# Service difficulty reports: N140DU

A list on [N140DU](https://openairdocs.org/aircraft/N140DU.md).

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

- [SDR DALA2026102105793](https://openairdocs.org/sdr/DALA2026102105793.md): Door Frame · corroded · Oct 19, 2026 · N140DU · Airbus BD5001A10 · Fuselage Main, Structure
  > CORROSION 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)
- [SDR DALA2026102105792](https://openairdocs.org/sdr/DALA2026102105792.md): Door Frame · corroded · Oct 19, 2026 · N140DU · Airbus BD5001A10 · Fuselage Main, Structure
  > CORROSION 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)
- [SDR DALA2026102105791](https://openairdocs.org/sdr/DALA2026102105791.md): Door Frame · corroded · Oct 19, 2026 · N140DU · Airbus BD5001A10 · Fuselage Main, Structure
  > CORROSION 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)
- [SDR DALA2026102105790](https://openairdocs.org/sdr/DALA2026102105790.md): Door Frame · corroded · Oct 19, 2026 · N140DU · Airbus BD5001A10 · Fuselage Main, Structure
  > CORROSION 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)
- [SDR DALA2026101905729](https://openairdocs.org/sdr/DALA2026101905729.md): Seat Track · corroded · Oct 15, 2026 · N140DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION 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 GRO
- [SDR DALA2026101405649](https://openairdocs.org/sdr/DALA2026101405649.md): Web · corroded · Oct 8, 2026 · N140DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > CORROSION 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)
- [SDR DALA2026100705543](https://openairdocs.org/sdr/DALA2026100705543.md): Seat Track · corroded · Oct 6, 2026 · N140DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION 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 G
- [SDR DALA2026100705540](https://openairdocs.org/sdr/DALA2026100705540.md): Seat Track · corroded · Oct 5, 2026 · N140DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION 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)
- [SDR DALA2025071405287](https://openairdocs.org/sdr/DALA2025071405287.md): Light · inoperative · Jul 8, 2025 · N140DU · Airbus BD5001A10 · Emergency Lighting
  > FORWARD 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. OP
- [SDR DALA2025050603478](https://openairdocs.org/sdr/DALA2025050603478.md): Unknown · odor · May 2, 2025 · N140DU · Airbus BD5001A10 · Air Distribution System
  > AFTER 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)
- [SDR DALA2024121711795](https://openairdocs.org/sdr/DALA2024121711795.md): Door Sill · corroded · Dec 13, 2024 · N140DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > FWD 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)
- [SDR DALA2024121711794](https://openairdocs.org/sdr/DALA2024121711794.md): Waste Box · corroded · Dec 12, 2024 · N140DU · Airbus BD5001A10 · Fuselage Main, Structure
  > WASTE 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# 0705
- [SDR DALA2024121711793](https://openairdocs.org/sdr/DALA2024121711793.md): Seat Track · corroded · Dec 11, 2024 · N140DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT 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)
- [SDR DALA2024121711792](https://openairdocs.org/sdr/DALA2024121711792.md): Seat Track · corroded · Dec 11, 2024 · N140DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT 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)
- [SDR DALA2024120511471](https://openairdocs.org/sdr/DALA2024120511471.md): Strip · deteriorated · Dec 2, 2024 · N140DU · Airbus BD5001A10 · Vertical Stabilizer, Plate/Skin
  > VERTICAL 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 A
- [SDR DALA2024120511470](https://openairdocs.org/sdr/DALA2024120511470.md): Slat Track · damaged · Nov 29, 2024 · N140DU · Airbus BD5001A10 · Leading Edge Devices
  > COMPLETE 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 SLA
- [SDR DALA2024120511469](https://openairdocs.org/sdr/DALA2024120511469.md): Slat Track · scratched · Nov 29, 2024 · N140DU · Airbus BD5001A10 · Leading Edge Devices
  > COMPLETE 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 SLAT
- [SDR DALA2023091807654](https://openairdocs.org/sdr/DALA2023091807654.md): Unknown · unknown · Sep 16, 2023 · N140DU · Bombdr BD1001A10 · Leading Edge Slat Actuator
  > ON 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 LEAK
- [SDR DALA2023090107136](https://openairdocs.org/sdr/DALA2023090107136.md): Unknown · unknown · Aug 31, 2023 · N140DU · Bombdr BD1001A10 · Air Distribution System
  > BURNING 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 FUM
- [SDR DALA2023060104398](https://openairdocs.org/sdr/DALA2023060104398.md): Unknown · unknown · May 25, 2023 · N140DU · Bombdr BD1001A10 · Fire Protection System
  > SHIP 8140 - DIV - TO ABQ DUE TO "EQUIP BAY SMOKE FAIL" CAUTION MESSAGE. CORRECTIVE ACTION: REPLACED BOTH EQUIPMENT BAY SMOKE DETECTORS. (LP# 9736464)
- [SDR DALA2023042603264](https://openairdocs.org/sdr/DALA2023042603264.md): Unknown · unknown · Apr 20, 2023 · N140DU · Bombdr BD1001A10 · Leading Edge Devices
  > ERA 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.
- [SDR DALA2023041102852](https://openairdocs.org/sdr/DALA2023041102852.md): Unknown · unknown · Apr 6, 2023 · N140DU · Bombdr BD1001A10 · Bleed Air Indicating System
  > SHIP 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.
- [SDR DALA2023020300860](https://openairdocs.org/sdr/DALA2023020300860.md): Not Entered · not entered · Jan 27, 2023 · N140DU · Bombdr BD1001A10 · Fuel Indicating System
  > SHIP 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 FLAN
- [SDR DALA2022082605751](https://openairdocs.org/sdr/DALA2022082605751.md): None · none · Aug 24, 2022 · N140DU · Bombdr BD1001A10 · Powerplant System
  > SHIP 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 9005198
- [SDR DALA2022071204849](https://openairdocs.org/sdr/DALA2022071204849.md): None · none · Jul 11, 2022 · N140DU · Bombdr BD1001A10 · Passenger/Crew Doors
  > TRANSFERRED 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 52-12-01
- [SDR DALA2022051003265](https://openairdocs.org/sdr/DALA2022051003265.md): Pin · broken · May 4, 2022 · N140DU · Bombdr BD1001A10 · Emergency Lighting
  > R/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)
- [SDR DALA2022042803005](https://openairdocs.org/sdr/DALA2022042803005.md): Light · inoperative · Apr 23, 2022 · N140DU · Bombdr BD1001A10 · Emergency Lighting
  > RT 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-
- [SDR DALA2022020400723](https://openairdocs.org/sdr/DALA2022020400723.md): None · none · Feb 1, 2022 · N140DU · Bombdr BD1001A10 · Trailing Edge Flaps
  > WHILE 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. ORI

## 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 = 'N140DU' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N140DU/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.