N140DU

Service difficulty reports · 28

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 = 'N140DU' 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 DALA2026102105793Door Frame · corrodedCORROSION AT FASTENER HOLE 12IN FWD FROM AFT CARGO DOOR AFT FRAME. C/W ER/A 637319-14 REV ORIGINAL, SILL REPLACED ON CC 00241 ASSOCIATED ER/A 14-637319. (LP# 1874278; AIRCRAFT WAS GROUNDED)Oct 19, 2026 · N140DU · Airbus BD5001A10 · Fuselage Main, StructureSDR DALA2026102105792Door Frame · corrodedCORROSION AT FASTENER HOLE 12IN AFT FROM AFT CARGO DOOR FWD FRAME. C/W ER/A 637319-14 REV ORIGINAL, SILL REPLACED ON CC 00241 ASSOCIATED ER/A 14-637319. (LP# 1874275; AIRCRAFT WAS GROUNDED)Oct 19, 2026 · N140DU · Airbus BD5001A10 · Fuselage Main, StructureSDR DALA2026102105791Door Frame · corrodedCORROSION AT FASTENER HOLE 7IN AFT FROM AFT CARGO DOOR FWD FRAME. C/W ER/A 637319-14 REV ORIGINAL, SILL REPLACED ON CC 00241 ASSOCIATED ER/A 14-637319 (LP# 1874271; AIRCRAFT WAS GROUNDED)Oct 19, 2026 · N140DU · Airbus BD5001A10 · Fuselage Main, StructureSDR DALA2026102105790Door Frame · corrodedCORROSION AT FASTENER HOLE 7IN FWD FROM AFT CARGO DOOR AFT FRAME. C/W ER/A 637319-14 REV ORIGINAL ASSOCIATED ER/A 14-637319 A. (LP# 1874267; AIRCRAFT WAS GROUNDED)Oct 19, 2026 · N140DU · Airbus BD5001A10 · Fuselage Main, StructureSDR DALA2026101905729Seat Track · corrodedCORROSION FOUND ON SEAT TRACK FORWARD OF FRAME 22 APPROXIMATELY 3 INCHES AT RBL 43.50. REMOVED AND REPLACED SEAT TRACK AT FR 20 TO FR 30 RBL 43.50 PER A220 ASRP BD500-A-J51-42-21-00AAA-078A-A AND BOMBARDIER DWG: C02312600 REV: K. (LP# 1868113; AIRCRAFT WAS GROOct 15, 2026 · N140DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026101405649Web · corrodedCORROSION FOUND ON WEB, APPROXIMATELY 6 INCHES AFT OF AFT PAX DOOR CUT OUT. FLOOR LEVEL APPROX LBL 50. R & R THE FLOOR WEB FROM FR 76 - 79, LBL 50 IAW ASRP BD500-A-J51-42-06-00AAA-078A-A, & DWG C01342700, REV T. (LP# 1855384; AIRCRAFT WAS GROUNDED)Oct 8, 2026 · N140DU · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2026100705543Seat Track · corrodedCORROSION FOUND ON SEAT TRACK AFT OF FRAME 74 APPROXIMATELY 2 INCHES AT RBL 23.00. REMOVED AND REPLACED SEAT TRACK AT FRAME 61 TO FR 74 RBL 23 I.A.W. DWG# BOMBARDIER PL C01342701 REV-G AND A220 ASRP BD500- A-J51-42-20-00AAA-078A-A. (LP# 1851958; AIRCRAFT WAS GOct 6, 2026 · N140DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026100705540Seat Track · corrodedCORROSION FOUND ON SEAT TRACK FORWARD OF FRAME 22 APPROXIMATELY 3 INCHES AT RBL 23.00. REMOVED AND REPLACED SEAT TRACK RBL 23 FR20-FR30 IAW A220 ASRP BD500-A-J51-42-20-00AAA-078A-A AN BOMBARDIER DWG# PL C02312600 REV-K. (LP# 1849440; AIRCRAFT WAS GROUNDED)Oct 5, 2026 · N140DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025071405287Light · inoperativeFORWARD PASSENGER DOOR OVERHEAD EMERGENCY LIGHT FOUND INOP DURING SERVICE CHECK. REMOVED FPD SURROUND STEPS 1A & 1B IAW A220 AMP 25-29-13. REMOVED AND REPLACED FPD OVERHEAD EMERGENCY LIGHT IAW A220 AMP 33-52-02. RE-INSTALLED FPD SURROUND IAW AMP 25-29-13. OPJul 8, 2025 · N140DU · Airbus BD5001A10 · Emergency LightingSDR DALA2025050603478Unknown · odorAFTER LANDING F/A SAYS STRONG BURNING SMELL IN AFT GALLEY. LEAD F/A SAYS LIGHT SMELL IN FRONT GALLEY. C/W ODI CHECK LIST IAW A220 AMDS WORKCARD 0550-2001. NO ODORS NOTED. OK FOR SVC. (LP# 7505920)May 2, 2025 · N140DU · Airbus BD5001A10 · Air Distribution SystemSDR DALA2024121711795Door Sill · corrodedFWD CARGO DOOR OPENING LOWER SILL CORRODED BEYOND LIMITS. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 057-0001:5331-01297-01C/009 00290 REPLACED LOWER DOOR SILL PER ER/A 622870-14 PRI REV 0 AND FINAL ER/A 622870-14 REV ORIGINAL. (LP# 0707685)Dec 13, 2024 · N140DU · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2024121711794Waste Box · corrodedWASTE BOX, CORROSION FOUND ON FWD EDGE OF EXTERIOR SKIN IN 2 PLACES, PHOTOS ATTACHED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0255:2021-2025/002 00087 COMPLIED WITH PRI 622663-14 REV 0, REV 1, REV 2 REV 3, REV 4 AND ER/A 622663-14 REV ORIGINAL. (LP# 0705Dec 12, 2024 · N140DU · Airbus BD5001A10 · Fuselage Main, StructureSDR DALA2024121711793Seat Track · corrodedSEAT TRACK RBL 43.5 CORRODED AFT OF LAV D4. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0005:2500-2647/088 00116 REPAIRED PER PRI 622771-14 REV 0 AND 1 AND ER/A 622771-14 REV ORIGINAL. (LP# 0705347)Dec 11, 2024 · N140DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2024121711792Seat Track · corrodedSEAT TRACK LBL 43.5 CORRODED AFT OF LAV C2. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0005:2500-2647/087 00115 REPAIRED PER PRI 622772-14 REV 0 AND 1 AND ER/A 622772-14 REV ORIGINAL CLOSING REQUIREMENTS RII: INSPECTOR 00965021. (LP# 0705217)Dec 11, 2024 · N140DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2024120511471Strip · deterioratedVERTICAL STAB - BOTH SIDES HAVE THE UPPERMOST (4EA RUNNING FORE AND AFT) LIGHTNING STRIPS DETERIORATING. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0280:2021-2059/003 00099 REPAIRED LIGHTNING DIVERTER STRIPS IAW ADec 2, 2024 · N140DU · Airbus BD5001A10 · Vertical Stabilizer, Plate/SkinSDR DALA2024120511470Slat Track · damagedCOMPLETE NDT OF LH SLAT TRACK 11 BLENDED AREAS AS NECESSARY PER AMDS 5742-01028-02A STEP 10 AND 11. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 154-0001:5742-01028-02A/003 00252 COMPLETED NDT OF BLENDED AREAS ON LH SLANov 29, 2024 · N140DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024120511469Slat Track · scratchedCOMPLETE NDT OF LH SLAT TRACK 7 BLENDED AREAS AS NECESSARY PER AMDS 5742-01028-02A STEP 10 AND 11. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 154-0001:5742-01028-02A/002 00251 COMPLETED NDT OF BLENDED AREAS ON LH SLATNov 29, 2024 · N140DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2023091807654Unknown · unknownON TAKE-OFF FROM ORD, NOTICE MUSTY SOCK SMELL FOR SEVERAL MINUTES. C/W WORKCARD 0550-2001 ISOLATE SMOKE + FUMES IN COCKPIT/CABIN UP TO STEP#4. FOUND HYDRALIC LEAK ON RT SIDE OF THE WING TO THE BODY FAIRING. REMOVED PANEL 192BB AND FOUND SLAT ANGLE GEARBOX LEAKSep 16, 2023 · N140DU · Bombdr BD1001A10 · Leading Edge Slat ActuatorSDR DALA2023090107136Unknown · unknownBURNING ELECTRICAL ODOR AFTER LANDING BOS. SIMILAR TO APU STARTUP SMELL BUT STRONGER. ASKED MAINT TO INSPECT. NO OTHER INDICATIONS. PERF JOB CARD 0550-2001 