPLACED CENTER TOP CAP SKIN GUSSET, IAW SRM 51-40-02.SDR RAIA00202074Web · corrodedMX-STL- DURING 8000 HOUR INSPECTION FOUND CORROSION ON FORWARD DIGITAL WEB PLATE. REMOVED AND REPLACED FORWARD DIGITAL WEB, IAW SRM 53-21-10SDR RAIA00202073Sill · corrodedMX-STL- DURING 8000 HOUR INSPECTION FOUND CORROSION ON THE GALLEY TIE DOWN POINT AFT OF THE SERVICE DOOR. REMOVED AND REPLACED RIGHT HAND SILL AFT OF SERVICE DOOR, IAW SRM 51-40-02.SDR RAIA00202072Sill · corrodedMX-STL- DURING 8000 HOUR INSPECTION FOUND CORROSION AT TIE DOWN POINT FOR GALLEY FORWARD OF SERVICE DOOR. REMOVED AND REPLACED SILL AT SERVICE DOOR, IAW SRM 53-21-10 AND 51-40-02.SDR RAIA00202071Support · corrodedMX-STL- DURING 8000 HOUR INSPECTION FOUND CORROSION ON ANGLE SUPPORT FOR FORWARD CENTER FLOOR BOARD. REMOVED AND REPLACED ANGLE SUPPORT AT FORWARD CENTER FLOOR BOARD IAW SRM 51-40-02.SDR RAIA00202070Sill · corrodedMX-STL- DURING 8000 HOUR INSPECTION FOUND CORROSION ON FLOOR SUPPORT AFT OF PAX DOOR. REMOVED AND REPLACED LEFT SILL IAW SRM 51-40-02.SDR RAIA00202069Gusset · corrodedMX-STL - DURING 8000 HOUR INSPECTION FOUND CORROSION ON FLOOR SUPPORT AT STRINGER 18L AT FRAME 17. REMOVED AND REPLACED FLOOR SUPPORT GUSSET AT STRINGER 18L FRAME 17 IAW SRM 51-40-02.SDR RAIA00202063Floorbeam · corrodedMX-STL- DURING 8000 HOUR INSPECTION FOUND CORROSION ON CENTER FUSELAGE OMEGA BEAM AT FRAME 20. REPAIRED OMEGA CENTER BEAM.SDR RAIA00201044SillMX-STL- DURING BLOCK CHECK FOUND MODERATE CORROSION ON FLOOR SUPPORTS AFT OF PAX DOOR. REMOVED AND REPLACED LEFT SILL AFT OF PAX DOOR, IAW SRM 51-40-02.SDR RAIA00201039GussetMX-STL- DURING BLOCK CK FOUND MODERATE CORROSION CENTER TOP CAP SKIN AT CENTER BEAM I/B OF SERVICE DOOR. REMOVED AND REPLACED CENTER TOP SKIN GUSSET IAW SRM 51-40-02.SDR RAIA00201041SillMX-STL- DURING BLOCK CHECK FOUND MODERATE CORROSION AT GALLEY TIE DOWN POINT AFT OF SERVICE DOOR. REMOVED AND REPLACED RIGHT HAND SILL AFT OF SERVICE DOOR IAW EMB145 SRM 51-40-02.SDR CHQ00098Electrical Box · shortedPILOT REPORTS SMOKE IN COCKPIT FROM F/O'S RELAY BOX.SDR CHQ00097Electrical Box · shortedPILOT REPORTS SMOKE IN COCKPIT FROM F/O'S RELAY BOX.SDR CHQ00099Smoke · detectedPILOT REPORTS SMOKE IN COCKPIT FROM F/O'S RELAY BOX.SDR C2XA02TY015Attach Fitting · gougedTYS DURING A SCHEDULED INSPECTION THE RIGHT HAND AILERON WAS FOUND TO BE GOUGED AT THE ACTUATOR ATTACHMENT POINT. MAINTENANCE ACCOMPLISHED A BLEND-OUT REPAIR AND DYE PENETRANT INSPECTION IAW EMBRAER GST 0046/02, THE REPAIR WAS FOUND TO BE SATISFACTORY. THE SDR