# Service difficulty reports: N128DU

A list on [N128DU](https://openairdocs.org/aircraft/N128DU.md).

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

- [SDR DALA2026031701848](https://openairdocs.org/sdr/DALA2026031701848.md): Valve · damaged · Mar 16, 2026 · N128DU · Airbus BD5001A10 · Landing Gear Position and Warning
  > MISC / DE CREW DECLARED EMERGENCY DUE TO WOW FAIL CAUTION MSG. FLIGHT SAFELY ON THE GROUND. ON JACKING UP AIRCRAFT, FOUND RT MLG NOT EXTENDING. CHARGE VALVE FOUND INTERNALLY DAMAGED. R/R VALVE ASSEMBLY AND STRUT SEALS. CARRIED OUT GEAR EXTENSION AND RETRACTI
- [SDR DALA2025102907934](https://openairdocs.org/sdr/DALA2025102907934.md): Engine · failed · Oct 27, 2025 · N128DU · Airbus BD5001A10 · Engine (Turbine/Turboprop)
  > SHIP 8128 -IFSD- CREW REPORTED A R ENGINE FAIL ON APPROACH TO SAV. THE R ENGINE DID ROLLBACK AND SHUTDOWN. CORRECTIVE ACTION: R/R ECS IP CHECK VALVE. (LP# 8207183)
- [SDR DALA2025081906213](https://openairdocs.org/sdr/DALA2025081906213.md): Service Panel · corroded · Aug 15, 2025 · N128DU · Airbus BD5001A10 · Fluid Service Doors
  > CORROSION ON WASTE WATER SERVICE PANEL SURROUNDING SKIN CUTOUT, FWD INBOARD CORNER [SSI:53-61-56-02]. GENERATED FOR SCEPTRE ENTRY UPDATE. REMOVED AND REPLACED WASTE SERVICE PANEL INTERNAL DOUBLER IAW ER /A 628360-14AD REV ORIGINAL. WORK ACCOMPLISHED ON CUSTOME
- [SDR DALA2025080705923](https://openairdocs.org/sdr/DALA2025080705923.md): Floor Panel · corroded · Aug 1, 2025 · N128DU · Airbus BD5001A10 · Fuselage Floor Panel
  > CORROSION ON AFT SERVICE DOOR LOWER ENTRY FLOOR PANEL AFT CORNER. REMOVED AND INSTALLED AFT SERVICE DOOR LOWER ENTRY FLOOR PANEL PER A220 AMP BD500-A-J53-00-47-14AAA-720A-A.
- [SDR DALA2025080705922](https://openairdocs.org/sdr/DALA2025080705922.md): Floor Panel · corroded · Aug 1, 2025 · N128DU · Airbus BD5001A10 · Fuselage Floor Panel
  > CORROSION ON AFT SERVICE DOOR LOWER ENTRY FLOOR PANEL AFT CORNER. REMOVED AND INSTALLED AFT SERVICE DOOR LOWER ENTRY FLOOR PANEL PER A220 AMP BD500-A-J53-00-47-14AAA-720A-A.
- [SDR DALA2025080705921](https://openairdocs.org/sdr/DALA2025080705921.md): Floor Panel · corroded · Aug 1, 2025 · N128DU · Airbus BD5001A10 · Fuselage Floor Panel
  > CORROSION ON AFT SERVICE DOOR LOWER ENTRY FLOOR PANEL AFT CORNER. REMOVED AND INSTALLED AFT SERVICE DOOR LOWER ENTRY FLOOR PANEL PER A220 AMP BD500-A-J53-00-47-14AAA-720A-A.
