# Service difficulty reports: N119DU

A list on [N119DU](https://openairdocs.org/aircraft/N119DU.md).

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

Page 1 of 2 · 90 reports

- [SDR DALA2026082704868](https://openairdocs.org/sdr/DALA2026082704868.md): Light · inoperative · Aug 25, 2026 · N119DU · Airbus BD5001A10 · Emergency Lighting
  > LEFT FWD OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LT FWD OVER WING EMERGENCY LIGHT IAW AMP 33-54. OPS CHKD GOOD. (LP 9156229; AIRCRAFT WAS GROUNDED)
- [SDR DALA2025053104188](https://openairdocs.org/sdr/DALA2025053104188.md): Support Frame · corroded · May 30, 2025 · N119DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > AIRCRAFT 8119, WTBF SUPPORT FRAME AT FR 36 LH CORRODED AT BL0. CORRECTIVE ACTION: REPLACED DAMAGED WTBF SUPPORT FRAME AT FR36 L/H IAW A220 ASRP J51-42-21. (LP 0996394)
- [SDR DALA2025052904135](https://openairdocs.org/sdr/DALA2025052904135.md): Support Frame · corroded · May 28, 2025 · N119DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > AIRCRAFT 8119, WTBF SUPPORT FRAME AT FR 36 RH LEVEL 2 CORRODED AT BL0. CORRECTIVE ACTION: REPLACED WTBF SUPPORT FRAME AT R/H FR36 IAW A220 ASRP J51-42-21. (LP 0991442)
- [SDR DALA2025052804101](https://openairdocs.org/sdr/DALA2025052804101.md): Paint · missing · May 27, 2025 · N119DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > FWD CARGO DOOR LWR CUTOUT FROM FR24 - FR29, HAS FASTENER HOLES WITH MISSING PAINT. ( TASK CARD 5331-01297-01C) LOG-PAGE UPDATED @ 27MAY25 1136 UTC 02 CORR BY ARANDA 01865357 MLB 27MAY25 ATA 5331 RII: N ENTR 01531485 W REMOVED CORROSION, EVALUATED DAMAGE ON FW
- [SDR DALA2025052704047](https://openairdocs.org/sdr/DALA2025052704047.md): Skin · corroded · May 24, 2025 · N119DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > FWD CARGO DOOR SILL HAS EXTERIOR SKIN CORROSION AT HOLES 12OL, 14OL, 18OL, 19OL, & 20OL. REMOVED CORROSION, EVALUATED DAMAGE ON FWD CARGO DOOR LWR SILL, FOUND OUT OF LIMITS IAW A220 ASRP J51-21-06, J53-21-01, RESTORE FINISH, ALL WORK ACCOMPLISHED IAW DELTA ERA
- [SDR DALA2025052704046](https://openairdocs.org/sdr/DALA2025052704046.md): Skin · corroded · May 24, 2025 · N119DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > FWD CARGO DOOR, AT HOLE 22 OL, FUSELAGE EXTERIOR SKIN HAS CORROSION. (TASK CARD 5331-01297-01C). REMOVED CORROSION, EVALUATED DAMAGE ON FWD CARGO DOOR LWR SKIN AREA, FOUND OUT OF LIMITS IAW A220 ASRP J51-21-06, J53-21-01. RESTORED FINISH, ALL WORK ACCOMPLISHED
- [SDR DALA2025052704037](https://openairdocs.org/sdr/DALA2025052704037.md): Skin · corroded · May 21, 2025 · N119DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > FWD PASSENGER DOOR, EXTERIOR FUSELAGE SKIN, @ HOLE LOCATION 8QL HAS CORROSION ON THE AIRCRAFT SKIN. ( TASK CARD 5331-01297-01A). REMOVED CORROSION, EVALUATED DAMAGE AREA, FOUND OUT OF LIMITS ON FWD PAX DOOR EXTERIOR FUSELAGE SKIN IAW A220 ASRP J51-21-06, J53-
- [SDR DALA2025052704036](https://openairdocs.org/sdr/DALA2025052704036.md): Skin · corroded · May 21, 2025 · N119DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > FWD PASSENGER DOOR, EXTERIOR FUSELAGE SKIN, @ HOLE LOCATION 2QL HAS CORROSION ON THE AIRCRAFT SKIN. (TASK CARD 5331-01297-01A). REMOVED CORROSION, EVALUATED DAMAGE AREA, FOUND OUT OF LIMITS ON FWD PAX/L1 DOOR CUTOUT IAW A220 ASRP J51-21-06, J53-21-01. RESTORED
