Embraer EMB-145LR
Service difficulty reports · 36,797
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 SIMA20151113003Flap · malfunctionedFLAP FAIL ON APPROACH, FAILED AT 0. RESET FLAP SYS & PERFORMED OPERATIONS TEST IAW AMM 27-51-00, WITH NO DEFECTS.SDR SIMA20151113002Attach Angle · crackedRIGHT WING LOWER LATERAL FAIRING ATTACHMENT ANGLE, 3RD FROM THE AFT IS CRACKED. REPLACED ANGLE IAW SRM 51-40-02.SDR SIMA20151113001Power Supply · inoperativeEMERGENCY LIGHTS LISTED ARE INOPERATIVE. EXTERNAL LT FWD WING FUSELAGE, MAIN DOOR ARM LIGHT & MAIN DOOR EXIT SIGN. R & R NR 1 EMER LIGHT BATTERY & BATTERY POWER SUPPLY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD. EMER LIGHTING BATTERY PN 2013-1ASMI & SN 6702SDR SIMA20151112011Connector · missingEMERGENCY LIGHT STRIP CONNECTOR AT FLOOR PANEL 261BF MISSING, ACFT SIDE. INSTALLED MISSING CONNECTOR AT FLOOR PANEL 261BF, ACFT SIDE, SP9212 WIRE NR W192-8832-22 IAW SWPM 20-50-00.SDR SIMA20151112009Skin · chafedFUSELAGE SKIN CHAFED UNDER PANEL 424DB. REPAIRED FUSELAGE SKIN CHAFE UNDER PANEL 424DB IAW ERS-EM-53MR-1779.SDR SIMA20151112010Skin · chafedFUSELAGE SKIN CHAFED UNDER PANEL 414DB. REPAIRED FUSELAGE SKIN CHAFE UNDER PANEL 414DB IAW ERS-EM-53MR-1778.SDR SIMA20151112008Battery · inoperativeR & R NR 3 EMER LIGHTING BATTERY ASSEMBLY & BATTERY CHARGER. R & R BATTERY ASSEMBLY & BATTERY CHARGER ASSEMBLY IAW WC 33-700-19. BATTERY CHARGER ASSEMBLY PN 11-0049.SDR SIMA20151112007Spoiler · crackedFOUND CRACK ON RT WING MIDDLE HINGE ATTACH POINT SURFACE OF INBD SPOILER. TRANSFERRED TO NRWC 604-MQT-02515. COMPLIED WITH REPAIR OF CRACK IAW ERS-EM-57MR-550. REF NRWC 604-MQT-02515.SDR UHLA201511120788Pressure Switch · malfunctionedDURING CLIMBOUT, THE CREW RECEIVED RUDDER 1 AND 2 INOPERATIVE MESSAGES. THE MESSAGES PERSISTED AFTER FOLLOWING THE QRH, THEREFORE THE CREW RETURNED TO THE FIELD OF DEPARTURE FOR AN UNEVENTFUL UNSCHEDULED LANDING. MAINTENANCE TROUBLESHOT THE MESSAGES TO AND RSDR SIMA20151112004Cradle · brokenAFTER PARKING, NOTICED A CLIP TO RETAIN FLASHLIGHT BEHIND CAPTAIN SEAT IN CRADLE HAS BROKEN OFF. R & R CAPTAIN'S FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.SDR SIMA20151112002Skin · damagedLEFT AFT FUSELAGE SKIN SHOWS ADVERSE SCREEN INDICATIONS DURING HFEC. THREE PLACES AT FRAME 75, BETWEEN STRINGERS 1L & 3L. REPAIRED LT AFT FUSELAGE SKIN IAW ERS-EM-53MR-1751.SDR SIMA20151112003Skin Panel · damagedHAIL DAMAGE EVENT. REPLACE FWD FUSELAGE II CROWN SKIN PANEL. ACFT WAS REMOVED FROM SERVICE FOR SKIN REPLACEMENT & WILL BE RETURNED TO SERVICE AFTER SKIN REPLACEMENT. R & R FWD FUSELAGE II CROWN SKIN PANEL IAW SRM 53-12-01 