RAIA00201024Stall Warning · malfunctioned5303- PIT- FLAP FAIL/STALL PROTECTION SYSTEM ADVANCED MESSAGE AFTER TAKEOFF. MAINTENANCE RESET FLAP SYSTEM, SYS OPS CHECK OK.SDR RAIA00201023Stall Warning · malfunctioned5281-TOL- STALL PROTECTION SYSTEM NR 2 INOP ALERT MESSAGE ON TAKEOFF ROLL. MAINTENANCE INSPECTED AOA VANE AND OPERATIONAL CHECKED SYSTEM, NO DEFECTS NOTED.SDR CHQ00094Control Unit · failedSPOILER FAIL MESSAGE DURING T/O ROLL, SPOILER CONTROL UNIT REMOVED AND REPLACED WITH A NEW UNIT. OPS CHECKED SERVICEABLE HIGH SPEED TAXI, CHECK C/O.SDR RAIA00201038Gusset · corrodedMX-STL- DURING BLOCK CHECK FOUND CORROSION ON FLOOR SUPPORT AT STRINGER 18L ON EITHER SIDE OF FRAME 17. REMOVED AND REPLACED FLOOR SUPPORT GUSSET AT STRINGER 18L FRAME 17 IAW SRM 51-40-02SDR C2XA02IA012Angle · corrodedIAH- DURING C-CHECK INSPECTION, NOTED: THE RIGHT FLOOR CROSS BEAM LOWER ANGLE HAS CORROSION BETWEEN FR 23 AND 24. MAINTENANCE CUT OUT THE CORRODED SECTION, FABRICATED AND INSTALLED A NEW SECTION.SDR RAIA00201020Receiver · inoperative5293-STL- DURING TAXI #1 COMM WOULD NOT RECEIVE. MAINTENANCE REMOVED AND REPLACED #1 RECEIVER TRANSMITTER.SDR CHQ00092Fitting · leakingAIRCRAFT HAD BLEED LEAK. REMOVED AND REPLACED BLEED FITTING.SDR CHQ00091Warning System · activatedLOUD BANG FOLLOWED BY NR 2 BLEED EICAS MESSAGE.SDR SIMA200206706Doubler · corrodedABI - DURING INSPECTION OF AIRCRAFT, FOUND CORROSION PREVIOUS REPAIR ON THE LEFT OMEGA BEAM AT FRAME 20. REMOVED PREVIOUS REPAIR AND CORROSION BY CUT OUT. FABRICATED AND INSTALLED A DOUBLER ANGLE AND FILLER. A PLATE AND TWO SHIMS IAW EMB145 SRM 145/1142 CHASDR C2XA02TY011Fitting · chafedTYS DURING A SCHEDULED INSPECTION THE HORIZONTAL STABILIZER LEFT HAND FAIL SAFE PIN FITTING WAS FOUND TO BE CHAFED. MAINTENANCE ACCOMPLISHED A BLEND-OUT REPAIR INCLUDING DYE PENETRANT INSPECTION IAW EMBRAER GST-0045/02, THE REPAIR WAS SATISFACTORY. THE AIRSDR C2XA02TY010Fitting · chafedTYS DURING A SCHEDULED INSPECTION THE HORIZONTAL STABILIZER RIGHT HAND FAIL SAFE PIN FITTING WAS FOUND TO BE CHAFED. MAINTENANCE ACCOMPLISHED A BLEND-OUT REPAIR IAW EMBRAER GST-0045/02 WHICH INCLUDED THE DYE PENETRANT INSPECTION. THE REPAIR WAS FOUND TO BESDR C2XA02TY009Fitting · gougedTYS During a scheduled inspection the right hand horizontal stabilizer bearing forward fitting was found to have a internal gouge. Maintenance accomplished a blend-out repair including dye penetrant inspection IAW Embraer GST-0095/02. The repair was satisfSDR C2XA02TY008Bracket · gougedTYS During a scheduled