# Service difficulty reports: N143DU

A list on [N143DU](https://openairdocs.org/aircraft/N143DU.md).

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

- [SDR DALA2026062303734](https://openairdocs.org/sdr/DALA2026062303734.md): Control Valve · faulted · Jun 21, 2026 · N143DU · Airbus BD5001A10 · Landing Gear Retraction/Extension System
  > ALTERNATE GEAR EXTENSION USED DUE TO GEAR FAIL MESSAGE AFTER GEAR SELECTED DOWN. REPLACED LANDING GEAR CONTROL VALVE (LGCV). (L/P# 8734702; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026062303733](https://openairdocs.org/sdr/DALA2026062303733.md): Skin · corroded · Jan 13, 2026 · N143DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > ERA 620866 REVISED TO REV A. SECTION I ISSUED FOR CORROSION TO AFT FUSELAGE SKIN SURROUND WASTE SERVICE CUTOUT. FOLLOW ON ACTION REQUIRED. ACCOMPLISH SECTION IV WITHIN 2 FC OF LOG PAGE CREATION. SECTION II REQUIRED EVERY 1000 FH THEREAFTER UNTIL SECTION III. S
- [SDR DALA2025102907933](https://openairdocs.org/sdr/DALA2025102907933.md): Engine · odor · Oct 23, 2025 · N143DU · Airbus BD5001A10 · Engine (Turbine/Turboprop)
  > WITH INBOUND W/U OF ODOR IN CABIN. C/W W/C 0550-2001. #1 ENG IDENTIFIED AS CAUSE OF SMELL @ 180K PARTICULATE COUNT. #1 ENG IS SOURCE OF SMELL, MEL 36-12-00A APPLIED AS WELL AS MON LOG FOR ENG WASH. C/W 0550-2003. RECIR FILTERS REPLACED. NO FINDINGS OF OIL PACK
- [SDR DALA2025100607257](https://openairdocs.org/sdr/DALA2025100607257.md): Oil Cooler · leaking · Oct 3, 2025 · N143DU · Airbus BD5001A10 · APU Oil System
  > FA SMELLED CHEMICAL SMELL IN AFT GALLEY ON APU AIR. PERFORMED W/C #0550-2001 TO ISOLATE SMELL OF SMOKE & FUMES. WHILE USING SNIFFER TOOL, NO PRESENCE OF ODOR FOUND. WHILE INSPECTING APU, FOUND OIL WETTING ON APU OIL COOLER. RECOMMEND REPLACING OIL COOLER. R/R
- [SDR DALA2025062004646](https://openairdocs.org/sdr/DALA2025062004646.md): Brake · fault message · Jun 17, 2025 · N143DU · Airbus BD5001A10 · Landing Gear Brake System
  > BRAKE ON MESSAGE ON IN FLIGHT. PARK BRAKE FAIL MESSAGE IN FLIGHT. PERFORMED TROUBLESHOOTING AND REPAIR REFERENCE LOG 1026603 FOR R /R #3 EMCU. FAULT IS CLEARED. OMS BDCU1 AND 1 SHOW NO PRESSURE. FAULT IS CLEARED. M PROCEDURES REVERSED. PLACARDS REMOVED. OK FOR
- [SDR DALA2025042403236](https://openairdocs.org/sdr/DALA2025042403236.md): Slat Track · corroded · Apr 23, 2025 · N143DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK #7 PINION TOOTH #2 LWR SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF. 5742-01028-02B. LIAISON ENGINEERING REQUIRED BEFORE FURTHER FLIGHT. COMPLIED WITH ER/A 625943-14AD REV 0 AND PRI 625943-14AD REV 0 MATCHES. (LP# 0929465)
- [SDR DALA2025030501718](https://openairdocs.org/sdr/DALA2025030501718.md): Unknown · odor · Feb 28, 2025 · N143DU · Airbus BD5001A10 · Air Distribution System
  > CHEMICAL SMELL FROM FLIGHT DECK GASPERS IN FLIGHT. STARTED DURING CLIMB OUT. WAS INTERMITTENT TILL CRUISE DISSIPATED WHEN REACHED TOP OF CLIMB. C/W NO GO ODI CK LIST REF LOG 0831762 AND DEFERRED APU TO MEL 49 -00-03A REF LOG 6481423. (LP# 6481422)
- [SDR DALA2025030301599](https://openairdocs.org/sdr/DALA2025030301599.md): Filter · odor · Feb 23, 2025 · N143DU · Airbus BD5001A10 · Air Distribution System
  > STRONG BURNT ELECTRICAL SMELL IN FWD GALLEY AND FLIGHT DECK AFTER APU START ON ARRIVAL IN MSY. C/W NO GO ODI ATA 2172 STEPS 1-4, REPLACED BOTH RECIR FILTERS IAW AJ21-22-03-01AAA-520A, ALSO POWERED UP ALL GALLEYS,NO ELECTRICAL SMELL DETECTED, OK FOR SVC. (LP#
- [SDR DALA2025010600119](https://openairdocs.org/sdr/DALA2025010600119.md): Unknown · odor · Jan 3, 2025 · N143DU · Airbus BD5001A10 · Air Distribution System
  > AFTER LANDING FA REPORTED STRONG BURNING SMELL IN THE AFT GALLEY AND SAID THAT THE PAX IN THE LAST TWO ROWS WERE COUGHING AND COVERING THEIR MOUTHS. C/W W/CS 0550-2001/0550-2003/0550-2002. R/R BOTH RECIRC FILTERS PER A220 AMP 21-22. OPS CHECK GOOD. OK FOR SVC.
- [SDR DALA2024092009270](https://openairdocs.org/sdr/DALA2024092009270.md): Skin · corroded · Sep 19, 2024 · N143DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE WASTE BOX EXTERIOR SKIN AROUND CUTOUT (146BR) FWD RT CORNER HAS CORROSION. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0255:2021-2025/002 00234 COMPLIED WITH PRI 620866-14 REV 0, PRI 620866-14 REV 1, AND ER/A 620866-14 REV ORIGINAL. (LP# 05652
