N110DU

Service difficulty reports · 37

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 = 'N110DU' 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 DALA2026031201744Unknown · odorRETURNED TO MSP DUE TO ODOR/FUME EVENT. REPLACED LT PACK REHEATER. PERFORMED APU AND BOTH ENGINE BURNOUTS, 3 TIMES EACH WITH REF TO W/C 0550-2003. RE-ACCOMPLISHED W/C 0550-2001-02. NO ANOMALIES NOTED. (LP# 8718424, 8718432, 1484365)Mar 10, 2026 · N110DU · Airbus BD5001A10 · Air Distribution SystemSDR DALA2026030501531Unknown · odorAFTER ARRIVING AT GATE, FA'S REPORTED A "JET FUEL" ODOR THROUGHOUT THE ENTIRE FLIGHT. FLIGHT CREW DID NOT SMELL THE ODOR , AND WERE NOT NOTIFIED OF ODOR UNTIL AT THE GATE. C/W NO GO ODI SMOKE AND FUME PREVENTION. PERFORMED BSI OF ENG 1, ESN 736186. NO WETTING Mar 4, 2026 · N110DU · Airbus BD5001A10 · Air Distribution SystemSDR DALA2026030401501Packing · leakingAFTER 35 MIN FLIGHT FAS REPORTED BURNING PLASTIC SMELL FROM THE BACK GALLEY. SHORTLY AFTER WE ALSO SMELLED IN THE FLIGHT DECK DONNED MASKS AND EXPEDITED TO SLC AND COMPLETED QRH. C/W W/C 0550-2001 STEPS 1-10+13-16 COMPLETED STEP 11 OF W/C 0550-2001. C/W BSI OFMar 1, 2026 · N110DU · Airbus BD5001A10 · Turbine Engine Oil SystemSDR DALA2026030201406Heater · odorDUE TO DECLARED EMERGENCY FOR BURNING PLASTIC SMELL. R/R AFT GALLEY HEATER AND Y REDUCER DUCT. (L/P# 8036184, 8036185)Feb 26, 2026 · N110DU · Airbus BD5001A10 · Heating SystemSDR DALA2026022601376Fan · odorSHIP 8110 - ATB - RETURNED TO SLC AND DECLARED EMERGENCY DUE TO FUMES IN THE CABIN. MASKS WERE DEPLOYED IN THE CABIN. FLIGHT LANDED SAFELY ON THE GROUND. CORRECTIVE ACTION: R/R AFT GALLEY FAN, HEATER AND SENSOR. REPLACED ALL THE ACTIVATED OXYGEN GENERATORS. CLFeb 25, 2026 · N110DU · Airbus BD5001A10 · Air Distribution FanSDR DALA2026022701386Oxygen Mask · deployedCREW DEPLOYED O2 MASKS AND ALL O2 GENERATORS DEPLOYED WITH THE EXCEPTION OF LAVATORIES. FWD TO 46 EA NON-ROUTINES FOR GEN REPLACEMENT, MASK CLEANING AND REINSTALL. (LP# 8036172, MSI# 2026-00141)Feb 24, 2026 · N110DU · Airbus BD5001A10 · Passenger Oxygen SystemSDR DALA2025061004422Sensor · inoperativeWHEN DISARMING DOORS FOR ARRIVAL, DOOR SLIDE FAULT EICAS MESSAGE CAME AND WENT A FEW TIMES. THERE WAS AN INFO MESSAGE RELATED TO FWD SERVICE DOOR TARGET SNSR INOP AS WELL. T/S AS PER A220 EFIM SOL.# 2-39021 (FAULT CODE:5277F0025). VERIFIED MT94/MT92 PROX SNSR Jun 6, 2025 · N110DU · Airbus BD5001A10 · Door Warning SystemSDR DALA2025060204206Support Frame · corrodedAIRCRAFT 8110, CORROSION ON WING TO BODY FAIRING SUPPORT FRAME AT FR 48, BETWEEN BL0 TO RBL 13. CORRECTIVE ACTION: ACCOMPLISHED REPAIR ERA 626621-14 REV ORG. (LP 0998166)May 31, 2025 · N110DU · Airbus BD5001A10 · Aerodynamic FairingsSDR DALA2025053104191Doubler · corrodedAIRCRAFT 8110, CORROSION ON WASTE WATER SERVICE PANEL DOUBLER, FWD EDGE, INBOARD HALF. COMPLIED WITH ER/A 626683-14 REV ORIGINAL SECTION I ASSOCIATED ER/A 14-626683. (LP 0996888)May 31, 2025 · N110DU · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2025053104190Support Frame · corrodedAIRCRAFT 8110, CORROSION