- [SDR DALA2025052704034](https://openairdocs.org/sdr/DALA2025052704034.md): Scuff Plate · corroded · May 20, 2025 · N119DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > AFT PAX DOOR (L2) SILL SCUFF PLATE AREA HAS EXTERNAL SKIN CORROSION AT HOLES 3OL, 4OL, 5OL, 8OL, 10OL, 11OL, & 12OL. REMOVED CORROSION, EVALUATED DAMAGE ON AFT PAX DOOR SCUFF PLATE AREA, FOUND OUT OF LIMITS IAW A220 ASRP J51-21-06, J53-62-33. RESTORED FINISH A
- [SDR DALA2025052704033](https://openairdocs.org/sdr/DALA2025052704033.md): Door Sill · corroded · May 20, 2025 · N119DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > SSI: 53-61-24-02 R2 PAX DOOR SILL. CORROSION AT FASTENER HOLE 1/16 INCH IN LENGTH, 1/18 INCH WIDE AT FR 75. REMOVED CORROSION, EVALUATED DAMAGE AREA OF R2 PAX DOOR SILL, FOUND OUT OF LIMITS IAW A220 ASRP J51-21-06, J53-61-24. RESTORE FINISH AND PERFORMED CO
- [SDR DALA2025052003858](https://openairdocs.org/sdr/DALA2025052003858.md): Seat Track · corroded · May 15, 2025 · N119DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > FWD SEAT TRACK RIGHT OUTBOARD @ LOCATION FR20 HAS CORROSION. REMOVED CORROSION FOUND WITHOUT LIMITS. REMOVED AND REPLACED SEAT TRACK FWD R/H O/B FR 20 IAW A220 J53-21-49-00-AAA-661A-A, J52-42-21-00AAA-078A-A, J51-40-11-01AAA-652A-A. (LP# 0967902)
- [SDR DALA2025051403744](https://openairdocs.org/sdr/DALA2025051403744.md): Support · corroded · May 10, 2025 · N119DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > PRODUCTION REQUEST: RH SIDE WTBF SUPPORT AT FR48 HAS CORROSION. REMOVED CORROSION ON FR48 R/H WTBF SUPPORT FRAME IAW A220 ASRP J51-21-06. REMOVED AND REPLACE SUPPORT FRAME IAW A220 ASRP J51- 42-20. (LP# 0959651)
- [SDR DALA2025051303711](https://openairdocs.org/sdr/DALA2025051303711.md): Seat Track · corroded · May 8, 2025 · N119DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > FWD SEAT TRACK RIGHT OUTBOARD @ LOCATION FR20 HAS CORROSION. REMOVED CORROSION FOUND WITHOUT LIMITS. REMOVED AND REPLACED SEAT TRACK FWD R/H O/B FR 20 IAW A220 J53-21-49-00-AAA-661A-A, J52-42-21-00AAA-078A-A, J51-40-11-01AAA-652A-A. (LP# 0955967)
- [SDR DALA2025050803577](https://openairdocs.org/sdr/DALA2025050803577.md): Frame · corroded · May 5, 2025 · N119DU · Airbus BD5001A10 · Fuselage Main, Frame
  > BELLY FRAME 48 HAS CORROSION AT STR 0 AROUND NUT PLATES. REMOVED CORROSION IAW A220-100 ASRP 51-21-06, FOUND BEYOND LIMITS IAW A220-100 ASRP 53-82-55, CUSTOMER WANTS FRAME REPLACED TO AVOID REPETITIVE INSP. REMOVED & REPLACED WTBF STRUCTURE L/H AT FR48 IAW A22
- [SDR DALA2025042403235](https://openairdocs.org/sdr/DALA2025042403235.md): Seat Track · corroded · Apr 24, 2025 · N119DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AFT SEAT TRACK LEFT INBOARD @ LOCATION FR74 HAS CORROSION. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW A220 ASRP J51-21- 06 AND J53-42-49. REMOVED AND REPLACED AFT L/H INBD SEAT TRACK IAW A220 ASRP J51-40-11 AND J51-42-21. (LP# 0929800)