- [SDR DALA2024030703124](https://openairdocs.org/sdr/DALA2024030703124.md): Unknown · fumes · Mar 4, 2024 · N143DU · Airbus BD5001A10 · Air Distribution System
  > SHIP 8143 - ATB - DUE TO FUMES IN FLIGHT DECK AFTER TAKEOFF. C/W AMDS CARD 0550-2001. ACCOMPLISHED BSI OF #1 & #2 ENGINES. ERA 613840-14 ADDED AND AIRCRAFT PUT ON MONITOR.
- [SDR DALA2024030603077](https://openairdocs.org/sdr/DALA2024030603077.md): Unknown · odor · Mar 3, 2024 · N143DU · Airbus BD5001A10 · Air Distribution System
  > FA IN BACK OF A/C REPORTED DIRTY SOCK SMELL ON TO UP TO 10000'. SMELL DISSIAPATED AND NO FUMES WERE PRESENT ON THE FLIGHT DECK. COWL ANTI ICE WAS ON FOR TO. SMOKE/FUMES SURVEY DONE ELECTRONIC. PERFORMED AMDS 0550-2001. ALL FIND SENT TO MC FOR REVIEW. WIP 66031
- [SDR DALA2024012401094](https://openairdocs.org/sdr/DALA2024012401094.md): Slat Track · corroded · Jan 24, 2024 · N143DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 7 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA 5742-01028-02B, LIASON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NBR 7 UPPER AFT SURFACE PER ERA 608052- 14AD REV B AND PRI REV 0 MATCH
- [SDR DALA2024012401093](https://openairdocs.org/sdr/DALA2024012401093.md): Slat Track · corroded · Jan 24, 2024 · N143DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 8 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA 5742-01028-02B, LIASON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NBR 8 LOWER AFT SURFACE PER ERA 608052- 14AD REV B AND PRI REV 0 MATCH
- [SDR DALA2024012401092](https://openairdocs.org/sdr/DALA2024012401092.md): Slat Track · corroded · Jan 24, 2024 · N143DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 6 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION IN TWO SEPERATE PLACES AND PREVIOUS REWORK. REF AA 5742-01028- 02B, LIASON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NBR 6 UPPER AFT SURFACE PER ERA 608052- 14AD R
- [SDR DALA2024012401091](https://openairdocs.org/sdr/DALA2024012401091.md): Slat Track · corroded · Jan 24, 2024 · N143DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 5 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA 5742-01028-02B, LIASON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NBR 5 UPPER AFT SURFACE PER ERA 608052- 14AD REV B AND PRI REV 0 MATCH
- [SDR DALA2024012401090](https://openairdocs.org/sdr/DALA2024012401090.md): Slat Track · corroded · Jan 24, 2024 · N143DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 5 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA 5742-01028-02B, LIASON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NBR 5 LOWER AFT SURFACE PER ERA 608052- 14AD REV B AND PRI REV 0 MATCH
- [SDR DALA2024012401089](https://openairdocs.org/sdr/DALA2024012401089.md): Slat Track · corroded · Jan 24, 2024 · N143DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA 5742-01028-02B, LIASON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NBR 5 UPPER FWD SURFACE PER ERA 608052- 14AD REV B AND PRI REV 0 MATCH
- [SDR DALA2024012401088](https://openairdocs.org/sdr/DALA2024012401088.md): Slat Track · corroded · Jan 24, 2024 · N143DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA 5742-01028-02B, LIASON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLIGHT.REPAIRED RH SLAT TRACK NBR 4 LOWER AFT SURFACE PER ERA 608052- 14AD REV B AND PRI REV 0 MATCHE
- [SDR DALA2024012401087](https://openairdocs.org/sdr/DALA2024012401087.md): Slat Track · corroded · Jan 24, 2024 · N143DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA 5742-01028-02B, LIASON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NBR 4 UPPER FWD SURFACE PER ERA 608052- 14AD REV B AND PRI REV 0 MATCH
- [SDR DALA2024012401086](https://openairdocs.org/sdr/DALA2024012401086.md): Slat Track · corroded · Jan 24, 2024 · N143DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 3 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND WITH NO EVIDENCE OF PREVIOUS REWORK. REF AA 5742-01028-02B, LIASON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NBR 3 UPPER AFT SURFACE PER ERA 608052- 14AD REV B
