# Service difficulty reports: N129DU

A list on [N129DU](https://openairdocs.org/aircraft/N129DU.md).

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

- [SDR DALA2026092405345](https://openairdocs.org/sdr/DALA2026092405345.md): Hose · leaking · Sep 17, 2026 · N129DU · Airbus BD5001A10 · Hydraulic System, Main
  > DIRTY SOCK ODOR IN AFT GALLEY AFTER TAKEOFF, DIRTY SOCK ODOR IN COCKPIT DURING DECENT AND LANDING. CREW REPORTED ODOR ON DESCENT STARTED AT 9000 FT. PAX COMPLAINED OF ODOR AS WELL WIP362362. WHILE CHANGING BUFFER AIR SOV OF NR 1 ENG, FOUND FLUID LEAKING FROM H
- [SDR DALA2026080404486](https://openairdocs.org/sdr/DALA2026080404486.md): Hydraulic Line · leaking · Aug 1, 2026 · N129DU · Airbus BD5001A10 · Hydraulic System, Main
  > SHORT LIVED OIL FUME ODOR OBSERVED DURING FINAL DESCENT. ODOR DISSIPATED QUICKLY ONLY PRESENT IN-FLT DECK. INSPECTED NR 1 ENG FOR LEAKS IAW AMP 72-00 FOUND AIR/OIL COOLER LEAK OIL W/BUILD UP OIL RESIDUE ON EXIT SIDE. ALSO FOUND QUICK DISCONNECT FOR HYD LINE LE
- [SDR DALA2026012100454](https://openairdocs.org/sdr/DALA2026012100454.md): Fire Bottle · faulted · Jan 19, 2026 · N129DU · Airbus BD5001A10 · Extinguishing System
  > DIVERTED TO SLC DUE TO CARGO BTL FAIL MESSAGE. PERFORMED RESISTANCE CHECKS OF WIRING FROM THE FIDEX TO THE CARGO BOTTLE AND PRESSURE SWITCH, FOUND RESISTANCE FLUCTUATING IN BOTTLE PRESSURE SWITCH WHEN TAPPING ON THE BOTTLE PRESSURE SWITCH, REPLACED LOW-RATE D
- [SDR DALA2026012700645](https://openairdocs.org/sdr/DALA2026012700645.md): Fire Bottle · failed · Jan 18, 2026 · N129DU · Airbus BD5001A10 · Extinguishing System
  > DIVERTED TO DFW DUE TO CARGO BTL FAIL MESSAGE. REPLACED THE LOW-RATE DISCHARGE (LRD) FIRE EXTINGUISHING BOTTLE 1. (LP# 8025421)
- [SDR DALA2025123109552](https://openairdocs.org/sdr/DALA2025123109552.md): Seat Track · corroded · Dec 30, 2025 · N129DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN RT OUTBOARD SEAT TRACK BETWEEN FR48-FR49 HAS EVIDENCE OF CORROSION. REPLACED RT OTBD SEAT TRACK BETWEEN FR48 TO FR49 IAW 51-42-20 AND E.R.A. 630524-14 PRI REV. 3. (LP 1377517)
- [SDR DALA2026020900940](https://openairdocs.org/sdr/DALA2026020900940.md): Door Sill · corroded · Dec 23, 2025 · N129DU · Airbus BD5001A10 · Fuselage Main, Structure
  > AMOC / MONITOR INSPECTION LOG REF 630257-14AD, FWD FUSELAGE, FWD CARGO DOOR SURROUND STRUCTURE SILL BTWN FR 25 - 28. SUBJECT REPAIR REQUIRES ADDITIONAL ENGINEERING APPROVAL. REPAIR APPROVAL IS LIMITED TO 40,600 TOTAL FLT HRS OR 20,300 TOTAL ACFT FLT CYCLES
- [SDR DALA2026011400340](https://openairdocs.org/sdr/DALA2026011400340.md): Door Sill · corroded · Dec 15, 2025 · N129DU · Airbus BD5001A10 · Fuselage Main, Structure
  > ER/A 630257-14; A220-100 / FWD FUSELAGE / FWD CARGO DOOR / SURROUND STRUCTURE / SILL / BTWN FR25 - FR28 / REPLACEMENT / CORROSION. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. ACCOMPLISH ER/A 630257-14, SECTION II INSPECTION BEFORE AIRCRAFT EXCEEDS 40,600 TOTAL F
- [SDR DALA2026020900941](https://openairdocs.org/sdr/DALA2026020900941.md): Door · corroded · Dec 2, 2025 · N129DU · Airbus BD5001A10 · Fluid Service Doors
  > ER/A 603892-14, REV B, LOWER AFT FUSELAGE, FR 75-76, WASTE SERVICE COMPART & DOOR CORRODED. REPAIR REQUIRES FOLLOW-ON ACTION.ACCOMPLISH 603892-14 REV B, SECTION II REPETITIVE INSPECTION WITHIN EVERY 1,000 FLIGHT HOURS FROM 14,907 TOTAL FH UNTIL SECTION I