SMOKE AND FUME ISOLATION ITEMS 1 THROUGH 8. PERF RUN AIR QUALITY FAULT ISOLATION ITEM 13. NO SIGN OF FUMAug 31, 2023 · N140DU · Bombdr BD1001A10 · Air Distribution SystemSDR DALA2023060104398Unknown · unknownSHIP 8140 - DIV - TO ABQ DUE TO "EQUIP BAY SMOKE FAIL" CAUTION MESSAGE. CORRECTIVE ACTION: REPLACED BOTH EQUIPMENT BAY SMOKE DETECTORS. (LP# 9736464)May 25, 2023 · N140DU · Bombdr BD1001A10 · Fire Protection SystemSDR DALA2023042603264Unknown · unknownERA 608151-14AD SECTION I ACCOMPLISHED IN MSP DURING SPECIAL VISIT. FOLLOW ON ACTION IS REQUIRED. LH WING SLAT TRACKS 2, 4-10 ARE AFFECTED. ACCOMPLISH ERA 608151-14AD SECTION II EVERY 850 FH AFTER SECTION I.ERA 608151-14AD SECTION IIS TIME LIMITED TO 8500 FH. Apr 20, 2023 · N140DU · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2023041102852Unknown · unknownSHIP 8140 -ATB- RETURNED TO SLC DUE TO LEFT ENGINE NACELLE OVERHEAT INDICATION. CORRECTIVE ACTION: REPLACED BUFFER AIR VALVE, BUFFER AIR VALVE SOLENOID, PRESSURE SENSOR, AND SENSE LINE DUE TO ASSOCIATED FAULTS.Apr 6, 2023 · N140DU · Bombdr BD1001A10 · Bleed Air Indicating SystemSDR DALA2023020300860Not Entered · not enteredSHIP 8140 - ATO - DURING THROTTLE UP DUE TO A RT FUEL EJECTOR FAIL MESSAGE AT ABOUT 55% N2. WHEN THROTTLE WAS BROUGHT BACK TO IDLE, CREW RECEIVED AN ENGINE 2 LOW FUEL PRESSURE MESSAGE. CORRECTIVE ACTION: FOUND MULTIPLE FUEL FEED PIPES WITH DAMAGED/CRACKED FLANJan 27, 2023 · N140DU · Bombdr BD1001A10 · Fuel Indicating SystemSDR DALA2022082605751None · noneSHIP 8140 -ATB- DUE TO LEFT ENGINE HIGH VIBRATION MESSAGE. CORRECTIVE ACTION: REMOVED NBR 1 ENGINE SPINNER, ACCOMPLISHED NBR 1 ENGINE FAN BLADES RE-SEQUENCE PER PW BALANCE BLADE SEQUENCE 736440. TESTED OK. LP 9005198Aug 24, 2022 · N140DU · Bombdr BD1001A10 · Powerplant SystemSDR DALA2022071204849None · noneTRANSFERRED FROM LOGBOOK: 9217326. CATERING REPORTED DENT ON BOTTOM RIGHT CORNER ON L2 DOOR REMOVED CORNER AND STRAIGHT SEAL RETAINERS. NO DAMAGE TO RETAINERS. REMOVED DAMAGE SKIN 1" X 2 3/4" ON LOWER AFT STRAIGHT EDGE JUST BEFORE CORNER. PER A220 SRM 52-12-01Jul 11, 2022 · N140DU · Bombdr BD1001A10 · Passenger/Crew DoorsSDR DALA2022051003265Pin · brokenR/H INTERIOR OVERWING EXIT SIGN INOP. FOUND BROKEN PIN ON SIGN. PARTS ON ORDER(WIP 868448) INSTALLED NEW LIGHT ASSEY PER A220 AMP 33-54-01. OPS CHECKS GOOD, OK FOR SERVICE. (LP# 2222753)May 4, 2022 · N140DU · Bombdr BD1001A10 · Emergency LightingSDR DALA2022042803005Light · inoperativeRT OWEED EMERGENCY UPPER LIGHT INOP. REMOVED AND REPLACED LIGHT PER A220 AMP 33-54. NO HELP. REINSTALLED ORIGINAL. FOUND 0 VOLTS AND NO SHORTS ON POWER WIRE IN REFERENCE WITH A220 ASDP 33-52-00-00AAA054A-A. POWERED DOWN AND POWERED UP AIRCRAFT PER A220 AMP 24-Apr 23, 2022 · N140DU · Bombdr BD1001A10 · Emergency LightingSDR DALA2022020400723None · noneWHILE IN MSP A FUELING TRUCK IMPACTED THE RH #3 FLAP FAIRING ON A/C 8140 (STK 81-5754-9-0044 / SN 00163 / FTN 5R8063). THE SUBJE CT FAIRING WAS ROUTED TO SHOP FOR REPAIR. ER/A 592835-14 REV 0RI G. SECT. I ACCOMPLISHED FOLLOW ON REQUIRED.ER/A 592835-14 REV. ORIFeb 1, 2022 · N140DU · Bombdr BD1001A10 · Trailing Edge Flaps
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