SI, 51-20-01, 51-20-03, 51-40-06, 5SDR SIMA20151112005Light · inoperativeMAIN DOOR EMER LIGHT INOPERATIVE. R & R MAIN DOOR EMER LIGHT LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.SDR SIMA20151112001Hinge Fitting · gougedRUDDER 2 TO RUDDER 1, UPPER HINGE FITTING, UPPER LUG IS GOUGED. INSTALLED NEW RUDDER 2 UPPER HINGE FITTING IAW SRM 55-40-02 & ETN EM-55-070.SDR SIMA20151111001Door Frame · crackedTOP OF FRAME 6, CRACKED AT LAST FASTENER HOLE AT CARGO DOOR LOWER SILL. REPAIRED TOP OF FRAME 67, CRACK AT LAST FASTENER HOLE IAW ERS-EM-53MR-1772.SDR SIMA20151111002Door Frame · crackedTOP OF FRAME 66 CRACKED AT LAST FASTENER HOLE AT CARGO DOOR LOWER SILL. REPAIRED TOP OF FRAME 66 CRACKED AT LAST FASTENER HOLE IAW ERS-EM-53MR-1772.SDR ASOA20151110191Floor Support · corrodedDURING C-CHECK. CENTER OMEGA BEAM CORRODED AT FRAME 59. REPAIRED CENTER OMEGA BEAM AT FRAME 59 IAW EC5310-01473, REV D. ACFT IS APPROVED FOR RETURN TO SERVICE.SDR SIMA20151109015Fitting · wornLEFT PCA TO AILERON ATTACH LUG BUSHINGS ARE MIGRATED. LT DAMPNER TO AILERON ATTACH LUG BUSHING REQUIRES REPLACEMENT, SEIZED TO BOLT. R & R PCA FITTING IAW EO EM-27MR-112. REPLACED DAMPER FITTING IAW EO EM-27MR-112. FITTING PN 145-69382-609.SDR SIMA20151109014Door Frame · crackedACCESS DOOR 123BL HAS A 1 INCH CRACK ON THE FRAME UNDER THE IPI PIN BRACKET. R & R FRAME UNDER ACCESS DOOR 123BL, PIP PIN BRACKET IAW SRM 51-10-02.SDR SIMA20151109012Bushing · migratedRIGHT AILERON PCA TO AILERON INBD ATTACHMENT, OTBD HAT BUSHING MIGRATING. REPLACED PCA FITTING IAW EO EM-27MR-112.SDR SIMA20151109013Door Sill · corrodedCARGO DOOR SILL IS CORRODED. R & R CARGO DOOR SILL IAW SRM 51-40-02.SDR SIMA20151109011Bracket · crackedBAGGAGE DOOR FWD TORSION SPRING BRACKET IS CRACKED. R & R BAGGAGE DOOR FWD TORSION SPRING BRACKET IAW SRM 51-40-02.SDR SIMA20151109009Skin · damagedHAIL DAMAGE EVENT. REPLACE CTR FUSELAGE II RT SKIN PANEL. ACFT WAS REMOVED FROM SERVICE FOR SKIN REPLACEMENT & WILL BE RETURNED TO SERVICE AFTER SKIN REPLACEMENT. R & R CTR FUSELAGE II RT SKIN PANEL IAW SRM 53-22-01 SI, 51-20-01, 51-20-03, 51-40-06, 51-40-0SDR SIMA20151109007Skin Panel · damagedHAIL DAMAGE EVENT. REPLACE CTR FUSELAGE I LT SKIN PANEL. ACFT WAS REMOVED FROM SERVICE FOR SKIN REPLACEMENT & WILL BE RETURNED TO SERVICE AFTER SKIN REPLACEMENT. R & R CTR FUSELAGE I LT SKIN PANEL IAW SRM 53-21-01 SI, 51-20-01, 51-20-03, 51-40-06, 51-40-02,SDR SIMA20151109006Skin Panel · damagedHAIL DAMAGE EVENT. REPLACE CTR FUSELAGE IV TOP SKIN PANEL. ACFT WAS REMOVED FROM SERVICE FOR SKIN REPLACEMENT & WILL BE RETURNED TO SERVICE AFTER SKIN REPLACEMENT. R & R CTR FUSELAGE IV