Embraer EMB-145LR
Service difficulty reports · 36,799
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 = 'EMB145LR' 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 = 'EMB145LR' 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 SIMA20130517001Contactor · inoperativeTHE CREW REPORTED THAT DURING THE CLIMB OUT, RECEIVED MW FUEL 2 LOW LEVEL. NOTICED A LOUD BANGING UNDER COCKPIT FLOOR. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. R & R THE EBC NR 1 K0079 CONTACTORSDR SIMA20130516002Light · inoperativeDURING MX INSPECTION, FOUND THE RT OVER WING EMERGENCY LIGHT INOPERATIVE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE RT OVERWING EMERGENCY LIGHT IAW AMM 33-50-10. THE OPS CHECKED GOOD. THE ACFT WAS RETURNED TO SERVICE.SDR CHQA20130515179Floor Support · damagedDURING INSPECTION, A MISDRILLED HOLE WAS IDENTIFIED ON A REPAIR DOUBLER ON THE RIGHT OMEGA BEAM AT FRAME 23. THE BEAM WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-009615.SDR SIMA20130515004Light · inoperativeDURING B INSPECTION FOUND THE MAIN CABIN DOOR MOUNTED EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN CABIN DOOR MOUNTED EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. THE OPERATISDR SIMA20130515002Handle · lack of lubeON FLIGHT 2939 THE CREW REPORTED THE MAIN CABIN DOOR HANDLE WAS DIFFICULT TO OPERATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED EXTERNAL HANDLE IAW PART TASK 52-18-00-640-00-640-001-A00. OPENED AND CLOSED GOOD IAW EMB145 AMM 52-10-00. THE AIRCRAFT SDR SIMA20130515001Unknown · odorON FLIGHT 2793 THE CREW REPORTED THAT ON CLIMBOUT THEY FLEW THROUGH A FLOCK OF BIRDS. SUSPECT ENGINE 1 & 2 INGESTION. FOUL ODOR THRU PACKS SHORTLY THERE AFTER. THE AIRCRAFT WAS REMOVED FROM SERVICE. ACCOMPLISHED BIRD STRIKE INSPECTION IAW WORKCARD 05-200-0SDR CHQA20130514184Torque Box · damagedDURING INSPECTION, THE LEFT WING LOWER SURFACE MOST INBOARD RIB/FLAP TORQUE BOX FORWARD MOST INBOARD HOLE SHOWS DAMAGE INDICATIONS. THE AREA WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-009827.SDR RAIA201305140001Reservoir · lowDURING CRUISE FLIGHT THE FLIGHT CREW GOT A HDY 1 LOW QUANTITY MESSAGE. CREW DECLARED AND EMERGENCY. MAINTENANCE INSPECTED FOR HDY LEAKS, SERVICED AND BLEED THE RESERVOIR. NO LEAKS FOUND AND SYSTEM OPS CHECK GOOD.SDR ASOA20130514315TFloor Support · corrodedCORROSION AT RT OMEGA BEAM AT NUTPLATE HOLES CORRODED BEYOND LIMITS. R & R HAT SECTION ASSY.SDR ASOA20130514314Profile · corrodedCORROSION AT "T" PROFILE BEYOND LIMITS. R & R T PROFILE LT SIDE AT OMEGA BEAM.SDR ASOA20130514313Gusset · corrodedCORROSION AT GUSSET Y=0.00 CORRODED AROUND SCREW HOLES BEYOND LIMITS. R & R GUSSETSDR ASOA20130514312Gusset · corrodedCENTER OMEGA BEAM GUSSET HAS CORROSION BEYOND LIMITS. R & R GUSSET.SDR CHQA20130513185Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR CLIP AT FRAME 66 BETWEEN STRINGERS 6L AND 7L. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20130513180Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR CLIP AT FRAME 65 BETWEEN STRINGERS 9L AND 7L. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20130513178Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OMEGA BEAM FRAME 20 REPAIR AT THE CARBON FIBER CROSSMEMBER ATTACH POINT. THE ARE WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-01.SDR CHQA20130513177Fitting · corrodedDURING INSPECTION, CORROSION WAS FOUND UNDER THE COCKPIT FLOOR ON THE SHEAR FOOT AT FRAME 11 AND STRINGER 21L. THE SHEAR FOOT WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-009728.SDR RAIA201305130001Actuator · malfunctionedDURING CLIMB FLIGHT CREW GOT A PITCH TRIM MAIN AND BACKUP FAIL MESSAGE ON EICAS. CREW DECLARED AN EMERGENCY AND RETURNED TO IAD. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE HORZ STAB ACTUATOR. SYSTEM OPS CHECKED GOOD.SDR ASOA20130513075Skin · crackedDURING A-CK INSPECTION THE AFT FUSELAGE II SKIN WAS FOUND TO BE CRACKED AT A RIVET BELOW STR 6L ON FR78. MX REMOVED THE DAMAGE, AND PERFORMED A FILLER/DOUBLER REPAIR IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-02501, AND THE ACFT WAS APPROVED FOR RSDR ASOA20130513074Skin · crackedDURING "A" CHECK INSPECTION, THE AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET EBLOW STR 8L AT FR77. MX REMOVED THE DAMAGE, AND PERFORMED A FILLER/DOUBLER REPAIR IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-02501, AND THE ACFT WAS APPROVED FSDR ASOA20130513073Skin · crackedDURING "A" CHECK INSPECTION, THE AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET BELOW STR 2R AT FR75. MX REMOVED THE DAMAGE, AND PERFORMED A FILLER/DOUBLER REPAIR IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-02501, AND THE ACFT WAS APPROVED SDR ASOA20130513072Skin · crackedDURING "A" CHECK INSPECTION, THE AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET BELOW STR 8R AT FR77. MX REMOVED THE DAMAGE, AND PERFORMED A FILLER/DOUBLER REPAIR IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-02501, AND THE ACFT WAS APPROVED FOSDR ASOA20130513071Skin · crackedDURING "A" CHECK INSPECTION, THE AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET BELOW STRINGER 4R AT FR78. MX REMOVED THE DAMAGE, AND PERFORMED A FILLER/DOUBLER REPAIR IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-02501, AND THE ACFT WAS APPROSDR ASOA20130513311Gusset · corrodedCORROSION BEYOND LIMITS ON GUSSET. R & R GUSSET.SDR ASOA20130513310Floor Support · corrodedFLOOR SUPPORT CORRODED BEYOND LIMITS. R & R FLOOR SUPPORT.SDR ASOA20130513309Floor Support · corrodedRT FLOOR SUPPORT CORRODED BEYOND LIMITS. R & R FLOOR SUPPORT.SDR ASOA20130513308Floor Support · corrodedCORROSION BEYOND LIMITS AT FLOOR SUPPORT. R & R FLOOR SUPPORT.SDR ASOA20130513307Floor Support · corrodedRT FLOOR SUPPORT CORRODED BEYOND LIMITS. R & R FLOOR SUPPORT.SDR ASOA20130513306Sill · corrodedRT SILL CORRODED BEYOND LIMITS. R & R SILL.SDR ASOA20130513305Sill · corrodedLT SILL CORRODED BEYOND LIMITS. R & R SILL.SDR ASOA20130513304Sill · corrodedLT SILL CORRODED BEYOND LIMITS. R & R SILL.SDR RAIA201305120001Switch · malfunctionedDURING CLIMB THE THE FLIGHT CREW GOT AN LANDING GEAR/AIR FAIL EICAS MESSAGE AND THE LANDING GEAR FAILED TO RETRACT. CREW DECLARED AN EMERGENCY AND RETURNED TO ORD. MAINTENANCE INSPECTED THE AIRCRAFT, AND THE AIRCRAFT WAS FERRIED FROM ORD TO STL GEAR DOWN. MSDR CHQA20130511183Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE NUT PLATE ON THE RIGHT OMEGA BEAM AT FRAME 23. THE BEAM WAS REPAIRED IN ACCORDANCE WITH SRM 51-40-02 AND ETD 2013-145-009615.SDR SIMA20130511003Power Unit · defectiveON FLIGHT 3350 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT WAS INOPERABLE (CHARGING LIGHT SHOWS FLASHLIGHT CHARGING BUT FAILS TO ILLUMINATE). THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT POWER UNIT IAW EMB AMM145 33-51-SDR SIMA20130511002Door · obstructedON FLIGHT 4290 THE FLIGHT ATTENDANT REPORTED SHE HAD A DIFFICULT TIME OPENING THE MAIN CABIN DOOR. THE HANDLE OPERATED SMOOTHLY, YET DOOR WAS HUNG UP AND MAIN CABIN DOOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND SEVERAL SECURITY SEALS ON DOOR FRAME SEALSDR SIMA20130511001Smoke Warning · false activationON FLIGHT 4046 CREW REPORTED WHILE CRUISING AT FLIGHT LEVEL 330 60 MILES WEST OF BUFFALO THEY RECEIVED AN EICAS BAGGAGE SMOKE MESSAGE AND MASTER WARNING LIGHT. THE CREW COMPLIED WITH MEMORY ITEMS, EPC AND AOM VOL 1 CHECKLIST AND DECLARED AN EMERGENCY. DIVERTSDR ASOA20130423152Door Frame · corrodedDURING A-CHECK, PAX DOOR CUTOUT WAS FOUND CORRODED AT FRAME 18 BETWEEN STRINGERS 15-16L. MX REMOVED THE CORRODED SECTION AND PERFORMED A SPLICE REPAIR IAW EC5310-01690. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR RAIA201305100006Support · corrodedDURING SCHEDULED MAINTENANCE, FOUND CORROSION AROUND TRANSPONDER. MX R & R THE SUPPORT ASSY AROUND THE TRANSPONDER ANTENNA.SDR RAIA201305100005Floor Support · corrodedDURING SCHEDULED MX, THE CARGO BAY FLOORBOARD SUPPORT PLATE ON BEAM Y-479 AT FRAME 65 TO FRAME 68 WAS FOUND CORRODED. MX R & R THE CARGO BAY FLOORBOARD SUPPORT PLATE ON BEAM Y-479 AT FRAME 65 TO FRAME 68.SDR RAIA201305100004Support Angle · corrodedDURING SCHEDULED MX, CARGO BAY RAMP SUPPORT ANGLE WAS FOUND CORRODED AT FRAME 65. MX R & R THE CARGO BAY RAMP SUPPORT ANGLE.SDR ASOA20130510046Window Frame · crackedDURING POST FLIGHT WALKAROUND, CREW REPORTED FINDING A FUSELAGE SKIN CRACK ON THE LT DV WINDOW UPPER FRAME AREA. MX PERFORMED REPAIR ON UPPER BEAM ATTACHED TO DV WINDOW AND WINDSHIELD POST ON LT SIDE IAW SRM 51-40-02. SHV MX ALSO PERFORMED REPAIR ON LT DV SDR RAIA201305100003Smoke Detector · false activationDURING FLIGHT, RECEIVED A CARGO SMOKE WARNING. FIRE BOTTLE DISCHARGED AND ACFT LANDED. MX INSPECTED AND FOUND NO INDICATION OF FIRE OR SMOKE. MX R & R THE HIGH RATE BAGGAGE FIRE BOTTLE. SYS OPS CHECKED GOOD. MAINTENANCE INSPECTED THE FIRE WARNING SYSTEM ASDR CHQA20130509163Battery · dischargedDURING INSPECTION, THE AFT OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR SIMA20130509003Wire · brokenDURING B INSEPECTION, FOUND THE SERVICE DOOR EMERGENCY EXTEROR LIGHT INOPERATIVE DUE TO A BROKEN WIRE. REPAIRED BROKEN WIRE IAW EMB WM 20-21-00. AIRCRAFT RETURNED TO SERVICE.SDR RAIA201305090001Connector · defectiveDURING CLIMB THE FLIGHT CREW SELECTED GEAR UP BUT THE HANDLE DID NOT MOVE, GEAR REMAINED DOWN AND LOCKED. CREW GOT A LANDING GEAR AIR FAIL MESSAGE ON EICAS. AIRCRAFT RETURNED TO IAH. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE RIGHT MLG FWD PROX SWITSDR SIMA20130509002Light · inoperativeDURING B INSPECTION FOUND THE LEFT WING EMERGENCY LANDING LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT EMERGENCY LANDING LIGHT LAMP IAW EMB AMM 33-41-02-000-801-A AND 33-41-02-400-801-A. THE OPERATIONAL CHECK WAS GOSDR CHQA20130508166Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT OMEGA BEAM SURFACE AT THE FORWARD NUT PLATE HOLE FOR THE GUSSET AT FRAME 20. THE RIGHT OMEGA BEAM AT FRAME 20 WAS REPAIRED IN ACCORDANCE WITH SRM 53-21-10 AND 51-40-02.SDR SIMA20130508002Battery · defectiveDURING UNSCHEDULED MAINTENANCE INSPECTION FOUND THE ELT BATTERY REQUIRES REPLACEMENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE ELT BATTERY IAW EMB145 AMM CHAPTER 25-61-04. NEW BATTERY EXPIRATION DATE IS APR/2018. THE BATTERY CHECK WASDR ASOA20130508150Frame · crackedDURING C-CHECK, FRAME 10 CRACKED UNDER RT DV WINDOW. MX R & R FRAME 10 AT RT UNDER DV WINDOW IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130508149VBeam · corrodedDURING C-CHECK CARGO DOOR CUTOUT LOWER BEAM 65-68 IS CORRODED (LOCAL LEVEL 2). MX PERFORMED REPAIR ON CARGO DOOR CUTOUT LOWER BEAM AT FRAMES 65-68 IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130508148VSeat Track · corrodedDURING C-CHECK LT UPPER SEAT TRACK SUPPORT CORRODED. (LOCAL LEVEL 2) AT FRAME 50. MX PERFORMED REPAIR TO LT UPPER SEAT TRACK SUPPORT FRAME 50 IAW EC5320-01522, REV B. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
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