- [SDR DALA2025072905700](https://openairdocs.org/sdr/DALA2025072905700.md): Seat Track · corroded · Jul 24, 2025 · N128DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND CORROSION ON SEAT TRACK FR74 RBL 43. REMOVED AND REPLACED SEAT TRACK AT FR 74 RBL 43 PER BOMBARDIER DWG# PL C01342701 REV G AND A220 ASRP BD500-A-J51-41-02-00AAA-078A-A. (LP# 1105839)
- [SDR DALA2025072405551](https://openairdocs.org/sdr/DALA2025072405551.md): Seat Track · corroded · Jul 21, 2025 · N128DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CORROSION ON SEAT TRACK AT FR20 RBL23. REMOVED AND REPLACED SEAT TRACK RBL25 FR20 TO FR30 IAW A220 ASRP BD500-A-J51-42-21-00AAA-078A-A AND BOMBARDIER DWG# PL C02312600 REV-E. (LP# 1097598)
- [SDR DALA2025072105447](https://openairdocs.org/sdr/DALA2025072105447.md): Seat Track · corroded · Jul 18, 2025 · N128DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND ON SEAT TRACK AT FR74 LBL43. REMOVED AND REPLACED SEAT TRACK LBL43 FR61 TO FR74 IAW BOMBARDIER DWG#C01342701 REV-G AND A220 ASRP BD500-A-J51-42-20- 00AAA-078A-A. (LP# 1092716)
- [SDR DALA2025072105446](https://openairdocs.org/sdr/DALA2025072105446.md): Seat Track · corroded · Jul 17, 2025 · N128DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CORROSION ON SEAT TRACK AT FR74 LBL23. REMOVED AND REPLACED SEAT TRACK FROM FR62 TO FR74 LBL23 IAW A220 ASRP BD500-J51-42-21-00AAA-078A-A AND BOMBARDIER DWG# C01342701 REV-G. (LP# 1090283)
- [SDR DALA2025072105445](https://openairdocs.org/sdr/DALA2025072105445.md): Seat Track · corroded · Jul 16, 2025 · N128DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CORROSION ON SEAT TRACK AT FR20 RBL 43. REMOVED AND REPLACED SEAT TRACK AT RBL 43 BTW FR20 AND FR30 IAW A220 ASRP BD500-A-J51-42-21-00AAA-078A-A AND DWG BOMBARDIER PL C02312600 REV-E. (LP# 1090119)
- [SDR DALA2025071705371](https://openairdocs.org/sdr/DALA2025071705371.md): Seat Track · corroded · Jul 15, 2025 · N128DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CORROSION ON SEAT TRACK AT FR74 RBL 23. REMOVED AND REPLACED SEAT TRACK FROM STA FR 63 +10" TO FR 74 + 10" RBL 23 IAW A220 ASRP BD500-A-J51-42-21-00AAA-078A-A AND BOMBARDIER DWG# C01342701 REV. G. (LP# 1084227)
- [SDR DALA2025052704045](https://openairdocs.org/sdr/DALA2025052704045.md): Valve · sheared · May 23, 2025 · N128DU · Airbus BD5001A10 · Passenger/Crew Doors
  > FOUND EMERGENCY EQUIPMENT, EOAM, PASSENGER SVC DOOR P/N C01519620-009 AIR SERVICING VALVE SHEARED OFF. REMOVED AFT PASSENGER SVC DOOR EOAM P/N C01519620-009 S/N FR0469 IAW A220 AMP 52-12-08. REMOVED AND INSTALLED APD RAIN COVER IAW A220 AMP 52-00-00, REQUIRES
- [SDR DALA2024082008305](https://openairdocs.org/sdr/DALA2024082008305.md): Filter · odor · Aug 20, 2024 · N128DU · Airbus BD5001A10 · Air Distribution System
  > SHIP 8128 - DIV - TO DTW DUE TO DIRTY SOCK SMELL CLIMBING THRU FL250 REPORTED BY FLIGHT CREW AND FLIGHT ATTENDANT. DISSIPATED AFTER 4 MIN. CORRECTIVE ACTION: C/W ODI WORK SCOPE. REPLACED RECIRC FILTERS. (LP# 5782624)
- [SDR DALA2024070106611](https://openairdocs.org/sdr/DALA2024070106611.md): Wire Harness · burned · Jun 17, 2024 · N128DU · Airbus BD5001A10 · Flight Control System Wiring
  > WHILE WORKING MEL 5104106 PRIMARY FLIGHT CONTROL INPUT REDUNDANCY. LOOKING FOR REU ELECTRICAL CONNECTORS. FOUND BURNT WIRES 6IN FROM CONNECTOR A809P1, DIODE SHUNT 1B REU. ACCOMPLISHED TIME LIMITED REPAIR PER ER/A 618850-14 REV. ORIGINAL. PERMANENT REPAIR DUE A
- [SDR DALA2024052305449](https://openairdocs.org/sdr/DALA2024052305449.md): Slat Track · corroded · May 22, 2024 · N128DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 5 UPPER FWN SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NBR 5 UPPER FWD SURFACE PER ER/A 607493- 14AD, REV D AND PRI REV