TOP SKIN PANEL IAW SRM 53-24-01 SI, 51-20-01, 51-20-03, 51-40-06, 51-40SDR SIMA20151109005Skin Panel · damagedHAIL DAMAGE EVENT. REPLACE FWD FUSELAGE II SKIN, WIPER PANEL. ACFT WAS REMOVED FROM SERVICE FOR SKIN REPLACEMENT & WILL BE RETURNED TO SERVICE AFTER SKIN REPLACEMENT. R & R FWD FUSELAGE II SKIN IAW SRM 53-12-01 SI, 51-20-01, 51-20-03, 51-40-06, 51-40-02, CPSDR SIMA20151109010Skin Panel · dentedHAIL DAMAGE EVENT. REPLACE CTR FUSELAGE II TOP SKIN PANEL. ACFT WAS REMOVED FROM SERVICE FOR SKIN REPLACEMENT & WILL BE RETURNED TO SERVICE AFTER SKIN REPLACEMENT. R & R CTR FUSELAGE II TOP SKIN PANEL IAW SRM 53-22-01 SI, 51-20-01, 51-20-03, 51-40-06, 51-40SDR SIMA20151109004Skin Panel · damagedHAIL DAMAGE EVENT. REPLACE FWD FUSELAGE I LT SKIN PANEL. ACFT WAS REMOVED FROM SERVICE FOR SKIN REPLACEMENT & WILL BE RETURNED TO SERVICE AFTER SKIN REPLACEMENT. R & R FWD FUSELAGE I LT SKIN PANEL IAW SRM 53-11-01 SI, 51-20-01, 51-20-03, 51-40-06, 51-40-02,SDR SIMA20151109003Skin Panel · damagedHAIL DAMAGE EVENT. REPLACE FWD FUSELAGE I RT SKIN PANEL. ACFT WAS REMOVED FROM SERVICE FOR SKIN REPLACEMENT & WILL BE RETURNED TO SERVICE AFTER SKIN REPLACEMENT. R & R FWD FUSELAGE I RT SKIN PANEL IAW SRM 53-11-01 SI, 51-20-01, 51-20-03, 51-40-06, 51-40-02,SDR SIMA20151109001Controller · failedFLAP FAIL ON EICAS MSG DURING APPROACH. TROUBLESHOOTING IAW FIM TASK 27-51-00-810-817. CMC INDICATED RT TRANSMISSION FAIL. RESET FLAP SYS & PERFORMED OPERATIONAL CHECK. OPERATIONS CHECKED GOOD. NO DEFECTS NOTED OR MSGS NOTED. ON PUSHBACK AFTER NR 1 ENG SSDR SIMA20151109002Cradle · brokenFLASHLIGHT CRADLE BROKEN BEHIND CAPTAINS SEAT. R & R FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.SDR SIMA20151108003Door Sill · corrodedCARGO DOOR SILL HAS AREAS OF CORROSION. R & R THE CARGO DOOR SILL IAW SRM 51-40-02.SDR SIMA20151108002Inverter · inoperativeFORWARD EMER LIGHT EXIT SIGN INOPERATIVE. R & R NR 1 INVERTER. OPERATIONS CHECKED GOOD IAW AMM 33-50-11.SDR SIMA20151108001Target · out of adjustAFTER TAKEOFF & AFTER LG AIR & GND FAIL MSG RECEIVED, THRUST 1 - 2 REVERSER DISAGREE CAUTION MSG ON EICAS. AFTER LANDING MSG WENT AWAY, FOUND MSG RELATED TO AFOREMENTIONED NLG WOW SWITCH TARGET ADJUSTMENT, REF THIS AML PAGE ITEM 1. MSG NO LONGER IN VIEW AFTESDR SIMA20151107002Skin · crackedLEFT UPPER FUSELAGE SKIN CRACKED AT FRAME 75, JUST ABOVE STRINGER 2L. REPAIRED CRACK AT FRAME 75, JUST ABOVE STRINGER 2L IN LT FUSELAGE SKIN IAW ERS-EM-53MR-1800.SDR SIMA20151107003Skin · crackedRIGHT UPPER FUSELAGE SKIN CRACKED AFT OF FRAME 75, JUST ABOVE STRINGER 2R CRACK ENDS MARKED. REPAIRED FRAME 75 RT IAW ERS-EM-53MR-1799.SDR