N121DU

Service difficulty reports · 68

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 = 'N121DU' 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 DALA2024021302091Slat Track · corrodedLH SLAT TRACK NBR 2 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 2 UPPER AFT SURFACE IAW ER/A 608710- 14AD REV B AND PRI 608710-14AD REV 0 MATCHED. (LP# 0196205)Feb 10, 2024 · N121DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024021302090Slat Track · corrodedLH SLAT TRACK NBR 1 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 1 UPPER AFT SURFACE IAW ER/A 608710- 14AD REV B AND PRI 608710-14AD REV 0 MATCHED. (LP# 0196202)Feb 10, 2024 · N121DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024012401095Longeron · crackedWHILE PERFORIMING W/C 5352-01038-01A WTBF INSP FOUND APPROX 3 INCH CRACK IN LEFT LONGERON ON BOTTOM FLANGE. AD RELATED. REMOVED 2 EA O/B FILLET PANELS L/H SIDE.(309252) REMOVED AND BEGAN DRILLING LONGERON PER WORKCARD 5352-01038-07A (373696) LONGERON SOFT MOUNJan 24, 2024 · N121DU · Airbus BD5001A10 · Aerodynamic FairingsSDR DALA2023121110111Unknown · unknownBIRD STRIKE DAMAGE COMMON TO THE RHS OF THE NOSE FUSELAGE ABOVE THE AFT SKIN STRINGER AND BETWEEN FR13-FR14. TWO DENTS ARE PRESENT FWD OF FR13 AND FR14. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0005:2000-2100/00Dec 10, 2023 · N121DU · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2024120511473Skin · damagedERA 614059-14 ISSUED FOR BIRD STRIKE REPAIR TO FWD RH FUSELAGE S KIN FR13-14. DAMAGE TOLERANCE EVALUATION IS REQUIRED. ERA 614059-14 ISSUED AND IS LIMITED TO 12MONTHS AFTER SECTION I. SECTION I ACCOMPLISHED IN MSP 07DEC23. OPERATION BEYOND 12 MONTHS REQUIRES ADec 7, 2023 · N121DU · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2023083007065Unknown · unknownDUE TO CHECK VALVE MISSING PARTS ON NR 29, REPORT FINDING TO PRATT AND WHITNEY, BASED ON THE RESULTS, ADDITIONAL INSPECTIONS MAY NEED TO BE COMPLETED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 025-0001:2820-01281-07AAug 25, 2023 · N121DU · Airbus BD5001A10 · Fuel StorageSDR DALA2023020801007None · noneDURING DEPARTURE AND DECENT SMELLED A "DIRTY SOCK" SMELL. ON #1 ENG FOR BOROSCOPE 607080 JB. PERFORMED BOROSCOPE OF #3 BEARING PER B500-A-372-34-00 AND HPC PER BD500-A-372-00-00. FOUND WETTING ON VANE BETWEEN #1 AND #2 HPC BLADES. PICTS SENT TO PROP OPS. QC510Feb 7, 2023 · N121DU · Airbus A300* · Engine Oil System (Airframe Furnished)SDR DALA2023012400595Autoland Sys · faultedDIVERSION DUE TO LOSS OF CATEGORY 3 AUTOLAND WITH WEATHER IN SEA. REENABLED SOFTWARE ENCRYPTED APPLICATION KEYS AND RTS.Jan 21, 2023 · N121DU · Airbus BD5001A10 · Auto Flight SystemSDR DALA2022102606960None · noneSHIP 8121 - FUMES/MISC - STRONG ELECTRICAL SMELL ON APPROACH. CORRECTIVE ACTION: FOUND VAPE LEAKING OIL ON IN SEAT POWER SUPPLY (ISPS). DISPATCHED PER ERA WITH ISPS DISCONNECTED AND CAPPED. (LP# 9706566)Oct 22, 2022 · N121DU · Airbus BD5001A10 · Air Conditioning SystemSDR DALA2022080905438None · noneREMOVE AND REPLACE WASTE BOX PAN REF A220 ABC DWG C01342100 REV - W AND ABC DWG C011342957 REV - E. ER/A 601047-14 REV ORIGINAL. PRI 