- [SDR DALA2024052305448](https://openairdocs.org/sdr/DALA2024052305448.md): Slat Track · corroded · May 22, 2024 · N128DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 9 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NBR 9 UPPER FWD SURFACE PER ER/A 607493- 14AD, REV D AND PRI REV
- [SDR DALA2024050204867](https://openairdocs.org/sdr/DALA2024050204867.md): Slide · unknown · Apr 30, 2024 · N128DU · Airbus BD5001A10 · Escape Slide
  > LH OVERWING SLIDE COULD NOT BE PINNED. SLIDE BLOWN MANUALLY. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 000-0002:2563-4002/001 00006 DEPLOYED AND REPLACED SLIDE REF AMDS 2561-9005. (LP# 0320144)
- [SDR DALA2024022702720](https://openairdocs.org/sdr/DALA2024022702720.md): Slat Track · corroded · Feb 25, 2024 · N128DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 10 LOWER FWD O/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 10 LOWER FWD O/B SIDE IAW ER/A 607495 -14AD REV C AND PRI 607493-14AD REV 0 MATCHED. (LP# 0217132)
- [SDR DALA2024022702719](https://openairdocs.org/sdr/DALA2024022702719.md): Slat Track · corroded · Feb 25, 2024 · N128DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 8 UPPER AFT I/B SIDE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. MEASURED LH SLAT TRACK NBR 8 UPPER AFT I/B SIDE IAW ER/A 607495- 14AD REV C AND PRI 607493-14AD REV 0 MATCHED. (LP# 0217130)
- [SDR DALA2024022702718](https://openairdocs.org/sdr/DALA2024022702718.md): Slat Track · corroded · Feb 25, 2024 · N128DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 7 UPPER AFT I/B SIDE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. MEASURED LH SLAT TRACK NBR 7 UPPER AFT I/B SIDE IAW ER/A 607495- 14AD REV C AND PRI 607493-14AD REV 0 MATCHED. (LP# 0217128)
- [SDR DALA2024022702717](https://openairdocs.org/sdr/DALA2024022702717.md): Slat Track · corroded · Feb 25, 2024 · N128DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 6 LOWER FWD O/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 6 LOWER FWD O/B SIDE IAW ER/A 607495- 14AD REV C AND PRI 607493-14AD REV 0 MATCHED. (LP# 0217126)
- [SDR DALA2024022702716](https://openairdocs.org/sdr/DALA2024022702716.md): Slat Track · corroded · Feb 25, 2024 · N128DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 6 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 6 UPPER AFT SURFACE IAW ER/A 607495- 14AD REV C AND PRI 607493-14AD REV 0 MATCHED. (LP# 0217123)
- [SDR DALA2024022702715](https://openairdocs.org/sdr/DALA2024022702715.md): Slat Track · corroded · Feb 25, 2024 · N128DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION IN TWO LOCATIONS AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 5 UPPER FWD SURFACE IAW ER/A 607495- 14AD REV C AND PRI 607493-14AD REV 0 MATCHED. (LP# 0217113)
- [SDR DALA2024022702714](https://openairdocs.org/sdr/DALA2024022702714.md): Slat Track · corroded · Feb 25, 2024 · N128DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 4 UPPER AFT I/B SIDE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. MEASURED LH SLAT TRACK NBR 4 UPPER AFT I/B SIDE IAW ER/A 607495- 14AD REV C AND PRI 607493-14AD REV 0 MATCHED. (LP# 0217110)
- [SDR DALA2024022702713](https://openairdocs.org/sdr/DALA2024022702713.md): Slat Track · corroded · Feb 25, 2024 · N128DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 4 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 4 UPPER AFT SURFACE IAW ER/A 607495- 14AD REV C AND PRI 607493-14AD REV 0 MATCHED. (LP# 0217107)
- [SDR DALA2024022702712](https://openairdocs.org/sdr/DALA2024022702712.md): Slat Track · corroded · Feb 25, 2024 · N128DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 3 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 3 UPPER FWD SURFACE IAW ER/A 607495- 14AD REV C AND PRI 607493-14AD REV 0 MATCHED. (LP# 0217106)
