N141DU

Service difficulty reports · 19

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N141DU' AND registry_match = 'registration'
  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.

SDR DALA2025121009036Fuel Sys · out of balanceATB, DUE TO "FUEL IMBALANCE" AND "FMS FUEL" CAUTION MESSAGES. CORRECTIVE ACTION: RH AND LH EJECTOR PUMPS AND 90 ELBOW TUBES FOUND DAMAGED ALONG WITH ONE LH CHECK VALVE. ALL DAMAGED COMPONENTS REPLACED. R/R LH TRANSFER FLOAT SOV. A/C RTS. (LP# 7950252, 1335358,Dec 8, 2025 · N141DU · Airbus BD5001A10 · Fuel StorageSDR DALA2025092306959Light · sparksFIRST OFFICERS READING LIGHT HAS EXPOSED WIRES THAT CAUSED SPARKING DURING FLIGHT. PLACED ON MEL PER ERA 595933-14TR REV A, ERA APPROVED PER DAL P.S. 900-5-1 NO.4. ERA SECT. 1 C/W, PERMANENT REPAIR REQUIRED W/IN 10 DAYS. PLACARDS INSTALLED. RH MAP LT. CB LOCKESep 17, 2025 · N141DU · Airbus BD5001A10 · Flight Compartment LightingSDR DALA2025080505881Pinion Gear · corrodedLEFT PINION NR 4 TEETH, NR 1 & 2 HAD EVIDENCE OF CORROSION, LOWER SURFACE & PREVIOUS REWORK IAW ER/A 622578-14AD, REV A. LIAISON ENGINEERING REQUIRED BEFORE FURTHER FLIGHT . COMPLIED WITH ERA 622578-14AD, REV B, SEC 2, & 4. PRI 622578-14AD, REV 0 MATCHES.Jul 31, 2025 · N141DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2025070805080Controller · faultedSHIP 8141 - ATB - DUE TO ALL LAVATORIES NOT FLUSHING AT ALTITUDE. CORRECTIVE ACTION: REPLACED WASTE SYSTEM CONTROLLER. (LP# 7558246, 1058111, 7558248, 1061771, 7558256)Jul 2, 2025 · N141DU · Airbus BD5001A10 · Waste Disposal SystemSDR DALA2025050603480B-Nut · leakingODD UNEXPLAINED BURNING ODOR WHEN EXITING RUNWAY APU OFF. MEDIUM STRONG DISSIPATED AFTER TEN SECONDS. ODOR REOCCURRED AT GATE WITH APU ON, BEFORE ENGINE SHUTDOWN BURNING ODOR NOT DIRTY SOCKS. ACCOMPLISHED AMDS 0550-2001 FOR ODI SMOKE AND FUMES. REF LOG 0937218Apr 30, 2025 · N141DU · Airbus BD5001A10 · Turbine Engine Oil SystemSDR DALA2025050603469Slat Track · corrodedLH PINION #4 TOOTH #1 AND #2 HAS EVIDENCE OF CORROSION LWR PREVIOUS REWORK REF. 5742-01028-02A. LIAISON ENGINEERING REQUIRED BEFORE FURTHER FLIGHT. COMPLIED WITH ERA 622578-14AD REV A AND PRI 622578-14AD REV 0 MATCHES. (LP# 0940743)Apr 30, 2025 · N141DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2025050603468Slat Track · corrodedLH SLAT TRACK #4, RACK TOOTH #1 AND #2 HAS EVIDENCE OF CORROSION AFT PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING REQUIRED BEFORE FURTHER FLIGHT. COMPLIED WITH ERA 622578-14AD REV A AND PRI 622578-14AD REV O MATCHES. (LP# 0940739)Apr 30, 2025 · N141DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2025042403237Unknown · odorSHORT FINAL ALL 3 FAS AND MULTIPLE PAX NOTICED CHEMICAL/BURNING PLASTIC SMELL IN CABIN WE DIDN'T NOTICE ANY FUMES IN FLIGHT DECK UNTIL WE OPENED FLIGHT DECK DOOR. SMELL PERSISTED THROUGH DEPLANING FOR APPROX 20 MINS. WHILE PERFORMING NO GO ODI FOUND ACRID SMELApr 20, 2025 · N141DU · Airbus BD5001A10 · Air Distribution SystemSDR DALA2025042203166Charger · faultedAFTER LANDING DURING TAXI FA CALLED TO COMPLAIN ABOUT A BURNING PLASTIC SMELL. NOTHING WAS VISIBLE . WE SMELLED IT TOO. WE STOPPED THE A/C PUT THE MASK ON AND ESTABLISHED COMMUNICATION AND CONTINUED TO GATE. AFTER ENGINE SHUTDOWN SMELL WAS GONE. C/W NO GO ODI Apr 17, 2025 · N141DU · Airbus BD5001A10 · Emergency LightingSDR DALA2025040402600Unknown · odorRETURN TO GATE DUE TO INEXPLICABLE AND CONTINUOUS SMELL OF FOOD COOKING AND NO FOOD ON BOARD. RAN BOTH ENGINES PER A220 WORKCARD # 0550-2001. SMELL STRONGEST FROM #1 ENGINE AT ALL POWER SETTINGS. #2 ENGINE SMELL FROM HIGH POWER SETTINGS APPROX. ABOVE 45% N1. UApr 1, 2025 · N141DU · Airbus BD5001A10 · Air Distribution SystemSDR DALA2025040102435Fan · failed5 SECONDS OF INTENSE ELECTRICAL BURNING SMELL AND IMMEDIATE EQUIP BAY COOL FAULT - IFAN INOP. (SMELL ASSOCIATED WITH FAN FAIL) . REMOVED AND REPLACED MID BAY AVIONICS FAN REF A220 AMP 21-26. OPS CHK GOOD. MEL AND PLACARD REMOVED. (LP# 7230740)Mar 30, 2025 · N141DU · Airbus BD5001A10 · Air Distribution FanSDR DALA2025032502215Oil System · leakingSHIP 8141 -ATB- RETURNED TO SEA DUE TO ODOR IN THE CABIN AND FLIGHT DECK. CREW DID DON O2 MASKS AND IS DECLARING AN EMERGENCY. CORRECTIVE ACTION: MTC FOUND OIL WETTING ON NBR 2 ENGINE FAN EXIT GUIDE VANES. #2 ENGINE REPLACED. (LP# 7215788, 0870339)Mar 22, 2025 · N141DU · Airbus BD5001A10 · Turbine Engine Oil SystemSDR DALA2025010600111Waste Box · corrodedWASTE BOX HAS CORROSION. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0088:5360-2017/001 00166 COMPLIED WITH ER/A 623105-14 PRI REV 0, REV 1, REV 2 AND ER/A 623105-14 REV ORIGINAL. ALL PARTS WERE REPLACED SO NO MEASJan 1, 2025 · N141DU · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2025010600112Door · corrodedAFT PASSENGER DOOR HAS CORROSION AT HOLES 4OL, 7OL, AND 10OL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 060-0001:5331-01297- 02A/001 00260 REPAIRED PER ER/A 623091-14 PRI REV 0, PRI REV 1, AND ERA 623091-14 REV ORIGINAL, ORIGINAL THICKNESS IS .125 MAX MATERIALDec 31, 2024 · N141DU · Airbus BD5001A10 · Passenger/Crew DoorsSDR DALA2025010612132Skin · crackedLH WING - #8 SLAT TRACK CUTOUT HAS CRACK ON UPPER EDGE. "M". SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0307:2021-2065-LH/001 00131 REPAIRED PER ER/A 602000-14TR REV. C SECTION1'. (LP# 0737272)Dec 31, 2024 · N141DU · Airbus BD5001A10 · Wing, Plate/SkinSDR DALA2025010612131Skin · crackedRT WING #6 SLAT TRACK CUTOUT IS CRACKED. "M". SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0317:2021-2065-RH/001 00132 REPAIRED REF ER/A 601962-14TR REV A SECTION 1. (LP# 0737269)Dec 31, 2024 · N141DU · Airbus BD5001A10 · Wing, Plate/SkinSDR DALA2025010212125Door Sill · corrodedFWD LH PASSENGER DOOR-LOWER SILL CORROSION FOUND AT SCREW HOLE 1OL. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 057-0001:5331-01297-01A/001 00205 COMPLIED WITH ER/A 623087-14 PRI REV 0, ER/A 623087-14 PRI REV 1 AND FINDec 30, 2024 · N141DU · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2025100207158Scuff Plate · corrodedMID SCUFF PLATE #4 HAS CORROSION AROUND HOLES ON BACKSIDE OF PLATE (M)(P). ELAPSE TIME HRS: 0004.0 RII: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0239:2000-1001/006 00234 REMOVED AND REPLACED SCUFF PLATE PER A220 ASRP 51-41-00. (LP# 0733686)Dec 28, 2024 · N141DU · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2022121908200Longeron · crackedWORKING A220 JIC AD RELATED 5352-01038-01B FOUND CRACK ON RIGHT LONGERON AT RBL 40.0 APPROX 8IN. R/R RIGHT LONGERON AT RBL 40.0 AND ALL AD TASKS ACCOMPLISHED IAW AMDS W/C 5352-01038-05B. (LP# 9637648)Dec 16, 2022 · N141DU · Bombdr BD1001A10 · Fuselage Structure (General)
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