- [SDR DALA2025042403234](https://openairdocs.org/sdr/DALA2025042403234.md): Seat Track · corroded · Apr 23, 2025 · N119DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > FWD SEAT TRACK RIGHT INBOARD @ LOCATION FR20 HAS CORROSION. REMOVED CORROSION IAW A220 ASRP J51-21-06, FOUND OUT OF LIMITS IAW A220 ASRP J53-21-49, REMOVED AND REPLACED SEAT TRACK IAW A220 ASRP J51-40-11 AND J51-42-20. (LP# 0929336)
- [SDR DALA2025042403233](https://openairdocs.org/sdr/DALA2025042403233.md): Seat Track · corroded · Apr 23, 2025 · N119DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AFT SEAT TRACK RIGHT INBOARD @ LOCATION FR74 HAS CORROSION. REMOVED CORROSION IAW A220 ASRP J51-21-06, FOUND OUT OF LIMITS IAW A220 ASRP J53-61-49, REMOVED AND REPLACED AFT R/H INBD SEAT TRACK IAW A220 ASRP 51-40-11 AND J51-42-21. (LP# 0929334)
- [SDR DALA2025042403232](https://openairdocs.org/sdr/DALA2025042403232.md): Seat Track · corroded · Apr 23, 2025 · N119DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AFT SEAT TRACK LEFT OUTBOARD @ LOCATION FR74 HAS CORROSION. REMOVED CORROSION IAW A220 ASRP J51-21-06, FOUND OUT OF LIMITS IAW A220 ASRP J53-61-49, REMOVED AND REPLACED AFT L/H OUTBOARD SEAT TRACK IAW A220 ASRP J51-40-11 AND J51-42-21. (LP# 0929331)
- [SDR DALA2025042403230](https://openairdocs.org/sdr/DALA2025042403230.md): Seat Track · corroded · Apr 22, 2025 · N119DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AFT SEAT TRACK RIGHT OUTBOARD @ LOCATION FR74 HAS CORROSION. REMOVED CORROSION ON AFT R/H OUTBOARD SEAT TRACK IAW A220 ASRP J51- 21-06, FOUND OUT OF LIMITS IAW ASRP J53-61-49. REMOVED AND REPLACED SEAT TRACK IAW A220 ASRP J51-40-11 AND J 51-42-02. (LP# 0927266
- [SDR DALA2025042203163](https://openairdocs.org/sdr/DALA2025042203163.md): Seat Track · corroded · Apr 17, 2025 · N119DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > FWD SEAT TRACK LEFT OUTBOARD @ LOCATION FR22 HAS CORROSION. REMOVED CORROSION FOUND OUT OF LIMITS, REMOVED AND REPLACED SEAT TRACK AT FR22 R/H O/B IAW A220-J53-21-49-00-AAA661A-A, J51-42- 21-00AAA-078A-A, J51-40-11-01AAA-652A-A, J53-21-49-00AAA-041A-A. (LP# 09
- [SDR DALA2025060504287](https://openairdocs.org/sdr/DALA2025060504287.md): Tape · damaged · Sep 3, 2024 · N119DU · Airbus BD5001A10 · Vertical Stabilizer, Plate/Skin
  > VERTICAL STABILIZER LEADING EDGE EROSION TAPE FOUND DAMAGED. INSPECTED VERTICAL STABILIZER LEADING EDGE EROSION TAPE AND FOUND NO UNDERLYING DAMAGE. TRIMMED OFF EXCESS EROSION BOOT MATERIAL TO MEET AERODYNAMIC SMOOTHNESS IAW A220 ASRP 55-32-01- 01AAA-662A-A. F
- [SDR DALA2024090408717](https://openairdocs.org/sdr/DALA2024090408717.md): Slat Track · corroded · Aug 30, 2024 · N119DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 3 UPPER AFT SURFACE FOUND WITH CORROSION AND BLENDED PER AMDS W/C 5742-01028-02B, REQUIRES NDT INSPECTION TO CHECK FOR SIGNS OF CRACKS. REMOVED RH SLAT TRACK NBR 3 UPPER AFT SURFACE CORRSION BY BLENDING PER AMDS W/C 5742-01028-02B. J.HENDRICK
- [SDR DALA2024090408716](https://openairdocs.org/sdr/DALA2024090408716.md): Slat Track · corroded · Aug 30, 2024 · N119DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 5 UPPER AFT SURFACE FOUND WITH CORROSION AND BLENDED PER AMDS W/C 5742-01028-02A, REQUIRES NDT INSPECTION TO CHECK FOR SIGNS OF CRACKS. REMOVED LH SLAT TRACK NBR 5 UPPER AFT SURFACE CORROSION BY BLENDING PER AMDS W/C 5742-01028-02A. J.HENDRIC
