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 SIMA20140520001Flashlight · inoperativeDURING FLIGHT 3514 FOUND CABIN COMPARTMENT AFT FLASHLIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. CORRECTIVE ACTION R & R CABIN COMPARTMENT AFT FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.SDR SIMA20140520003Battery · dischargedAFT CABIN EMERGENCY FLASHLIGHT WILL NOT HOLD CHARGE. R & R FLASHLIGHT BATTERY IAW CMM 25-60-02. OPERATIONS CHECKED GOOD.SDR ASOA20140520088VNut Plate · corrodedDURING C-CHECK, CORROSION AROUND TWO NUTPLATES ON CENTER OMEGA BEAM GUSSET , Y-0.0, BETWEEN FRAMES 14 AND 18 AS MARKED IN CENTER FUSELAGE I. MAINTENANCE R & R GUSSETT AND 3 EA DOUBLERS ON FWD CENTER BEAM NR FRAME 14 IAW SRM 51-40-02, APPLIED PRIMER AND TOPCOASDR ASOA20140520087Threshold · corrodedDURING C-CHECK, CARGO DOOR THRESHOLD HAS CORROSION, AT NUTPLATES HOLES. R & R CARGO DOOR THRESHOLD IAW SRM 51-40-02 AND CPM 51-21-04. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA20140519005Light · missingEMERGENCY FLOOR PROXIMITY LIGHTING STRIP AT ROWS 17 & 18 DISCOVERED TO BE NOT ON ACFT. LOCATION UNKNOWN. DISCOVERED LOCATION OF ROW 17 & 18 EMERGENCY FLOOR PROXIMITY LIGHTING STRIP. INSTALLED EMERGENCY LIGHTING STRIP IAW AMM 33-50-12. OPERATIONAL CHECK GOODSDR SIMA20140519004Floor Support · corrodedDURING MBV INSPECTION, QA FOUND LT OMEGA BEAM CORRODED AROUND NUTPLATE HOLE ON LOWER FLANGE BETWEEN FRAME 22 & 23. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. PERFORMED PERMANENT REPAIR ON LT OMEGA BEASDR SIMA20140519003Flashlight · inoperativeFORWARD CABIN EMERGENCY FLASHLIGHT INOPERATIVE. R & R FWD CABIN EMERGENCY FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.SDR ASOA20140519086Connector · dirtyACFT HAD MULTIPLE EICIAC MESSAGES THAT THE E2 FIRE DETECT FAIL. ACFT LANDED WITHOUT ISSUE AND MAINTENANCE REMOVED AND REINSTALLED FIRE DETECT PANEL TO FACILITATE CLEANING IAW AMM 26-00-01. REMOVED AND REINSTALLED ENGINE 2 FIRE DETECT CONNECTOR FOR CLEANING ISDR RAIA201405180001Bulb · inoperativeCEILING EMERGENCY EXIT LIGHTS ARE INOP AT ROWS 18 AND 23. MAINTENANCE REPLACED BULBS AND OPS CHECKED GOOD.SDR CHQA20140518150Flap · malfunctionedDURING APPROACH, THE FLIGHT CREW RECEIVED A FLAP FAIL MSG ON THE EICAS DISPLAY. AFTER RUNNING THE CHECKLIST IN THE QRH, AN EMERGENCY WAS DECLARED & A SUCCESSFUL LANDING WAS COMPLETED. RESET THE FLAP SYS & THE MSG CLEARED. NO FURTHER DEFECTS HAVE BEEN NOTED.SDR CHQA20140518151Battery · dischargedDURING INSPECTION, THE OVERHEAD MAIN ENTRY DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE NR 1 EMERGENCY LIGHT BATTERY & ALL OPERATIONAL CHECKED GOOD.SDR ASOA20140518042Brake Assy · wornTHE CREW REPORTED BRAKES COULD NOT BE APPLIED FULL, GRAB HARD AND RELEASE AND PULL LEFT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 BRAKE ASSEMBLY. OPS CHECKED GOOD.SDR ASOA20140518056Brake Sys · malfunctionedPILOT REPORTED BRAKES SURGED DURING LANDING ROLLOUT. MAINTENANCE PERFORMED TAXI AND FUNCTIONAL CHECK OF MAIN