inspection the right hand aileron PCA rod end attachment bracket was found to be gouged. Maintenance acomplished a blend-out repair including a dye penetrant inspection IAW Embraer GST-0046/02. The repair was found to be satisfactorySDR C2XA02TY007Hinge Fitting · gougedTYS, DURING A SCHEDULED 1C/2C INSPECTION THE LEFT HORIZONTAL STAB HINGE FITTING ON VERTICAL STAB WAS FOUND GOUGED ON THE UPPER SURFACE, ABOVE THE PIN BEARING. MAINTENANCE BLENDED OUT THE DAMAGE, PERFORMED DYE-PENETRATE INSPECTION (NO CRACKS FOUND) AND RESTORESDR C2XA02TY006Hinge Fitting · gougedTYS, DURING A SCHEDULED 1C/2C INSPECTION, THE RIGHT HORIZONTAL STAB HINGE FITTING ON VERTICAL STAB WAS FOUND GOUGED ON THE UPPER SURFACE, ABOVE THE PIN BEARING. MAINTENANCE BLENDED OUT THE DAMAGE, PERFORMED DYE-PENETRATE INSPECTION (NO CRACKS FOUND) AND RESTOSDR CHQ00090B-Nut · looseLOST NR 1 HYDRAULIC (DECLARED EMERGENCY) LANDED IN CMH. B-NUT WAS FOUND LOOSE ON NOSEWHEEL STEERING MANIFOLD, TIGHTENED SCREW AND OPS CHECK GOOD.SDR C2XA02TY005Line · dentedTYS DURING A SCHEDULED 1C/2C INSPECTION, THE NR 1 ENGINE FIRE EXTINGUISHER LINE AT FRAME 70 IN THE CARGO BAY WAS FOUND DENTED. MAINTENANCE REMOVED AND REPLACED THE LINE IAW EMB-145-AMM-20-10-03. REPAIR PROCEDURES WERE SATISFACTORY AND THE AIRCRAFT WILL BE RSDR C2XA01TY228Line · dentedTYS, DURING A SCHEDULED 1C/2C INSPECTION, THE NR 1 ENGINE FIRE EXTINGUISHER LINE AT FRAME 70 IN THE CARGO BAY WAS FOUND DENTED. MAINTENANCE REMOVED AND REPLACED THE LINE IAW EMB-145-AMM-20-10-03. REPAIR PROCEDURES WERE SATISFACTORY AND THE AIRCRAFT WILL BE RSDR C2XA01TY227Line · dentedTYS, DURING A SCHEDULED 1C/2C INSPECTION, THE NR 2 ENGINE FIRE EXTINGUISHER LINE AT FRAME 70 WAS FOUND DENTED. MAINTENANCE REMOVED AND REPLACED THE FIRE EXTINGUISHER LINE IAW-EMB-145-AMM-20-10-03. THE REPAIR PROCEDURES WERE SATISFACTORY AND THE AIRCRAFT WILLSDR RAIS00201004Warning System · malfunctioned5278-GRR- CREW REPORTED MAIN PITCH TRIM FAILED AFTER TAKEOFF. MAINTENANCE DID FUNCTIONAL CHECK OF PITCH TRIM SYSTEM. SYS OPS CHECK OK.SDR CHQ00088Warning System · activatedICE CONDITIONS AND A/I INOP ON EICAS. ABORTED TAKEOFF AND CANCELLED FLIGHT.SDR CHQ00087Proximity Switch · dirtyCREW RETURNED TO FIELD DUE AUTO PRESSURIZATION INOP. DECIDED TO RAISE GEAR AGAIN AND TRY MANUAL PRESS, GOT LANDING GEAR DISAGREE AND COULD NOT GET GEAR BACK UP. RESET A/C AND CLEANED ALL PROX SWITCHES ON THE LANDING GEAR. TEST FLIGHT GOOD FOR GEAR AND PRESSSDR C2XA02IA007Sill · corrodedIAH- DURING C-CHECK IT WAS NOTED THAT THE