- [SDR DALA2024022702711](https://openairdocs.org/sdr/DALA2024022702711.md): Slat Track · corroded · Feb 25, 2024 · N128DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 2 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 2 UPPER FWD SURFACE IAW ER/A 607495- 14AD REV C AND PRI 607493-14AD REV 0 MATCHED. (LP# 0217105)
- [SDR DALA2024022702710](https://openairdocs.org/sdr/DALA2024022702710.md): Slat Track · corroded · Feb 25, 2024 · N128DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 1 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 1 UPPER FWD SURFACE IAW ER/A 607495- 14AD REV C AND PRI 607493-14AD REV 0 MATCHED. (LP# 0217103)
- [SDR DALA2024022702709](https://openairdocs.org/sdr/DALA2024022702709.md): Slat Track · corroded · Feb 25, 2024 · N128DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 8 LOWER I/B FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 8 LOWER I/B FWD SURFACE IAW ER/A 607493-14AD REV C AND PRI 607493-14AD REV 0 MATCHED. (LP# 0217011)
- [SDR DALA2024022702708](https://openairdocs.org/sdr/DALA2024022702708.md): Slat Track · corroded · Feb 25, 2024 · N128DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 7 LOWER O/B FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 7 LOWER O/B FWD SURFACE IAW ER/A 607493-14AD REV C AND PRI 607493-14AD REV 0 MATCHED. (LP# 0217009)
- [SDR DALA2024022702707](https://openairdocs.org/sdr/DALA2024022702707.md): Slat Track · corroded · Feb 25, 2024 · N128DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 6 LOWER O/B FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 6 LOWER O/B FWD SURFACE IAW ER/A 607493-14AD REV C AND PRI 607493-14AD REV 0 MATCHED. (LP# 0217006)
- [SDR DALA2024022702706](https://openairdocs.org/sdr/DALA2024022702706.md): Slat Track · corroded · Feb 24, 2024 · N128DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 6 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 6 LOWER AFT SURFACE IAW ER/A 607493- 14AD REV C AND PRI 607493-14AD REV 0 MATCHED. (LP# 0217000)
- [SDR DALA2024022702705](https://openairdocs.org/sdr/DALA2024022702705.md): Slat Track · corroded · Feb 24, 2024 · N128DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 4 UPPER FWD SURFACE IAW ER/A 607493- 14AD REV C AND PRI 607493-14AD REV 0 MATCHED. (LP# 0216998)
- [SDR DALA2024022702704](https://openairdocs.org/sdr/DALA2024022702704.md): Slat Track · corroded · Feb 24, 2024 · N128DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 3 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 3 UPPER FWD SURFACE IAW ER/A 607493- 14AD REV C AND PRI 607493-14AD REV 0 MATCHED. (LP# 0216995)
- [SDR DALA2024022702703](https://openairdocs.org/sdr/DALA2024022702703.md): Slat Track · corroded · Feb 24, 2024 · N128DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 2 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 2 UPPER FWD SURFACE IAW ER/A 607493- 14AD REV C AND PRI 607493-14AD REV 0 MATCHED. (LP# 0216992)
- [SDR DALA2024022702702](https://openairdocs.org/sdr/DALA2024022702702.md): Slat Track · corroded · Feb 24, 2024 · N128DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 1 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 1 UPPER FWD SURFACE IAW ER/A 607493- 14AD REV C AND PRI 607493-14AD REV 0 MATCHED. (LP# 0216990)
- [SDR DALA2023092607919](https://openairdocs.org/sdr/DALA2023092607919.md): Unknown · unknown · Sep 22, 2023 · N128DU · Airbus BD5001A10 · Leading Edge Devices
  > REF AMDS 5742-01028-02A L/H SLAT TRACK 11 FOUND WITH ROLLER WEAR ON (LOWER AFT) SURFACE. NO EVIDENCE OF PREVIOUS REWORK NOTED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 002-0001:5742-01028-02A/010 00020 ACCOMPLISHED
- [SDR DALA2023092607918](https://openairdocs.org/sdr/DALA2023092607918.md): Unknown · unknown · Sep 22, 2023 · N128DU · Airbus BD5001A10 · Leading Edge Devices
  > REF AMDS 5742-01028-02A L/H SLAT TRACK 9 FOUND WITH ROLLER WEAR ON (LOWER AFT) SURFACE. EVIDENCE OF PREVIOUS REWORK NOTED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 002-0001:5742-01028-02A/009 00019 ACCOMPLISHED PRI
