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 ASOA20140728061Control Unit · faultyTHE CREW REPORTED PRONOUNCED RIGHT PULL WHEN BRAKE IS APPLIED AT TAXI SPEEDS, F/O LEFT BRAKE FEELS SPONGY, BRAKES LOUD WHEN APPLIED. MAINTENANCE INSPECTED AND REPLACED THE BRAKE CONTROL UNIT AND NR 4 BRAKE ASSY. OPS CHECKS WERE GOOD.SDR ASOA20140728060Housing · faultyTHE CREW REPORTED LAVATORY SMOKE WARNING, ELECTRICAL FIRE ODOR IN AND AROUND LAV. LAVATORY LIGHT WARM TO TOUCH. MAINTENANCE INSPECTED AND REPLACED THE LAVATORY LIGHT LAMP HOUSING. OPS CHECKED GOOD.SDR ASOA20140728242Support · corrodedDURING C-CHECK, FOUND SEAT TRACK SUPPORT CORRODED BETWEEN FRAMES 36-41. REMOVED CORROSION AND FOUND WITHIN LIMITS SRM 53-00-11. RESTORED SURFACE PROTECTION IAW CPM 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140728241Floor Support · corrodedDURING C-CHECK, LT FLOOR SUPPORT BETWEEN FRAMES 18 AND 23 CHAFED AND CORRODED. MAINTENANCE REMOVED CORROSION IAW SRM 53-21-10. FOUND OUT OF LIMITS IAW SRM 53-21-10. REMOVED AND INSTALLED FLOOR SUPPORT IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SESDR ASOA20140728240Support · corrodedDURING C-CHECK, MULTIPLE AREAS OF CORROSION ON LT SIDEWALL SEAT TRACK SUPPORT FROM FRAME 41-36. MAINTENANCE REMOVED CORROSION AND WAS FOUND OUT OF LIMITS SRM 53-00-11, R & R IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140728239Support · corrodedDURING C-CHECK, FOUND CORROSION ON LT WALL SEAT TRACK SUPPORT BETWEEN FRAMES 48 AND 52. MAINTENANCE REMOVED CORROSION AND FOUND WITHIN LIMITS SRM 53-00-11. RESTORED SURFACE PROTECTION IAW CPM 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140728238Support · corrodedDURING C-CHECK, FOUND CORROSION ON LT WALL SEAT TRACK SUPPORT BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED CORROSION ON LT WALL SEAT TRACK SUPPORT BETWEEN FRAMES 52 AND 53, WITH-IN LIMITS SRM 53-00-11. RESTORED SURFACE PROTECTION IAW CPM 51-21-06. THE ACFSDR ASOA20140728237Angle · crackedDURING C-CHECK AFT FUSELAGE INSIDE ACCESS 312AR AT FRAME 81, STRINGER 10, RT END CLIP IS CRACKED AT APU FIREWALL. MAINTENANCE R & R FRAME 81, STRINGER 10, RT END CLIP IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140728236Angle · crackedDURING C-CHECK, AFT FUSELAGE INSIDE ACCESS 312AR AT FRAME 81, STRINGER 11, RT END ANGLE IS CRACKED AT APU FIREWALL. MAINTENANCE R & R END ANGLE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA20140727001Bleed Valve · failedFROM REDUCING THRUST AT CRUISE FOR DECENT HEARD & FELT A LOUD BANG. FLIGHT ATTENDANT REPORTS LOUDEST IN CTR OF CABIN. ENGINE INDICATIONS ALL NORMAL DURING CRUISE, POSSIBLE COMPRESSOR STALL. TROUBLESHOT IAW FIM 72-00-00-810-817. R & R RT ENGINE 9TH STAGE VASDR SIMA20140727002Warning System · false activationBLEED 2 LEAK ON EICAS WITH LEAK ILLUMINATED ON BLEED 2 BUTTON. OPERATIONS CHECKED GOOD IAW AMM 36-11-05. OK FOR SERVICE.SDR SIMA20140726021Reveal · crackedRIGHT EMER EXIT WINDOW REVEAL ASSEMBLY IS CRACKED. R & R RT EMER EXIT WINDOW REVEAL ASSEMBLY IAW AMM 25-23-09.SDR SIMA20140726015Splice · damagedEMERGENCY LIGHTING, EXIT LOCATOR, FWD INDICATOR ON CEILING PANEL INOPERATIVE. REPAIRED SPLICES SP 9208 & SP 9209 ON EMER LIGHTING IAW SWPM 20-21-00. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.SDR SIMA20140726014Panel · crackedLEFT & RIGHT RAM AIR PANEL INTAKES ARE CRACKED NEXT TO ACTUATORS. REPAIRED LT & RT RAM AIR PANEL INTAKES IAW ERS-EM-5300-695 OVEN 6132 GAGE 3337.SDR SIMA20140726023Wire · brokenLIGHT STRIP NR 5 HAS BROKEN WIRE AT STRIP. REPLACED NR 5 EMER LIGHT STRIP IAW AMM 33-50-08. SEE BOW 161234 FOR FINAL INSTALL & OPERATIONAL CHECK.SDR SIMA20140726022Support · crackedRIGHT BEAM INBD SUPPORT CRACKED AT FRAME 47. REMOVED CRACKED RT BEAM INBD SUPPORT AT FRAME 47, PREPPED & INSTALLED SERVICEABLE BEAM SUPPORTS IAW SRM 53-23-02.SDR SIMA20140726016Wire · damagedEMERGENCY LIGHTING, EXIT MARKER, AFT OF RT OVERWING EXIT INOPERATIVE. REPAIRED WIRE ON EMER LIGHTING IAW SWPM 20-21-00. OPERATIONS CHECKED GOOD.SDR SIMA20140726020Light · crackedLIGHT STRIP NR 4 EXTRUSION IS CRACKED. REPLACED LIGHT STRIP NR 4 EXTRUSION IAW AMM 33-50-08. SEE BOW 161234 FOR FINAL INSTALL.SDR SIMA20140726019Cover · crackedLEFT WING NR 2 TORQUE BOX COVER CRACKED. REPAIRED LT WING NR 2 TORQUE BOX COVER IAW ERS-EM-5700-216.SDR SIMA20140726018Skin · crackedLEFT FUSELAGE SKIN CRACKED AT FRAME 75, 1ST FASTENER BELOW STRINGER 2L. CRACK APPROX LENGTH 1/2 INCHES. SEE NRWC E400943 FOR CORRECTIVE ACTION FOR REPAIR.SDR SIMA20140726017Window Frame · corrodedPILOT'S WINDSHIELD INNER FRAME CORRODED ALONG LOWER SURFACE NEAR FASTENERS HOLES. BLENDED AREAS ALONG LOWER SURFACE FASTENER HOLES ON PILOT'S WINDSHIELD & ACCEPTED AS IS IAW ERS-EM-5600-041.SDR SIMA20140726012Light · crackedLIGHT STRIP NR 6 EXTRUSION IS CRACKED. REPLACED LIGHT STRIP IAW AMM 33-50-08. SEE BOW 161234 FOR FINAL INSTALL.SDR SIMA20140726011Light · crackedLIGHT STRIP NR 5 EXTRUSION IS CRACKED. REPLACED LIGHT STRIP IAW AMM 33-50-08. SEE BOW 161234 FOR FINAL INSTALL.SDR SIMA20140726009Light · crackedLIGHT STRIP NR 3 EXTRUSION IS CRACKED. REPLACED LIGHT STRIP IAW AMM 33-50-08. SEE BOW 161234 FOR FINAL INSTALL.SDR SIMA20140726008Light · crackedLIGHT STRIP NR 1 EXTRUSION IS CRACKED. REPLACED LIGHT STRIP IAW AMM 33-50-08. SEE BOW 161234 FOR FINAL INSTALL.SDR SIMA20140726013Relief Valve · failedEMERGENCY & PARKING BRAKE SYS THERMAL RELIEF VLV FAILED FUNCTIONAL CHECK. R & R EMER & PARKING BRAKE SYS THERMAL RELIEF VLV IAW AMM 32-44-06. LEAK CHECKED GOOD.SDR SIMA20140726010Skin · crackedRIGHT FUSELAGE SKIN CRACKED AT FRAME 75, 1ST FASTENER BELOW STRINGER 2R. CRACK APPROX LENGTH 3/8 INCHES. SEE NRWC E400940 FOR CORRECTIVE ACTION OF REPAIR FOR RT FUSELAGE SKIN.SDR CHQA20140726236Battery · dischargedDURING INSPECTION THE EMER LIGHTS AFT OF ROW 12 WERE FOUND TO BE INOPERATIVE. REPLACED THE NR 3 EMER LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR SIMA20140726007Light · inoperativeMAIN DOOR EMER LAMP INOPERATIVE. R & R MAIN DOOR EMER LIGHT LAMP IAW AMM 33-50-06-000-801-A & 33-50-06-400-801-A. OPERATIONS CHECKED GOOD.SDR SIMA20140726002Packing · leakingSMOKE & HYD FLUID ON ON LT MAIN GEAR. R & R BLEEDER VLV PACKING IAW CMM 32-49-03. OPERATIONS CHECKED GOOD IAW AMM 32-49-07. LEAK CHECKED GOOD.SDR SIMA20140726003Brake Assy · damagedNUMBER 1 MLG SMOKING AT GATE. REPLACED NR 1 MLG BRAKE ASSEMBLY IAW WC 32-600-14.SDR SIMA20140726004Battery · overtempBATTERY 2 OVER TEMP. R & R NR 1 & 2 MAIN BATTERIES IAW WC 24-600-00. OPERATIONS CHECKED GOOD. NO MSG NOTED. LT PN 32248-001 & SN 10800544.SDR SIMA20140725005Roller · lack of lubeFLIGHT ATTENDANT REPORTS THE MAIN CABIN DOOR IS HARD TO OPEN. LUBRICATED MAIN CABIN DOOR ROLLERS IAW AMM 53-21-02. OPERATIONS CHECKED GOOD.SDR SIMA20140725003Warning System · false activationFLAP FAILURE ALERTED FROM 0 TO 9. OPERATIONS CHECKED FLAPS IAW 27-53-00, OPERATIONS CHECKED GOOD.SDR SIMA20140725001Warning System · false activationBLEED 2 LEAK INDICATION ON EICAS ONLY, APPLIED PROCEDURE & MSG REMAINED. WENT OUT AFTER APPROX 10 - 12 MINUTES. NO FURTHER INDICATION. PERFORMED LEAK TEST OF RT BLEED. OPERATIONS CHECK & LEAK CHECKED GOOD IAW AMM 36-00-00. NO FURTHER DEFECT NOTED.SDR SIMA20140725006Wire · disconnectedNUMBER 5 EMER LIGHT FLOOR STRIP BY OVERWING EXITS INOPERATIVE. SOLDERED WIRE TO CONNECTOR TO EMER LIGHT FLOOR STRIP IAW SWPM 20-30-00. OPERATIONS CHECKED GOOD IAW WC 33-700-17.SDR ASOA20140725235Frame · gougedDURING C-CHECK THE FRAME CHANNEL AT FRAME 61 BETWEEN STRINGERS 16L-17L WAS FOUND TO BE GOUGED. MAINTENANCE BLENDED OUT THE DAMAGE AND PERFORMED A DOUBLER REPAIR IAW SRM 53-00-04. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140725234Yoke · crackedDURING C-CHECK, THE RT ENGINE FORWARD LOWER MOUNT YOKE WAS FOUND TO BE CRACKED. MAINTENANCE R & R THE YOKE IAW EC5450-01094. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140724082Engine · bird ingestionPILOT REPORTED A STRONG ODOR OF SMOKE APPROACH AND SHUTOFF PACKS AND ODOR WENT AWAY. MX INSPECTED ACFT AND DETERMINED NR 1 ENGINE INGESTED A BIRD. MX PERFORMED A BIRD STRIKE INSPECTION, ENGINE COMPRESSOR SECTION BORESCOPE, AND FOD INSPECTION IAW MM 05-50-00. SDR ASOA20140725059Duct · leakingTHE CREW REPORTED AFTER LANDING THERE WAS A BURNING ELECTRICAL ODOR IN THE COCKPIT. MAINTENANCE INSPECTED AND REPLACED THE DUCT ON THE NR 1 PACK HEAT EXCHANGER. OPS CHECKED GOOD.SDR SIMA20140724002Warning System · activatedHYDRAULIC NR 1 SYS LOW CAUTION MSG. TRANSFERRED HYD FROM NR 2 TO NR 1 IAW ETN-EM-29-023. NO LEAKS NOTED ACFT OK FOR SERVICESDR ASOA20140724233Skin · crackedDURING C-CHECK, THE FORWARD FUSELAGE SKIN WAS FOUND TO BE CRACKED AT THE TOP OF THE WINDSHIELD AND LT DV WINDOW LATERAL POST. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5310-01804. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140724232Skin · crackedDURING C-CHECK, THE REAR E/E BAY DOOR INNER SKIN WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5240-01082. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140724231Bracket · wornDURING C-CHECK, THE HORIZONTAL STABILIZER ACTUATOR UPPER MOUNT BRACKET WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE R & R THE BRACKET IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140724230Door Sill · corrodedDURING C-CHECK, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140724229VFitting · wornDURING C-CHECK, THE LT AND RT HORIZONTAL STABILIZER HINGE PIN FITTINGS WERE FOUND TO BE WORN AND WOULD NOT RETAIN THE BUSHINGS. MAINTENANCE PERFORMED A REAMING REPAIR TO THE FIRST OVERSIZE IAW SRM 55-10-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140724228Door Frame · corrodedDURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140724227Door Frame · corrodedDURING C-CHECK, THE CARGO DOOR LOWER FRAME WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE FRAME IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140724226VFloor Support · corrodedDURING C-CHECK, THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAMES 59-61. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01959. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA20140724001Flashlight · faultyFLIGHT ATTENDANT FLASHLIGHT HOLDER ASSEMBLY WILL NOT HOLD FLASHLIGHT SECURELY. R & R FLIGHT ATTENDANT FWD FLASHLIGHT ASSEMBLY & OPERATIONS CHECKED IAW AMM 25-60-03 SATISFACTORY.
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