SPOTS ON WASTE WATER SERVICE PANEL, BALL VALVE SURROUNDING FRAME, FWD INBOARD CORNER. COMPLIED WITH ER/A 626683-14 REV ORIGINAL SECTION I ASSOCIATED ER/A 14-626683. (LP 0996881)May 31, 2025 · N110DU · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2025053104189Skin · corrodedAIRCRAFT 8110, CORRODED SKIN LOWER FR75 BETWEEN STR 35-36 FWD EDGE OF WASTE SERVICE DOOR/PAN. CORRECTIVE ACTION: COMPLIED WITH ER/A 626683-14 REV ORIGINAL SECTION I ASSOCIATED ER/A 14-626683. (LP 0996874)May 31, 2025 · N110DU · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2025053104187Support Angle · corrodedAIRCRAFT 8110, CORROSION SPOT ON WASTE WATER SERVICE PANEL, BONDING JUMPER SUPPORT ANGLE. REPLACED BONDING JUMPER SUPPORT ANGLE ON WASTE SERVICE BOX PER IPDP A220BD500-A-J52-47-06-05AAA-941A-A. (LP 0996337)May 30, 2025 · N110DU · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2025053104186Hinge · corrodedAIRCRAFT 8110, CORROSION ON WASTE WATER SERVICE DOOR, INBOARD HINGE ARM. SSI: 53-61-56-02. REPLACED AND INSTALLED NEW DOOR ASSEMBLY IAW A220 AMP BD500-A-J52-47-06-05AAA-720A-A. (LP 0996322)May 30, 2025 · N110DU · Airbus BD5001A10 · Fuselage, Door HingeSDR DALA2025053004148Skin · not reportedAIRCRAFT 8110, EXTERNAL SKIN BETWEEN FRAMES 26 AND 27 AND STRINGER 36L-36R. CORRECTIVE ACTION: ACCOMPLISHED ERA 626447-14 REV ORG. (LP 0994286)May 29, 2025 · N110DU · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2025052704053Floor Panel · corrodedCORROSION ALONG INBOARD EDGE AND INBOARD AFT CORNER OF ASD ACCESS FLOOR PANEL 242MRF. REMOVED AND REPLACED APD FLOOR PANEL 242MRF IAW A220 AMP BD500- A-J53-00-47-14AAA-520A-A AND AMP BD500-A-J53-00-47-14AAA-720A-A. (LP# 0987498)May 26, 2025 · N110DU · Airbus BD5001A10 · Fuselage Floor PanelSDR DALA2025052704052Floor Panel · corrodedCORROSION ALONG INBOARD EDGE AND INBOARD AFT CORNER OF APD ACCESS FLOOR PANEL 241MLF. REMOVED AND REPLACED APD FLOOR PANEL 241MLF IAW A220 AMP BD500- A-J53-00-47-13AAA-520A-A AND AMP BD500-A-J53-00-47-13AAA-720A-A. (LP# 0987490)May 26, 2025 · N110DU · Airbus BD5001A10 · Fuselage Floor PanelSDR DALA2025052704051Web · corrodedCORROSION ON CABIN FLOOR STRUCTURE WEB AT FR76 AND 4.5 INCHES AFT OF FR76, BETWEEN RBL50 AND RBL48, WL151. REMOVED AND REPLACED FLOOR STRUCTURE WEB RBL50 TO RBL 48, FR 76 TO FR 79 IAW A220 ASRP BD 500-A-J51-42-06-00AAA-078A-A AND BOMBARDIER DWG C0132700 REV. LMay 26, 2025 · N110DU · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2025052704042Seat Track · corrodedCORROSION ON SEAT TRACK AFT END AT FR74, RBL43, WL151 (CORROSION SSI: 53-61-43-01). REMOVED AND REPLACED NEW SEAT TRACK FROM FR60 TO FR74, RBL 43, WL 151 IAW A220 ASRP BD500-A-J51-42-21-00AAA-078A-A AND DWG C01342701 REV: E AND DWG C01303300 REV G . CORRECTIONMay 21, 2025 · N110DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025052704041Seat Track · corrodedCORROSION ON SEAT TRACK AFT END AT FR74, LBL23, WL151 ( CORROSION SSI: 53-61-43-01). REMOVED AND REPLACED SEAT TRACK BETWEEN FR61 TO FR74, LBL 23, WL 151 PER A220 ASRP BD500-A-J51-42-21-00AAA-078A-A AND DWG C01342701 REV:-E AND