BRAKE SYSTEM WITH NO DEFECT NOTED AND OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA20140517011Skin · corrodedEVIDENCE OF CORROSION ON THE INNER SKIN BETWEEN FRAMES 13 & 14 & STRINGERS 20L & 18L, PAINT BUBBLING. BLENDED OUT CORROSION ON INNER SKIN BETWEEN FRAMES 13 & 14 & STRINGERS 21L - 18L IAW SRM 51-10-03 ERS-EM-5300-491 ACCEPTED AS IS. SEE TASK 2 FOR PAINT RESTOSDR SIMA20140517012Door · corrodedCARGO DOOR, NUMEROUS NUTPLATE HOLES, TOP, SIDES, BOTTOM & INTERNAL HAVE CORROSION. REPAIRED MARKED CORRODED NUTPLATE HOLES ON TOP, SIDES, BOTTOM & INTERNAL ON CARGO DOOR IAW ERS-EM-5200-146. SEE TURNOVER FOR DETAILS.SDR SIMA20140517013Structure · corrodedLEFT WINDSHIELD INNER MOUNTING SURFACE CORRODED ON LOWER OTBD SURFACE. BLENDED AS REQUIRED TO REMOVE CORROSION FROM LT WINDSHIELD INNER MOUNTING SURFACE ON LOWER OTBD CORNER IAW SRM 51-10-03 & ACCEPTED AS IS IAW ERS 5600-033.SDR SIMA20140517015Tab · looseBOTH PRESS TABS ON POTABLE WATER SERVICE DOOR ARE LOOSE & HAVE SPINNING OR CORRODED FERRELL’S. PREPPED & APPLIED FILLER & INSTALLED FOUR INSERTS FOR BOTH PRESS TABS ON INSIDE OF POTABLE WATER SERVICE DOOR IAW ERS-EM-5200-157. FLUKE 7569 & GAUGE 3337.SDR SIMA20140517014Frame · corrodedCORROSION FOUND AROUND ALL NUTPLATE HOLES ON THE ABOVE FLOOR SECTION OF FRAMES 65 & 68. BLENDED DAMAGED AREA ON ALL NUTPLATE HOLES ABOVE FLOOR ON FRAMES 65 & 68 IAW SRM 51-10-03. ACCEPTED AS IS IAW ERS-EM-5300-483. SEE WIP & TASK FOR DETAILS.SDR SIMA20140517010Frame · corrodedLEFT ENG HAS CORROSION ALONG THE LOWER SURFACE BETWEEN THE CONTAINMENT RING & THE FWD FRAME, ABOVE THE GENERATORS. REMOVED LT ENG CORROSION FROM ALONG THE LOWER FRONT FRAME FWD FLANGE, ABOVE THE GENERATORS IAW RRMM 72-25-45-300-805 & 70-00-00-300-805, APPLIEDSDR SIMA20140517009Support · corrodedRIGHT AILERON TORQUE TUBE SUPPORT CORRODED AROUND FASTENER. BLEND AREA ON RT AILERON TORQUE TUBE SUPPORT ACCEPTED AS IS IAW ERS-EM-5300-485. SEE WIP & TASK ENTRIES FOR DETAILS.SDR SIMA20140517005Reinforcement · crackedFORWARD TO AFT DIGITAL SPLICE REINFORCEMENT CRACKED AT LT FLOORBEAM BETWEEN FRAME 16 & 17. REMOVED CRACKED REINFORCEMENT & INSTALLED SERVICEABLE REINFORCEMENT AT LT FLOORBEAM BETWEEN FRAME 16 & 17 IAW SRM 51-40-02.SDR SIMA20140517006Floor Support · corrodedFORWARD DIGITAL CORRODED AT NUTPLATE AT PAX DOOR ENTRANCE AT FRAME 15. REPAIRED FWD DIGITAL AT PAX DOOR ENTRANCE AT FRAME 15 IAW ERS-EM-5300-488.SDR SIMA20140517007Trim Panel · crackedFOUR EACH RT FLOOR TRIM EXTRUSIONS CRACKED. R & R FOUR EACH RT FLOOR TRIM EXTRUSIONS IAW AMM 33-50-12.SDR SIMA20140517008Light · inoperativeSERVICE DOOR EMER LIGHT INOPERATIVE. R & R SERVICE DOOR EMER LIGHT BULB IAW AMM 33-50-10 & OPERATIONS CHECKED GOOD.SDR SIMA20140517004Holder · failedBATTERY HOLDER ASSEMBLY FAILED CHECKS. R & R BATTERY HOLDER ASSEMBLY.SDR SIMA20140517001Battery · dischargedFIRST OFFICER'S FLASHLIGHT DOESN'T HOLD CHARGE. REMOVED & INSTALLED BATTERY ON FIRST OFFICER`S FLASHLIGHT IAW AMM 25-60-00.SDR SIMA20140517002Roller · dirtyFLIGHT