SIMA20151107001Firewall · crackedWHILE PERFORMING EO EM53AD-1883 PART B, FOUND ONE EACH .500 INCH CRACK ON THE APU FIREWALL AROUND THE J0274 ELEC CONNECTOR. COMPLIED WITH EO EM-53AD-1883 PART B.SDR UHLA201511070784Electronic Unit · failedDURING CLIMBOUT, THE CREW RECEIVED A LANDING GEAR DISAGREE MESSAGE WHEN RETRACTING THE GEAR AND THE GEAR CONTINUED TO INDICATE DOWN AND LOCKED. IAW THE QRH, THE CREW MADE AN UNEVENTFUL UNSCHEDULED LANDING AT THE FIELD OF DEPARTURE. MAINTENANCE R & R THE LANDSDR ASOA20151107190Fitting · crackedDURING C-CHECK, THE LT ENGINE FORWARD LOWER YOKE FITTING WAS FOUND TO BE CRACKED AND VERIFIED WITH EDDY CURRENT. MAINTENANCE R & R THE YOKE FITTING IAW EC5450-01182. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20151107189VFitting · crackedDURING C-CHECK, THE RT ENGINE LOWER FORWARD YOKE FITTING WAS FOUND TO BE CRACKED AND VERIFIED WITH EDDY CURRENT. MAINTENANCE R & R THE FITTING IAW EC5450-01182. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA20151106011Fitting · crackedFRAME CLIP CRACKED 1 INCH AT FRAME 68, STRINGER 6L. R & R SHEAR CLIP AT FRAME 68, STRINGER 6L IAW SRM 51-40-02.SDR SIMA20151106010Fitting · crackedFRAME CLIP CRACKED 1/2 INCH AT FRAME 67, STRINGER 6R. R & R CLIP AT FRAME 67, STRINGER 6R IAW SRM 51-40-02.SDR SIMA20151106008Support · crackedRIGHT OMEGA BEAM OTBD LT ANGLE SUPPORT IS CRACKED, BETWEEN FRAMES 47 & 48. REPAIRED IAW SRM 53-23-02. CHANNEL PN 140-04213-607.SDR SIMA20151106009Angle · crackedLEFT OMEGA BEAM LT ANGLE IS CRACKED, BETWEEN FRAMES 47 & 48. COMPLETED REPAIR OF LT OMEGA BEAM LT ANGLE IAW SRM 53-23-02. CHANNEL PN 140-04213-611, SHEAR CLIP PN 140-04214-605 & 140-04214-611.SDR SIMA20151106005Support · crackedRIGHT OMEGA BEAM INBD LT ANGLE SUPPORT IS CRACKED, BETWEEN FRAMES 47 & 48. REPAIRED IAW SRM 53-23-02. SHEAR CLIP PN 140-04213-609.SDR SIMA20151106007Support · crackedLEFT SIDE OVERWING FAIRING, UPPER SUPPORT IS CRACKED AFT OF FRAME 41 LOCATION. REPAIRED IAW SRM 53-2312.SDR SIMA20151106006Support · crackedRIGHT SIDE OVERWING FAIRING, UPPER SUPPORT IS CRACKED AFT OF FRAME 41 LOCATION. COMPLIED WITH REPAIR AT AFT OF FRAME 41 RT SIDE IAW SRM 53-23-12.SDR SIMA20151106003Fitting · crackedFRAME CLIP CRACKED 1/2 INCH AT FRAME 73, STRINGER 8L. REPLACED CLIP IAW SRM 51-40-02.SDR SIMA20151105005Light · crackedLEFT NR 2 EMER LIGHT STRIP EXTRUSION CRACKED. R & R LT NR 2 EMER LIGHT STRIP EXTRUSION IAW AMM 33-50-12. SEE BOW 205187 FOR OPERATIONS CHECK.SDR SIMA20151105004Door Sill · corrodedAFT CARGO DOOR SILL CORRODED. COMPLETED INSTALLATION OF CARGO DOOR SILL IAW SRM 51-40-02.
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