- [SDR DALA2025111208278](https://openairdocs.org/sdr/DALA2025111208278.md): Skin · corroded · Nov 10, 2025 · N129DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > EVIDENCE OF CORROSION FOUND ON LWR FUSELAGE SKIN BETWEEN FR34 AND FR35 JUST AFT OF DRAIN BETWEEN S36L AND S36R. REMOVED CORROSION ON LWR FUSELAGE SKIN FR34-FR35, S36L-S36R, NO DAMAGE PERMITTED IN THIS AREA IAW A220 ASRP J51-21-06, J53-31-01. RESTORED FINISH A
- [SDR DALA2025111208274](https://openairdocs.org/sdr/DALA2025111208274.md): Door Sill · corroded · Nov 5, 2025 · N129DU · Airbus BD5001A10 · Fuselage Main, Structure
  > AFT CARGO DOOR LWR SILL HAS CORROSION AROUND FASTENER HOLES AREAS 7 EA. REMOVED CORROSION ON AFT CARGO DOOR LWR SILL, FOUND OUT OF LIMITS IAW A220 ASRP 51-21-06 & 53-61-25, PERFORMED ALL WORK & RESTORED FINISH IAW A220 ERA 629989-14 REV ORIGINAL. ASSOCIATED ER
- [SDR DALA2025111208273](https://openairdocs.org/sdr/DALA2025111208273.md): Scuff Plate · corroded · Nov 5, 2025 · N129DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR SCUFF PLATE SURFACE, CORROSION FOUND AROUND FASTENER HOLES OF LOWER CARGO AFT CARGO DOOR SCUFF PLATE AREA. HOLE # 100L, 80L, 70L, 60L, 50L, 40L, 10L. REMOVED CORROSION ON AFT CARGO DOOR SCUFF PLATE, FOUND OUT OF LIMITS IAW A220 ASRP J51-21-06,
- [SDR DALA2025102407808](https://openairdocs.org/sdr/DALA2025102407808.md): Seat Track · corroded · Oct 19, 2025 · N129DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > PRODUCTION REQUEST: RH OB FWD SEAT TRACK HAS EVIDENCE OF CORROSION AT FR22. REMOVED AND REPLACED R/H O/B FWD SEAT TRACK AT FR22 IAW A220 ASRP J51-40-11, J51-42-21. REMOVED CORROSION, FOUND OUT OF LIMITS IAW A220 ASRP J51-21-06, J53-21-49. (LP# 1259632)
- [SDR DALA2025102407810](https://openairdocs.org/sdr/DALA2025102407810.md): Seat Track · corroded · Oct 18, 2025 · N129DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > PRODUCTION REQUEST: RH 0B AFT SEAT TRACK HAS EVIDENCE OF CORROSION AT FR71. REMOVED CORROSION ON AFT R/H O/B SEAT TRACK, FOUND OUT OF LIMITS IAW A220 ASRP J51-21-06, J53-61-49. REMOVED AND REPLACED DAMAGED SEAT TRACK IAW A220 ASRP J51-40-11, J51-42-21. (LP# 12
- [SDR DALA2025102407809](https://openairdocs.org/sdr/DALA2025102407809.md): Seat Track · corroded · Oct 18, 2025 · N129DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > PRODUCTION REQUEST: RH IB AFT SEAT TRACK HAS EVIDENCE OF CORROSION AT FR71. REMOVED CORROSION ON R/H I/B AFT SEAT TRACK, FOUND OUT OF LIMITS IAW A220 ASRP J51-21-06, J53-61-49. REMOVED AND REPLACED DAMAGED SEAT TRACK IAW A220 ASRP J51-40-11, J51-42-21. (LP# 12
- [SDR DALA2025102407807](https://openairdocs.org/sdr/DALA2025102407807.md): Seat Track · corroded · Oct 18, 2025 · N129DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > PRODUCTION REQUEST: RH IB FWD SEAT TRACK HAS EVIDENCE OF CORROSION AT FR22. REMOVED CORROSION ON R/H I/B FWD SEAT TRACK, FOUND OUT OF LIMITS IAW A220 ASRP J51-21-06, J53-2149. REMOVED AND REPLACED DAMAGED SEAT TRACK IAW A220 ASRP J51-40-11, J51-42-21. (LP# 125
- [SDR DALA2025102407806](https://openairdocs.org/sdr/DALA2025102407806.md): Seat Track · corroded · Oct 18, 2025 · N129DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > PRODUCTION REQUEST: AFT L/H O/B SEAT TRACK HAS SIGNS OF CORROSION. REMOVED AND REPLACED SEAT TRACK AFT L/H O/B IAW A220 ASRP BD-500 -A-J51-42-21, J51-40-11. REMOVED CORROSION, FOUND OUT OF LIMITS IAW A220 ASRP J51-21-00, J53-42-21. (LP# 1259625)