601047-14 REV 0,1,2,3,4,5. REMOVED AND REPLACED WASTE BOX PAN REF A220 ABC DWG C01342100 REV - W AND ABC DWG C011342957 REV - EAug 5, 2022 · N121DU · Airbus BD5001A10 · Fuselage Internal Mounting StructureSDR DALA2022080905437None · noneREMOVE AND REPLACE WASTE BOX PAN REF A220 ABC DWG C01342100 REV - W AND ABC DWG C011342957 REV - E. ER/A 601047-14 REV ORIGINAL. REMOVED AND REPLACED WASTE BOX PAN REF A220 ABC DWG C01342100 REV - W AND ABC DWG C011342957 REV - E. ER/A 601047-14 REV ORIGINAL. Aug 5, 2022 · N121DU · Airbus BD5001A10 · Fuselage Internal Mounting StructureSDR DALA2022080905439None · noneACCOMPLISH PRI 601047-14 REV 0, REV 1, REV 2, REV 3, REV 4, REV 5 AND ER/A 601047-14AD REV ORIGINAL. DUE TO LAV SERVICE PANEL CORROSION. ACCOMPLISHED PRI 601047-14 REV 0, REV 1, REV 2, REV 3, REV 4, REV 5 AND ER/A 601047-14AD REV ORIGINAL. SEE EMPOWER WORKORDEAug 4, 2022 · N121DU · Airbus BD5001A10 · Fuselage Internal Mounting StructureSDR DALA2022080505376None · noneERA 601047-14AD SECTION I ACCOMPLISHED IN MSP DURING C CHECK.FO LLOW ON ACTION IS REQUIRED. ACCOMPLISH ERA 601047-14AD SECTION II EVERY 850 FH AFTER SECTION I UNTIL SECTION III. SECTION I REPAIR IS TIME LIMITED TO 8500 F H. THIS RESTRICTION IS TRACKED PER SECTAug 3, 2022 · N121DU · Airbus BD5001A10 · Fuselage Internal Mounting StructureSDR DALA2022072805209Air Duct · damagedFWD LEFT RAM AIR DUCT HAS INTERNAL DAMAGE-EXPOSED FIBERS. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0228:2157-2001/001 00204 REPAIRED PER ERA 583836-14TR. ADDITIONAL INFOR MATION 001-0228:2157-2001/001 00204 REPAJul 26, 2022 · N121DU · Airbus BD5001A10 · Cabin Cooling SystemSDR DALA2022072605133Pressure Sensor · failedLH/IB MLG TIRE PRESSURE MODULE FAILS PER AMDS WORKCARD 3247-2001. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0072:3247-2001/001 00226 REMOVED AND REPLACED LH INBOARD MLG TIRE PRESSURE MODULE REF. A220 AMP 32-47 -1Jul 22, 2022 · N121DU · Airbus BD5001A10 · Landing Gear Brake SystemSDR DALA2021120507479None · noneRAMP REPORTED DAMAGE TO FWD CARGO DOOR AFT LOWER CORNER. FOUND TWO GOUGES TO LOWER AFT CORNER EDGE OF FWD CARGO DOOR. PERFORMED REPAIR PER ERA 593924-14 REV ORIGINAL. DEFERRED TO MON FOR PERMANENT REPAIR. ER/A PERMANENT REPAIR INSTRUCTIONS MUST BE ACCOMPLISHEDDec 1, 2021 · N121DU · Airbus BD5001A10 · Cargo/Baggage DoorsSDR DALA2021101906442None · noneON WALK AROUND FOUND BUBBLING PAINT ON VERT STABILIZER ON RIGHT HAND SIDE. C/W INSPECTION OF VERTICAL STABILIZER PAINT DAMAGE IAW A220 ASRP 55-31. FOUND AREAS OF EXPOSED COMPOSITE. C/W TEMPORARY REPAIR W / SPEED TAPE PER ASRP 51-27. RESTORATION DEFERRED FOR MAOct 15, 2021 · N121DU · Airbus BD5001A10 · Vertical Stabilizer, Plate/SkinSDR DALA2020020700972Warning Message · false activationMASTER CAUTION: FUEL LEAK SUSPECT AT FL390 COMPLIED WITH CHECKLIST, DIVERTED TO KTYS. R ENG FUEL LEAK DETECTED/REPORTED BY R EEC CH A OR B. RAN ENG & PERFORMED GVI. NO LEAKS NOTED. SUSPECT INT. FAULT MAY HAVE BEEN GENERATED BY FUEL FLOW XMTR ON MEL, REF A/C LOFeb 5, 2020 · N121DU · Airbus BD5001A10 · Engine Fuel Indicating System
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