GALLEY AREA HAS NUMEROUS AREAS OF CORROSION ON THE UPPER SURFACES OR THE FLOORBEAMS FROM FRAME 15 TO FRAME 23. MAINTENANCE REMOVED AND REPLACED THE RIGHT FLOOR SILL FROM FRAME 22 TO FRAME 23 AND THE AIRCRAFT WAS APPRSDR C2XA02IA006Sill · corrodedIAH- DURING C-CHECK IT WAS NOTED THAT THE GALLEY AREA HAS NUMEROUS AREAS OF CORROSION ON UPPER SURFACES OF FLOORBEAMS FROM FRAME 15 TO FRAME 23. MAINTENANCE REMOVED AND REPLACED THE RIGHT FLOOR SILL FROM FRAME 19 TO FRAME 20 AND THE AIRCRAFT WAS APPROVED FORSDR C2XA02IA005Floorbeam · corrodedIAH- DURING C-CHECK INSPECTION IT WAS NOTED THAT THE OMEGA BEAM AT FRAME 20 WAS CORRODED. MAINTENANCE REMOVED THE CORRODED AREA, FABRICATED A FILLER, REINFORCEMENT AND INSTALLED IT ON THE OMEGA BEAM AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE, WHEN RSDR C2XA01IA426Apu · leakingLCH- DURING TAXI, THE APU SHUT DOWN WITH APU FAIL EICAS MESSAGE,FOLLOWED BY SMOKE IN COCKPIT and CABIN. DOWNPOWERED A/C. I TRIED TO RESTART AFTER SEVERAL MINUTES,APU SPOOLED ONLY TO 5% FOR TEN SECONDS, THEN SHUT DOWN AGAIN, AIRCRAFT RETURNED TO GATE. LCH- SDR C2XA02IA004Floor Support · corrodedIAH- DURING "C" CHECK IT WAS NOTED THAT THE FLOOR BEAM CROSS STRUCTURE ABOVE FUSELAGE FRAME 23 WAS CORRODED AT THE INBOARD FORWARD CORNER. IAH- MAINTENANCE REMOVED THE DAMAGED AREA,AND, INSTALLED A DOUBLER WITH A FILLER,AND, THE AIRCRAFT WAS APPROVED FOR RESDR CHQ00080Engine · making metalNR 2 ENGINE ABNORMAL VIBRATION. FOUND CHIPS ON ALL CHIP DETECTOR. REPLACED ENGINE ON AIRCRAFT.SDR SIMA200201815Channel · corrodedABI - LEVEL 2 CORROSION ON CENTER HAT BEAM AT FRAME 20. REPLACED CENTER HAT BEAM AT FRAME 20 IAW EMB 145 SRM 51-40-02 AND EMB GST 4142/01. (M)SDR CHQ00076Cap · out of positionAFTER TAKEOFF, F/A NOTICED LOUD AIR RUSHING FROM BEHIND LAV MIRROR, CAPT AND F/O VERIFIED AND TURNED OFF EACH PACK SEPARATELY, AND TRIED APU BLEED, NOISE CONTINUED. NOTICED WHILE AIRCRAFT WAS PRESSURIZED, FOUND AIR COMING FROM WATER TANK, FOUND CAP THAT ATTACSDR SIMA200201806Channel · corrodedLEVEL 2 CORROSION, ON RIGHT HAT BEAM AT FRAME 23. BLENDED OUT CORROSION ON INSTALLED DOUBLER ON RIGHT HAT BEAM AT FRAME 23 IAW EMB GST 4055/01. (M)SDR SIMA200201807Angle · corrodedLEVEL 2 CORROSION ON RIGHT 'L' PROFILE AT FRAME 23. REPLACED RT 'L' PROFILE AT FRAME 23 IAW EMB 145 SRM 51-40-02. (M)SDR SIMA200201808Crossbeam · corrodedCORROSION ON RIGHT CROSS MEMBER AT FRAME 23. REPLACED RIGHT CROSS MEMBER AT FRAME 23 IAW EMB 145 SRM 51-40-02. (M)
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