- [SDR DALA2024090408715](https://openairdocs.org/sdr/DALA2024090408715.md): Slat Track · corroded · Aug 30, 2024 · N119DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 2 UPPER AFT SURFACE FOUND WITH CORROSION AND BLENDED PER AMDS W/C 5742-01028-02A, REQUIRES NDT INSPECTION TO CHECK FOR SIGNS OF CRACKS. REMOVED LH SLAT TACK NBR 2 UPPER AFT SURFACE CORROSION BY BLENDING PER AMDS W/C 5742-01028-02A. J.HENDRICK
- [SDR DALA2024090408714](https://openairdocs.org/sdr/DALA2024090408714.md): Slat Track · corroded · Aug 30, 2024 · N119DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 1 UPPER AFT SURFACE FOUND WITH CORROSION AND BLENDED PER AMDS W/C 5742-01028-02A, REQUIRES NDT INSPECTION TO CHECK FOR SIGNS OF CRACKS. REMOVED LH SLAT TRACK NBR 1 UPPER AFT SURFACE CORROSION BY BLENDING PER AMDS W/C 5742-01028-02A. J.HENDRIC
- [SDR DALA2024020801742](https://openairdocs.org/sdr/DALA2024020801742.md): Slat System · corroded · Feb 5, 2024 · N119DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 3 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-2B. REPAIRED RH SLAT TRACK NBR 3 LOWER AFT SURFACE IAW ER/A 607714- 14AD REV B AND PRI REV 0 MATCHED. (LP# 0187621)
- [SDR DALA2024020801741](https://openairdocs.org/sdr/DALA2024020801741.md): Slat System · corroded · Feb 5, 2024 · N119DU · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 3 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028-02B. REPAIRED R/H SLAT TRACK NBR 3 UPPER FWD SURFACE IAW PRI 607714- 14AD REV 0 AND ERA REV B MATCHED. (LP# 0187620)
- [SDR DALA2024020801740](https://openairdocs.org/sdr/DALA2024020801740.md): Slat System · corroded · Feb 5, 2024 · N119DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-2B. REPAIRED RH SLAT TRACK NBR 4 UPPER AFT SURFACE IAW ER/A 607714- 14AD REV B AND PRI REV 0 MATCHED. (LP# 0187619)
- [SDR DALA2024020801739](https://openairdocs.org/sdr/DALA2024020801739.md): Slat System · corroded · Feb 5, 2024 · N119DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 6 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 6 LOWER AFT SURFACE IAW PRI 607715- 14AD REV 0 AND ERA REV B MATCHED. (LP# 0187617)
- [SDR DALA2024020801738](https://openairdocs.org/sdr/DALA2024020801738.md): Slat System · corroded · Feb 5, 2024 · N119DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-2B. REPAIRED RH SLAT TRACK NBR 4 UPPER FWD SURFACE IAW ER/A 607714- 14AD REV B AND PRI REV 0 MATCHED. (LP# 0187616)
- [SDR DALA2024020801737](https://openairdocs.org/sdr/DALA2024020801737.md): Slat System · corroded · Feb 5, 2024 · N119DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 7 UPPER IBD AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 7 UPPER IBD AFT SURFACE IAW PRI 607715-14AD REV 0 AND ERA REV B MATCHED. (LP# 0187615)
- [SDR DALA2024020801736](https://openairdocs.org/sdr/DALA2024020801736.md): Slat System · corroded · Feb 5, 2024 · N119DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-2B. REPAIRED RH SLAT TRACK NBR 4 LOWER AFT SURFACE IAW ER/A 607714- 14AD REV B AND PRI REV 0 MATCHED. (LP# 0187611)