DWG C01303300 REV:G. CORRECTION:May 21, 2025 · N110DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025052704031Seat Track · corrodedCORROSION ON FWD END OF SEAT TRACK @ FR20, RBL23, WL151. REMOVED AND REPLACED SEAT TRACK BETWEEN FR19+9"TO FR30+9", RBL 23, WL151 IAW A220 ASRP BD500-A-J51-42-21-00AAA-078A-A AND BOMBARDIER DWG: C02312600 REV: E. (LP# 0976208)May 20, 2025 · N110DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025052103921Cargo Track · corroded**CORROSION*** ON SEAT TRACK AFT END AT FR74, RBL23, WL151 ( CORROSION SSI: 53-61-43-01). REMOVED AND REPLACED SEAT TRACK FROM FR 64 TO FR 71 RBL 23 WL 151 IAW A220 ASRP BD500-A-J51-42-21-00AAA-078A-A AND DWG PL C01342701 REV-G. (LP# 0971647)May 17, 2025 · N110DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025052103920Cargo Track · corroded***CORROSION*** ON FWD END OF SEAT TRACK @ FR20, RBL43, WL151. REMOVED AND REPLACED SEAT TRACK BETWEEN FR 19+9" TO FR 30+9", RBL 43, WL 151 IAW A220 ASRP BD500-A-J51-42-20-00AAA-078A-A AND BOMBARDIER DWG C02312600 REV: E CORRECTED REF: ASRP BD500-A-J51-42-21-0May 17, 2025 · N110DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025052003866Seat Track · corroded***CORROSION*** ON SEAT TRACK AFT END AT FR74, LBL43, WL 151 ( CORROSION SSI: 53-61-43-01). REPLACED SEAT TRACK LBL 43, WL 151 FR61 TO FR 75 IAW A220 ASRP BD500-A-J51-42-20-00AAA-078A-A AND BOMBARDIER DWG C01342701 REV. -G. (LP# 0969996)May 16, 2025 · N110DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2023062005005Unknown · unknownWHILE PERFORMING WORKCARD 5352-01038-01A, FOUND DAMAGE ON LONGERON STEP 10 D. R/R LT LONGERON P/N C02383111-001. C/W WORK CARD 5352-01038-07A. A/C OK FOR SVC. (LP# 4748362)Jun 19, 2023 · N110DU · Bombdr BD1001A10 · Aerodynamic FairingsSDR DALA2022121908202Computer · degradedSHIP 8110 - ATB - DUE TO PRIMARY FLIGHT CONTROL COMPUTERS 2 AND 3 DEGRADED. ALONG WITH PRIMARY POWER CONTROL UNIT INOP. REMOVED AND REPLACED #1 AFT REU.Dec 17, 2022 · N110DU · Bombdr BD1001A10 · Flight Control SystemSDR DALA2022110407169Longeron · crackedAIRCRAFT 8110, DURING AMDS 5352-01038-01A STEP 10 FOUND LT LONGERON P/N 53-1111-501 CRACKED. CORRECTIVE ACTION: REPLACED LT LONGERON REF AMDS 5352-01038-07A. P/N OFF 53-1111-501. LP 2480660Nov 3, 2022 · N110DU · Bombdr BD1001A10 · Fuselage Main, Longeron/StringerSDR DALA2022040502308Door · faultySHIP 8110 - 1 DOOR EOAM IN YELLOW BAND. CORRECTIVE ACTION: SERVICE EOAM WITH NITROGEN PER AMP 52-46-08-01AAA-214A-A. (8758316)Apr 4, 2022 · N110DU · Bombdr BD1001A10 · Passenger/Crew DoorsSDR DALA2022032502003Hinge · crackedL/H ELEVATOR #3 HINGE CRACKED AFT I/B SIDE. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0258:5521-2001-LH/ 001 00035 ACCOMPLISHED PRI 597909-14, REV. 0 AND ERA 597909-14, REV. ORIGINAL. (LP# 2167657)Mar 23, 2022 · N110DU · Bombdr BD1001A10 · Elevator StructureSDR DALA2022031701761None · noneER/A 597910-14 ISSUED FOR CORROSION ON THE WASTE BOX. FOLLOW ON ACTION IS REQUIRED. ER/A IS AD 2021-13-20 RELATED. ACCOMPLISH SECTION II WITHIN 8500FH FOLLOWING THE ACCOMPLISHMENT OF SECTION I. AD RELATED, NO DEVIATIONS ALLOWED. ASSOCIATED ER/A 00-597910 ADDEDMar 15, 2022 · N110DU · Bombdr BD1001A10 · Fuselage Internal Mounting StructureSDR DALA2022030901546None · none32 GEAR FAULT R GEAR UPLOCK MOTOR FAULT. T/S REF A220 EFIM SOL # 1-6996. FAULT RESET, NO CURRENT FAULTS NOTED AT THIS TIME. VER 4136A0000-03 UPLOCK ACT INSTALLED SVC LETTER EFFECTIVE. FOUND EVIDENCE OF HYD FLUID ON UPLOCK ACT. VERIFIED NO LEAKS AT THIS TIME, WMar 5, 2022 · N110DU · Bombdr BD1001A10 · Landing Gear ActuatorSDR DALA2021110206754None · noneA220-100 / FUSELAGE / NOSE FWD FUSELAGE / BL5.76R FWD OF FR10 / DENT. REPAIR APPROVAL IS LIMITED TO 30,000FC/52,500FH, (WHICHEVER OCCURS FIRST) FROM SECTION I REPAIR. ADDITIONAL ENGINEERING AUTHORIZATION IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. NOTOct 28, 2021 · N110DU · Bombdr BD1001A10 · Fuselage Main, Plate/SkinSDR DALA2021082004885Light · malfunctionedGREEN EMERGENCY EXIT LIGHTS ON EXITS DO NOT ILLUMINATE WHEN GEAR EXT. TURNED ON EMERGENCY EXIT LIGHTS. ALL EXIT SIGNS AT EMERGENCY EXIS ILLUMINATED. PERFORMED TEST OF INTERNAL EMERGENCY LIGHTING SYSTEM PER A220 AMP 33-52-00. TEST OK. (LP# 7920426)Aug 19, 2021 · N110DU · Airbus BD5001A10 · Emergency LightingSDR DALA2021102906689None · noneAMOC TRACKING LOG. ER/A 588339-14 SECTION I ISSUED FOR A REPAIR OF THE FUSELAGE SKIN AND INTERCOSTAL FWD OF FRAME 10, BL 5.76R. FOLLOW ON ACTION IS REQUIRED. THE REPAIR APPROVAL IS LIMITED TO 16000 TOTAL A/C FLIGHT CYCLES. AN AMOC TO AD 2019-23-15 IS REQUIRED Oct 30, 2020 · N110DU · Bombdr BD1001A10 · Fuselage Main, Plate/SkinSDR DALA2021102906688None · noneDTE TRACKING LOG. ER/A 588339-14 SECTION I WAS ISSUED FOR A FUSELAGE SKIN AND INTERCOSTAL REPAIR FWD OF FRAME 10 AT BL 5.76R FOLLOW ON ACTION IS REQUIRED. THE REPAIR APPROVAL IS LIMITED TO 12 MONTHS FROM SECTION I ACCOMPLISHMENT. A DAMAGE TOLERANCE EVALUATION Oct 30, 2020 · N110DU · Bombdr BD1001A10 · Fuselage Main, Plate/SkinSDR DALA2019071204254Reu · malfunctionedAT CRUISE 27-FLT CTRL FAULTS: SPOILER REU CCDL REDUND LOSS/ PFCC 3/ PFCC 2/ PFCC 1 DEGRADED/ IMM 1 INOP MESSAGES RECEIVED. TROUBLESHOT PER EFIM. CONTACTED MCC. PERFORMED RESET OF FLY-BY-WIRE POWER CONVERTER REU MFS 1 PER CS100 AMP BD500-A-J24- 00-00-07AAA-398DJul 12, 2019 · N110DU · Bombdr BD1001A10 · Drag Control SystemSDR DALA2019061873625Unknown · malfunctionedACARS MESSAGE ENROUTE ON J-6 APPROACHING ESL VOR ATC ADVISED WE WERE 10NM NORTH OF COURSE. AFTER SEVERAL ATTEMPTS TO PROCEED RAW DATA TO HVQ WERE ABLE TO REESTABLISH BACK ON J6. REMAINDER OF FLIGHT OK. PERFORMED TASK AMP BD 500-A-J34-45-00-01AAA-320A-A. INERTIJun 12, 2019 · N110DU · Bombdr BD1001A10 · Navigation SystemSDR DALA2019043002741Bleed Valve · malfunctionedSHIP 8110 DECLARED AN EMERGENCY FOR RIGHT ENGINE DEGRADED MESSAGE WITH A FADAC 1 FAULT ON DESCENT INTO DTW . CORRECTIVE ACTION: MTC FOUND 2.5 BLEED ACTUATOR FAULT TRIGGERED. BLEED VALVE REPLACED IN ACCORDANCE WITH AS-100 AMP TASK PW1000G-A-75-32-01. (LP# 51193Apr 24, 2019 · N110DU · Bombdr BD1001A10 · Compressor Bleed Valve
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