ATTENDANT REPORTS MAIN CABIN DOOR VERY DIFFICULT TO OPEN. LUBRICATED DOOR ROLLERS & PERFORMED OPERATIONS CHECK OF CABIN DOOR IAW AMM 52-18-00. OPERATIONS CHECKED OK.SDR SIMA20140517003Inverter · inoperativeFLOOR EMERGENCY LIGHT SECTIONS 4 & 5, WING EMERGENCY EXIT SIGNS INOPERATIVE. R & R NR 5 EMERGENCY LIGHT INVERTER IAW AMM 33-50-11 & NR 3 BATTERY PACK & CHARGER IAW AMM 33-50-04. OPERATIONS CHECKED OK PN 11-0049 & SN 20100.SDR ASOA20140517086VFloor Support · corrodedDURING C-CHECK, RT FLOOR SUPPORT AT FRAME 53 HAS CORROSION. MAINTENANCE R & R RT FLOOR SUPPORT IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140517085VFloor Support · corrodedDURING C-CHECK, CORROSION AROUND NUTPLATE ON CENTER OMEGA BEAM, Y=0.0, GUSSET AT FRAME 20. MAINTENANCE BLENDED CORROSION AROUND NUTPLATE ON CENTER OMEGA BEAM GUSSET AT FRAME 20, MATERIAL LOSS IS WITHIN LIMITS IAW SRM 53-21-10. PREPPED, ALODINED, PRIMED AND TSDR ASOA20140517084Floor Support · corrodedDURING C-CHECK RT FLOOR SILL IN CARGO AREA FRAMES 61-63 IS CORRODED. MAINTENANCE R & R FLOOR SILL AND SPLICE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140517083Floor Support · corrodedDURING C-CHECK, CORROSION AROUND NUTPLATE BOTH NUTPLATES ON GUSSETT AT RT OMEGA BEAM, Y+479.0, FRAME 22. MAINTENANCE DETERMINED CORROSION AROUND NUTPLATE HAS 100 PERCENT MATERIAL LOSS, R & R RT GUSSETT IAW SRM 41-40-02. THE ACFT WAS APPROVED FOR RETURN TO SESDR ASOA20140517082Floor Support · corrodedDURING C-CHECK, FOUND CORROSION AROUND NUTPLATE ON GUSSETT RT OMEGA BEAM, Y=479.0, FRAME 20. MAINTENANCE DETERMINED CORROSION AROUND NUTPLATE IN GUSSETT IS 100 PERCENT MATERIAL LOSS, R & R RT GUSSETT IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERSDR ASOA20140517081Floor Support · corrodedDURING C-CHECK LAVATORY UNDER FLOOR OMEGA BEAM CAP IS CORRODED, LOCAL LEVEL 2, AS MARKED ON RT SIDE AROUND NUTPLATE. MAINTENANCE BLENDED CORROSION AROUND NUTPLATE 100 NR MATERIAL LOSS, R & R OMEGA BEAM CAP IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TSDR ASOA20140517076Beam · corrodedDURING C-CHECK THE LT WINDSHIELD LOWER FRONT CUTOUT BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED BUSHING REPAIRS IAW EC5310-01782. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140517080VFirewall · crackedDURING C-CHECK, THE APU FIREWALL WAS FOUND TO BE CRACKED INBD OF STRINGER 12L WHERE THE APU CONTROL HARNESS CONNECTS. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW SRM 53-32-10. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140517079VFloorbeam · corrodedDURING C-CHECK THE CENTER AISLE CROSSBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140517078Shear Tie · corrodedDURING C-CHECK THE FRAME 65 SHEAR CLIP WAS FOUND TO BE CORRODED BETWEEN STRINGERS 15-16L. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A SPLICE REPAIR IAW SRM 53-31-04. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140517077Frame · corrodedDURING C-CHECK, FRAME 65 WAS FOUND TO BE CORRODED BETWEEN STRINGERS 16-17L. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-31-04. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140517075Flange · crackedDURING C-CHECK, THE RUDDER II UPPER ATTACHMENT POINT NUTPLATE FLANGE WAS FOUND TO BE CRACKED. MAINTENANCE R & R THE FLANGE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140516074Bearing Cap · corrodedDURING C-CHECK CORROSION FOUND ON LT AND RT NLG BEARING CAPS. MAINTENANCE REPLACED LT AND RT NLG BEARING CAPS AND SHIMMED IAW AMM 32-20-01, FOR INSTALLATION SEE W04249, TASK 7021. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140516073Partition · corrodedDURING C-CHECK CORROSION ON RT WALL DOUBLER AT FRAME 61 AT FLOOR LEVEL. MAINTENANCE DETERMINED CORROSION 100 PERCENT MATERIAL LOSS, REMOVED WALL DOUBLER, LOCATED, DRILLED, ALODINED AND INSTALLED NEW RT WALL DOUBLER AT FRAME 61 IAW SRM 51-20-03 AND SRM 51-40-0SDR ASOA20140516072Floor Support · corrodedDURING C-CHECK LAVATORY UNDER FLOOR OMEGA BEAM CAP IS CORRODED AS MARKED ON LT SIDE AROUND NUT PLATE. MAINTENANCE DETERMINED CORROSION ON OMEGA BEAM CAP LT SIDE FRAMES 59-61 IS 100 PERCENT MATERIAL LOSS IAW SRM 53-24-10. MAINTENANCE R & R LT GUSSET IAW SRM 5SDR ASOA20140516071Floor Support · corrodedDURING C-CHECK, CARGO UNDERFLOOR SUPPORT 65-68 LT SIDE UNDER FLOORBOARD 271FF HAS CORROSION. MAINTENANCE R & R FLOOR SUPPORT IAW SRM 51-40-02 AND 53-31-10. ACFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20140516070VPartition · damagedDURING C-CHECK, BOTH SHOT BOLT HOLES FOR LT COCKPIT PARTION ARE ELONGATED. MAINTENANCE REMOVED CHAFED UPPER PIN GUIDE FABRICATED, LOCATED AND DRILLED UPPER PIN GUIDE DOUBLER IAW EC5320-017018. INSTALLED AND TOP COATED UPPER AND LOWER PIN GUIDES IAW EC5320-0SDR ASOA20140516069Stringer · crackedDURING C-CHECK, STRINGER 3L AT FRAME 20 IS CRACKED. MAINTENANCE R & R STRINGER IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20140516068Access Panel · corrodedDURING C-CHECK RT WING ACCESS PANEL 532AB FOUND CORRODED ON BACKSIDE AROUND FASTENER HOLES. MAINTENANCE BLENDED CORROSION AND REMAINED WITHIN ALLOWABLE LIMITS IAW EC5720-01178. ACFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20140516067Access Panel · corrodedDURING C-CHECK, RT WING ACCESS PANEL 632AB FOUND CORRODED ON BACKSIDE AROUND FASTENER HOLES. MAINTENANCE BLENDED CORROSION. REMAINED WITHIN ALLOWABLE LIMITS IAW EC5720-01178. ACFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20140516066VFrame · brokenDURING C-CHECK, FRAME 10 BENEATH CO-PILOT'S DV WINDOW BROKEN. MAINTENANCE REMOVED BROKEN FRAME 10, LOCATED, DRILLED, ALODINED, AND INSTALLED NEW FRAME 10 IAW SRM 51-20-03, 51-40-03 AND CPM 51-14-05. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140516065Frame · brokenFRAME 10 BENEATH PILOT'S DV WINDOW BROKEN. MAINTENANCE REMOVED BROKEN FRAME 10, LOCATED, DRILLED, ALODINED AND INSTALLED NEW FRAME 10 IAW SRM 53-00-04, 51-40-02, AND CPM 51-21-04. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
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