- [SDR DALA2025052704054](https://openairdocs.org/sdr/DALA2025052704054.md): Slat Track · cracked · May 27, 2025 · N129DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK #5 LOWER FWD INBOARD REQUIRES EDDY CURRENT INSPECTION TO BLENDED AREAS, CHECK FOR SIGNS OF CRACKS. LH SLAT TRACK #5 LOWER FWD INBD SURFACE WAS NDT INSPECTED REF A220 ANDTP J-51-01-20. DEFECTS NOTED QC 5257 453307. (LP# 0988435)
- [SDR DALA2024032003520](https://openairdocs.org/sdr/DALA2024032003520.md): Slat Track · corroded · Mar 18, 2024 · N129DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 6 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 6 UPPER FWD SURFACE IAW ER/A 607345- 14AD REV B AND PRI 607345-14AD REV 0 MATCHED. (LP# 0251247)
- [SDR DALA2024032003519](https://openairdocs.org/sdr/DALA2024032003519.md): Slat Track · corroded · Mar 18, 2024 · N129DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 6 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 6 UPPER AFT SURFACE IAW ER/A 607345- 14AD REV B AND PRI 607345-14AD REV 0 MATCHED. (LP# 0251242)
- [SDR DALA2024032003518](https://openairdocs.org/sdr/DALA2024032003518.md): Slat Track · corroded · Mar 18, 2024 · N129DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 5 UPPER FWD SURFACE IAW ER/A 607345- 14AD REV B AND PRI 607345-14AD REV 0 MATCHED. (LP# 0251236)
- [SDR DALA2024032003517](https://openairdocs.org/sdr/DALA2024032003517.md): Slat Track · corroded · Mar 18, 2024 · N129DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 UPPER FWD SURFACE IN TWO LOCATIONS HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 4 UPPER FWD SURFACE IAW ER/A 607345- 14AD REV B AND PRI 607345-14AD REV 0 MATCHED. (LP# 0251228)
- [SDR DALA2024032003516](https://openairdocs.org/sdr/DALA2024032003516.md): Slat Track · corroded · Mar 18, 2024 · N129DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 3 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 3 UPPER AFT SURFACE IAW ER/A 607345- 14AD REV B AND PRI 607345-14AD REV 0 MATCHED. (LP# 0251215)
- [SDR DALA2024032003515](https://openairdocs.org/sdr/DALA2024032003515.md): Slat Track · corroded · Mar 18, 2024 · N129DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 3 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 3 LOWER AFT SURFACE IAW ER/A 607345- 14AD REV B AND PRI 607345-14AD REV 0 MATCHED. (LP# 0251199)
- [SDR DALA2024032003514](https://openairdocs.org/sdr/DALA2024032003514.md): Slat Track · corroded · Mar 18, 2024 · N129DU · 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 607345- 14AD REV B AND PRI 607345-14AD REV 0 MATCHED. (LP# 0251192)
- [SDR DALA2024032003513](https://openairdocs.org/sdr/DALA2024032003513.md): Slat Track · corroded · Mar 18, 2024 · N129DU · 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 607345- 14AD REV B AND PRI 607345-14AD REV 0 MATCHED. (LP# 0251182)
- [SDR DALA2024032003512](https://openairdocs.org/sdr/DALA2024032003512.md): Slat Track · corroded · Mar 18, 2024 · N129DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 11 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 11 UPPER FWD SURFACE IAW ER/A 607347- 14AD REV D AND PRI 607347-14AD REV 0 MATCHED. (LP# 0251161)
