# Service difficulty reports: N110DU

A list on [N110DU](https://openairdocs.org/aircraft/N110DU.md).

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

- [SDR DALA2026031201744](https://openairdocs.org/sdr/DALA2026031201744.md): Unknown · odor · Mar 10, 2026 · N110DU · Airbus BD5001A10 · Air Distribution System
  > RETURNED 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)
- [SDR DALA2026030501531](https://openairdocs.org/sdr/DALA2026030501531.md): Unknown · odor · Mar 4, 2026 · N110DU · Airbus BD5001A10 · Air Distribution System
  > AFTER 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
- [SDR DALA2026030401501](https://openairdocs.org/sdr/DALA2026030401501.md): Packing · leaking · Mar 1, 2026 · N110DU · Airbus BD5001A10 · Turbine Engine Oil System
  > AFTER 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 OF
- [SDR DALA2026030201406](https://openairdocs.org/sdr/DALA2026030201406.md): Heater · odor · Feb 26, 2026 · N110DU · Airbus BD5001A10 · Heating System
  > DUE TO DECLARED EMERGENCY FOR BURNING PLASTIC SMELL. R/R AFT GALLEY HEATER AND Y REDUCER DUCT. (L/P# 8036184, 8036185)
- [SDR DALA2026022601376](https://openairdocs.org/sdr/DALA2026022601376.md): Fan · odor · Feb 25, 2026 · N110DU · Airbus BD5001A10 · Air Distribution Fan
  > SHIP 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. CL
- [SDR DALA2026022701386](https://openairdocs.org/sdr/DALA2026022701386.md): Oxygen Mask · deployed · Feb 24, 2026 · N110DU · Airbus BD5001A10 · Passenger Oxygen System
  > CREW 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)
- [SDR DALA2025061004422](https://openairdocs.org/sdr/DALA2025061004422.md): Sensor · inoperative · Jun 6, 2025 · N110DU · Airbus BD5001A10 · Door Warning System
  > WHEN 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
- [SDR DALA2025060204206](https://openairdocs.org/sdr/DALA2025060204206.md): Support Frame · corroded · May 31, 2025 · N110DU · Airbus BD5001A10 · Aerodynamic Fairings
  > AIRCRAFT 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)
- [SDR DALA2025053104191](https://openairdocs.org/sdr/DALA2025053104191.md): Doubler · corroded · May 31, 2025 · N110DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > AIRCRAFT 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)
- [SDR DALA2025053104190](https://openairdocs.org/sdr/DALA2025053104190.md): Support Frame · corroded · May 31, 2025 · N110DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > AIRCRAFT 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)
- [SDR DALA2025053104189](https://openairdocs.org/sdr/DALA2025053104189.md): Skin · corroded · May 31, 2025 · N110DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > AIRCRAFT 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)
- [SDR DALA2025053104187](https://openairdocs.org/sdr/DALA2025053104187.md): Support Angle · corroded · May 30, 2025 · N110DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > AIRCRAFT 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)
- [SDR DALA2025053104186](https://openairdocs.org/sdr/DALA2025053104186.md): Hinge · corroded · May 30, 2025 · N110DU · Airbus BD5001A10 · Fuselage, Door Hinge
  > AIRCRAFT 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)
- [SDR DALA2025053004148](https://openairdocs.org/sdr/DALA2025053004148.md): Skin · not reported · May 29, 2025 · N110DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > AIRCRAFT 8110, EXTERNAL SKIN BETWEEN FRAMES 26 AND 27 AND STRINGER 36L-36R. CORRECTIVE ACTION: ACCOMPLISHED ERA 626447-14 REV ORG. (LP 0994286)
- [SDR DALA2025052704053](https://openairdocs.org/sdr/DALA2025052704053.md): Floor Panel · corroded · May 26, 2025 · N110DU · Airbus BD5001A10 · Fuselage Floor Panel
  > CORROSION 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)
- [SDR DALA2025052704052](https://openairdocs.org/sdr/DALA2025052704052.md): Floor Panel · corroded · May 26, 2025 · N110DU · Airbus BD5001A10 · Fuselage Floor Panel
  > CORROSION 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)
- [SDR DALA2025052704051](https://openairdocs.org/sdr/DALA2025052704051.md): Web · corroded · May 26, 2025 · N110DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > CORROSION 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. L
- [SDR DALA2025052704042](https://openairdocs.org/sdr/DALA2025052704042.md): Seat Track · corroded · May 21, 2025 · N110DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION 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. CORRECTION