- [SDR DALA2024020801735](https://openairdocs.org/sdr/DALA2024020801735.md): Slat System · corroded · Feb 5, 2024 · N119DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 7 LWR IBD FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 7 LWR IBD FWD SURFACE IAW PRI 607715- 14AD REV 0 AND ERA REV B MATCHED. (LP# 0187610)
- [SDR DALA2024020801734](https://openairdocs.org/sdr/DALA2024020801734.md): Slat System · corroded · Feb 5, 2024 · N119DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 5 LWR IB FWD SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-2B. REPAIRED RH SLAT TRACK NBR 5 LOWER IB FWD SIDE IAW ER/A 607714- 14AD REV B AND PRI REV 0 MATCHED. (LP# 0187608)
- [SDR DALA2024020801733](https://openairdocs.org/sdr/DALA2024020801733.md): Slat System · corroded · Feb 5, 2024 · N119DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 7 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 7 UPPER FWD SURFACE IAW PRI 607715- 14AD REV 0 AND ERA REV B MATCHED. (LP# 0187603)
- [SDR DALA2024020801732](https://openairdocs.org/sdr/DALA2024020801732.md): Slat System · corroded · Feb 5, 2024 · N119DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 5 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK AT 2 LOCATIONS, REF 5742-01028-2B. REPAIRED RH SLAT TRACK NBR 5 UPPER AFT SURFACE AT 2 LOCATIONS IAW ER/A 607714-14AD REV B AND PRI REV 0 MATCHED. (LP# 0187601)
- [SDR DALA2024020801731](https://openairdocs.org/sdr/DALA2024020801731.md): Slat System · corroded · Feb 5, 2024 · N119DU · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 2 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028-02B. REPAIRED R/H SLAT TRACK NBR 11 LOWER AFT SURFACE IAW PRI 607714- 14AD REV 0 AND ERA REV B MATCHED. (LP# 0187599)
- [SDR DALA2024020801730](https://openairdocs.org/sdr/DALA2024020801730.md): Slat System · corroded · Feb 5, 2024 · N119DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 8 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 8 UPPER FWD SURFACE IAW PRI 607715- 14AD REV 0 AND ERA REV B MATCHED. (LP# 0187597)
- [SDR DALA2024020801729](https://openairdocs.org/sdr/DALA2024020801729.md): Slat System · corroded · Feb 5, 2024 · N119DU · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 2 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028-02B. REPAIRED R/H SLAT TRACK NBR 2 LOWER AFT SURFACE IAW PRI 607714- 14AD REV 0 AND ERA REV B MATCHED. (LP# 0187595)
- [SDR DALA2024020801728](https://openairdocs.org/sdr/DALA2024020801728.md): Slat System · corroded · Feb 5, 2024 · N119DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 9 LWR IBD FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 9 LWR IBD FWD SURFACE IAW PRI 607715- 14AD REV 0 AND ERA REV B MATCHED. (LP# 0187593)
- [SDR DALA2024020801727](https://openairdocs.org/sdr/DALA2024020801727.md): Slat System · corroded · Feb 5, 2024 · N119DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 5 LOWER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-2B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 05FEB24 0434 UTC 02 CORR BY HENDRICK 02372882 IAH 05FEB24 ATA 5742 RI