- [SDR DALA2023092607917](https://openairdocs.org/sdr/DALA2023092607917.md): Unknown · unknown · Sep 22, 2023 · N128DU · Airbus BD5001A10 · Leading Edge Devices
  > REF AMDS 5742-01028-02A L/H SLAT TRACK 8 FOUND WITH ROLLER WEAR ON (UPPER AFT), (LOWER AFT), (UPPER INBD) SURFACES. NO EVIDENCE OF PREVIOUS REWORK NOTED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 002-0001:5742-01028-
- [SDR DALA2023092607916](https://openairdocs.org/sdr/DALA2023092607916.md): Unknown · unknown · Sep 22, 2023 · N128DU · Airbus BD5001A10 · Leading Edge Devices
  > REF AMDS 5742-01028-02A L/H SLAT TRACK 7 FOUND WITH ROLLER WEAR ON (UPPER AFT), (LOWER AFT), (UPPER INBD), (LOWER INBD), (UPPER OTBD) SURFACES. EVIDENCE OF PREVIOUS REWORK NOTED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMA
- [SDR DALA2023092607915](https://openairdocs.org/sdr/DALA2023092607915.md): Unknown · unknown · Sep 22, 2023 · N128DU · Airbus BD5001A10 · Leading Edge Devices
  > REF AMDS 5742-01028-02A L/H SLAT TRACK 6 FOUND WITH ROLLER WEAR ON (LOWER AFT) SURFACE. EVIDENCE OF PREVIOUS REWORK NOTED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 002-0001:5742-01028-02A/006 00016 ACCOMPLISHED PRI
- [SDR DALA2023092607914](https://openairdocs.org/sdr/DALA2023092607914.md): Unknown · unknown · Sep 22, 2023 · N128DU · Airbus BD5001A10 · Leading Edge Devices
  > REF AMDS 5742-01028-02A L/H SLAT TRACK 5 FOUND WITH ROLLER WEAR ON (UPPER AFT), (LOWER AFT), (LOWER OTBD), (LOWER INBD) SURFACES. EVIDENCE OF PREVIOUS REWORK NOTED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 002-0001
- [SDR DALA2023092607913](https://openairdocs.org/sdr/DALA2023092607913.md): Unknown · unknown · Sep 22, 2023 · N128DU · Airbus BD5001A10 · Leading Edge Devices
  > REF AMDS 5742-01028-02A L/H SLAT TRACK 4 FOUND WITH ROLLER WEAR ON (UPPER AFT), (UPPER FORWARD), (LOWER AFT), (LOWER OTBD), ( LOWER INBD) SURFACES. EVIDENCE OF PREVIOUS REWORK NOTED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INF
- [SDR DALA2023092607912](https://openairdocs.org/sdr/DALA2023092607912.md): Unknown · unknown · Sep 22, 2023 · N128DU · Airbus BD5001A10 · Leading Edge Devices
  > REF AMDS 5742-01028-02A L/H SLAT TRACK 3 FOUND WITH ROLLER WEAR ON (LOWER AFT) SURFACE. EVIDENCE OF PREVIOUS REWORK NOTED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 002-0001:5742-01028-02A/003 00013 ACCOMPLISHED PRI
- [SDR DALA2023092607911](https://openairdocs.org/sdr/DALA2023092607911.md): Unknown · unknown · Sep 22, 2023 · N128DU · Airbus BD5001A10 · Leading Edge Devices
  > REF AMDS 5742-01028-02A L/H SLAT TRACK 2 FOUND WITH ROLLER WEAR ON (LOWER AFT), (LOWER INBD) SURFACES. EVIDENCE OF PREVIOUS REWORK NOTED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 002-0001:5742-01028-02A/002 00012 AC
- [SDR DALA2023092607910](https://openairdocs.org/sdr/DALA2023092607910.md): Unknown · unknown · Sep 22, 2023 · N128DU · Airbus BD5001A10 · Leading Edge Devices
  > REF AMDS 5742-01028-02A L/H SLAT TRACK 1 FOUND WITH ROLLER WEAR (LOWER AFT) SURFACE. EVIDENCE OF PREVIOUS REWORK NOTED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 002-0001:5742-01028-02A/001 00011 ACCOMPLISHED PRI 607
- [SDR DALA2023081506633](https://openairdocs.org/sdr/DALA2023081506633.md): Unknown · unknown · Aug 9, 2023 · N128DU · Airbus BD5001A10 · Fuselage Structure (General)
  > PERFORMED AD RELATED INSPECTION WC 5352-01038-01A. FOUND CRACK ON LONGERON (P/N 53-1111-502) RT, STARTING 16" FROM FWD EDGE RUNNING AFT FOR APPROX. 16". REMOVED LONGERON WIP 234225. REPLACED RH LONGERON IAW AMDS WORKCARD 5352-01038-07B. (LP# 2908918)

## 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 = 'N128DU' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N128DU/reports

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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.