- [SDR DALA2025052704041](https://openairdocs.org/sdr/DALA2025052704041.md): Seat Track · corroded · May 21, 2025 · N110DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION 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:
- [SDR DALA2025052704031](https://openairdocs.org/sdr/DALA2025052704031.md): Seat Track · corroded · May 20, 2025 · N110DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION 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)
- [SDR DALA2025052103921](https://openairdocs.org/sdr/DALA2025052103921.md): Cargo Track · corroded · May 17, 2025 · N110DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > **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)
- [SDR DALA2025052103920](https://openairdocs.org/sdr/DALA2025052103920.md): Cargo Track · corroded · May 17, 2025 · N110DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > ***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-J51-42-21-0
- [SDR DALA2025052003866](https://openairdocs.org/sdr/DALA2025052003866.md): Seat Track · corroded · May 16, 2025 · N110DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > ***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)
- [SDR DALA2023062005005](https://openairdocs.org/sdr/DALA2023062005005.md): Unknown · unknown · Jun 19, 2023 · N110DU · Bombdr BD1001A10 · Aerodynamic Fairings
  > WHILE 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)
- [SDR DALA2022121908202](https://openairdocs.org/sdr/DALA2022121908202.md): Computer · degraded · Dec 17, 2022 · N110DU · Bombdr BD1001A10 · Flight Control System
  > SHIP 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.
- [SDR DALA2022110407169](https://openairdocs.org/sdr/DALA2022110407169.md): Longeron · cracked · Nov 3, 2022 · N110DU · Bombdr BD1001A10 · Fuselage Main, Longeron/Stringer
  > AIRCRAFT 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 2480660
- [SDR DALA2022040502308](https://openairdocs.org/sdr/DALA2022040502308.md): Door · faulty · Apr 4, 2022 · N110DU · Bombdr BD1001A10 · Passenger/Crew Doors
  > SHIP 8110 - 1 DOOR EOAM IN YELLOW BAND. CORRECTIVE ACTION: SERVICE EOAM WITH NITROGEN PER AMP 52-46-08-01AAA-214A-A. (8758316)
- [SDR DALA2022032502003](https://openairdocs.org/sdr/DALA2022032502003.md): Hinge · cracked · Mar 23, 2022 · N110DU · Bombdr BD1001A10 · Elevator Structure
  > L/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)
- [SDR DALA2022031701761](https://openairdocs.org/sdr/DALA2022031701761.md): None · none · Mar 15, 2022 · N110DU · Bombdr BD1001A10 · Fuselage Internal Mounting Structure
  > ER/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 ADDED
- [SDR DALA2022030901546](https://openairdocs.org/sdr/DALA2022030901546.md): None · none · Mar 5, 2022 · N110DU · Bombdr BD1001A10 · Landing Gear Actuator
  > 32 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, W
- [SDR DALA2021110206754](https://openairdocs.org/sdr/DALA2021110206754.md): None · none · Oct 28, 2021 · N110DU · Bombdr BD1001A10 · Fuselage Main, Plate/Skin
  > A220-100 / 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. NOT
- [SDR DALA2021082004885](https://openairdocs.org/sdr/DALA2021082004885.md): Light · malfunctioned · Aug 19, 2021 · N110DU · Airbus BD5001A10 · Emergency Lighting
  > GREEN 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)
- [SDR DALA2021102906689](https://openairdocs.org/sdr/DALA2021102906689.md): None · none · Oct 30, 2020 · N110DU · Bombdr BD1001A10 · Fuselage Main, Plate/Skin
  > AMOC 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
- [SDR DALA2021102906688](https://openairdocs.org/sdr/DALA2021102906688.md): None · none · Oct 30, 2020 · N110DU · Bombdr BD1001A10 · Fuselage Main, Plate/Skin
  > DTE 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
- [SDR DALA2019071204254](https://openairdocs.org/sdr/DALA2019071204254.md): Reu · malfunctioned · Jul 12, 2019 · N110DU · Bombdr BD1001A10 · Drag Control System
  > AT 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-398D
- [SDR DALA2019061873625](https://openairdocs.org/sdr/DALA2019061873625.md): Unknown · malfunctioned · Jun 12, 2019 · N110DU · Bombdr BD1001A10 · Navigation System
  > ACARS 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. INERTI
- [SDR DALA2019043002741](https://openairdocs.org/sdr/DALA2019043002741.md): Bleed Valve · malfunctioned · Apr 24, 2019 · N110DU · Bombdr BD1001A10 · Compressor Bleed Valve
  > SHIP 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# 51193

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N110DU/reports

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