- [SDR DALA2024020801726](https://openairdocs.org/sdr/DALA2024020801726.md): Slat System · corroded · Feb 5, 2024 · N119DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 9 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 9 LOWER AFT SURFACE IAW PRI 607715- 14AD REV 0 AND ERA REV B MATCHED. (LP# 0187589)
- [SDR DALA2024020801725](https://openairdocs.org/sdr/DALA2024020801725.md): Slat System · corroded · Feb 5, 2024 · N119DU · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 8 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028-02B. REPAIRED R/H SLAT TRACK NBR 8 UPPER AFT SURFACE IAW PRI 607714- 14AD REV 0 AND ERA REV B MATCHED. (LP# 0187584)
- [SDR DALA2024020801724](https://openairdocs.org/sdr/DALA2024020801724.md): Slat System · corroded · Feb 5, 2024 · N119DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 6 LOWER OB FWD SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-2B. REPAIRED RH SLAT TRACK NBR 6 LOWER OB FWD SIDE IAW ER/A 607714- 14AD REV B AND PRI REV 0 MATCHED. (LP# 0187579)
- [SDR DALA2024020801723](https://openairdocs.org/sdr/DALA2024020801723.md): Slat System · corroded · Feb 5, 2024 · N119DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 11 LWR IBD FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 11 LWR IBD FWD SURFACE IAW PRI 607715 -14AD REV 0 AND ERA REV B MATCHED. (LP# 0187577)
- [SDR DALA2024020801722](https://openairdocs.org/sdr/DALA2024020801722.md): Slat System · corroded · Feb 5, 2024 · N119DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 6 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-2B. REPAIRED RH SLAT TRACK NBR 6 UPPER AFT SURFACE IAW ER/A 607714- 14AD REV B AND PRI REV 0 MATCHED.
- [SDR DALA2024020801721](https://openairdocs.org/sdr/DALA2024020801721.md): Slat System · corroded · Feb 5, 2024 · N119DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 11 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 11 LOWER AFT SURFACE IAW PRI 607715- 14AD REV 0 AND ERA REV B MATCHED. (LP# 0187569)
- [SDR DALA2024020801720](https://openairdocs.org/sdr/DALA2024020801720.md): Slat System · corroded · Feb 5, 2024 · N119DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 3 LWR IBD FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 05FEB24 0426 UTC 02 CORR BY COBB 01831429 IAH 05FEB24 ATA 5742 RII:
- [SDR DALA2024020801719](https://openairdocs.org/sdr/DALA2024020801719.md): Slat System · corroded · Feb 5, 2024 · N119DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 6 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-2B. LIAISON ENGINEERING LOG-PAGE UPDATED @ 05FEB24 0426 UTC 02 CORR BY HENDRICK 02372882 IAH 05FEB24 ATA 5742 RII: N ENTR 02372882 W REPAIRED RH SLAT TRACK NBR
- [SDR DALA2024020801718](https://openairdocs.org/sdr/DALA2024020801718.md): Slat System · corroded · Feb 5, 2024 · N119DU · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 9 LOWER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF AA5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 05FEB24 0425 UTC 02 CORR BY EASTMAN 01895233 IAH 05FEB24 ATA 5742

Next page: https://openairdocs.org/aircraft/N119DU/reports.md?page=2

## 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 = 'N119DU' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N119DU/reports

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