- [SDR DALA2024012401085](https://openairdocs.org/sdr/DALA2024012401085.md): Slat Track · corroded · Jan 24, 2024 · N143DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 2 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND NO EVIDENCE OF PREVIOUS REWORK. REF AA 5742-01028-02B, LIASON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NBR 2 UPPER AFT SURFACE PER ERA 608052- 14AD REV B AND
- [SDR DALA2024012401084](https://openairdocs.org/sdr/DALA2024012401084.md): Slat Track · corroded · Jan 24, 2024 · N143DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 1 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA 5742-01028-02B, LIASON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NBR 1 UPPER FWD SURFACE PER ERA 608052- 14AD REV B AND PRI REV 0 MATCH
- [SDR DALA2024012401083](https://openairdocs.org/sdr/DALA2024012401083.md): Slat Track · corroded · Jan 23, 2024 · N143DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 6 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA 5742-01028-02A, LIASON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 6 LOWER AFT SURFACE PER ERA 608053- 14AD REV B AND PRI REV 0 MATCH
- [SDR DALA2024012401082](https://openairdocs.org/sdr/DALA2024012401082.md): Slat Track · corroded · Jan 23, 2024 · N143DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 3 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA 5742-01028-02A, LIASON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 3 UPPER FWD SURFACE PER ERA 608053- 14AD REV B AND PRI REV 0 MATCH
- [SDR DALA2024012401081](https://openairdocs.org/sdr/DALA2024012401081.md): Slat Track · corroded · Jan 23, 2024 · N143DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 2 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA 5742-01028-02A, LIASON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 2 UPPER AFT SURFACE PER ERA 608053- 14AD REV B AND PRI REV 0 MATCH
- [SDR DALA2024012401080](https://openairdocs.org/sdr/DALA2024012401080.md): Slat Track · corroded · Jan 23, 2024 · N143DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 4 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA 5742-01028-02A, LIASON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 4 UPPER FWD SURFACE PER ERA 608053- 14AD REV B AND PRI REV 0 MATCH
- [SDR DALA2024012401079](https://openairdocs.org/sdr/DALA2024012401079.md): Slat Track · corroded · Jan 23, 2024 · N143DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 4 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA 5742-01028-02A, LIASON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR4 LOWER AFT SURFACE PER ERA 608053- 14AD REV B AND PRI REV 0 MATCHE
- [SDR DALA2024012401078](https://openairdocs.org/sdr/DALA2024012401078.md): Slat Track · corroded · Jan 23, 2024 · N143DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA 5742-01028-02A, LIASON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 5 UPPER FWD SURFACE PER ERA 608053- 14AD REV B AND PRI REV 0 MATCHE
- [SDR DALA2024012401077](https://openairdocs.org/sdr/DALA2024012401077.md): Slat Track · corroded · Jan 23, 2024 · N143DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 6 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF AA 5742-01028-02A, LIASON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 6 UPPER AFT SURFACE PER ERA 608053- 14AD REV B AND PRI REV 0 MATCH
- [SDR DALA2023042003130](https://openairdocs.org/sdr/DALA2023042003130.md): Unknown · unknown · Apr 17, 2023 · N143DU · Airbus BD5001A10 · Leading Edge Devices
  > ERA 608052-14AD SECTION I ISSUED FOR CORROSION TO RH SLAT TRACKS. ACCOMPLISH SECTION II EVERY 850 FH UNTIL SECTION III. SECTION III REQUIRED PRIOR TO 8500FH FROM SECTION I ACCOMPLISHMENT. ASSOCIATED AA 5742-01028 ADDED FOR AC 8143 ASSOCIATED ER/A 00-608052 ADD

## 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 = 'N143DU' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N143DU/reports

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