- [SDR DALA2024032003511](https://openairdocs.org/sdr/DALA2024032003511.md): Slat Track · corroded · Mar 18, 2024 · N129DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 6 LOWER FWD I/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 6 LOWER FWD I/B SIDE IAW ER/A 607347- 14AD REV D AND PRI 607347-14AD REV 0 MATCHED. (LP# 0251154)
- [SDR DALA2024032003510](https://openairdocs.org/sdr/DALA2024032003510.md): Slat Track · corroded · Mar 18, 2024 · N129DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 6 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 6 UPPER FWD SURFACE IAW ER/A 607347- 14AD REV D AND PRI 607347-14AD REV 0 MATCHED. (LP# 0251146)
- [SDR DALA2024032003509](https://openairdocs.org/sdr/DALA2024032003509.md): Slat Track · corroded · Mar 18, 2024 · N129DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 5 UPPER FWD SURFACE IAW ER/A 607347- 14AD REV D AND PRI 607347-14AD REV 0 MATCHED. (LP# 0251142)
- [SDR DALA2024032003508](https://openairdocs.org/sdr/DALA2024032003508.md): Slat Track · corroded · Mar 18, 2024 · N129DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 5 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 5 UPPER AFT SURFACE IAW ER/A 607347- 14AD REV D AND PRI 607347-14AD REV 0 MATCHED. (LP# 0251137)
- [SDR DALA2024032003507](https://openairdocs.org/sdr/DALA2024032003507.md): Slat Track · corroded · Mar 18, 2024 · N129DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 4 LOWER FWD I/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 4 LOWER FWD I/B SIDE IAW ER/A 607347- 14AD REV D AND PRI 607347-14AD REV 0 MATCHED.
- [SDR DALA2024032003506](https://openairdocs.org/sdr/DALA2024032003506.md): Slat Track · corroded · Mar 18, 2024 · N129DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 2 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 2 UPPER AFT SURFACE IAW ER/A 607347- 14AD REV D AND PRI 607347-14AD REV 0 MATCHED.
- [SDR DALA2022120107683](https://openairdocs.org/sdr/DALA2022120107683.md): None · none · Dec 1, 2022 · N129DU · Bombdr BD1001A10 · Standard Practices/Structures
  > DOCUMENT WORK FOR LOG 2455907 ACCOMPLISH ER/A 602362-14. ACCOMPLISHED AND RECORDED WTBF MODIFICATION PER PRI 602362-14 REV 0, REV 1, REV 2, REV 3, AND REV 4 AND VERIFIED WORK ACCOMPLISHED WITH FINAL ER/A 602362-14AD REV C SECTION I. REPAIR IS CLASSIFIED MAJOR
- [SDR DALA2022120107682](https://openairdocs.org/sdr/DALA2022120107682.md): Structure · corroded · Nov 30, 2022 · N129DU · Bombdr BD1001A10 · Fuselage Miscellaneous Structure
  > AFT FUSELAGE WASTE BOX CORRODED IN FWD AND AFT OF THE CUT OUT AREA. SEE NON-ROUTINE 00041 OF WORK PACKAGE P541181220221020 FOR MORE INFORMATION. ALL CORRODED PARTS WERE REPLACED WITH NEW. REPAIRED WASTE SERVICE COMPARTMENT PER DAL ER/A PRI 603892-14 REV. 0, RE
- [SDR DALA2022120107681](https://openairdocs.org/sdr/DALA2022120107681.md): None · none · Nov 28, 2022 · N129DU · Bombdr BD1001A10 · Standard Practices/Structures
  > AMOC AD 2021-22-17 ER/A 602362-14AD REV A INCLUDES INSTRUCTION FOR MODIFICATION OF THE WTBF ON 8129. SEC II TRACKS LIMIT FOR THE NEXT DUE AD 2021-22-17 INSPECTION. AMOC APPROVING TERMINATING ACTION MUST BE ACQUIRED PRIOR TO REACHING THIS LIMIT. *AMOC* REVISE E
- [SDR DALA2022120607825](https://openairdocs.org/sdr/DALA2022120607825.md): Waste Box · corroded · Nov 26, 2022 · N129DU · Bombdr BD1001A10 · Fuselage Miscellaneous Structure
  > WASTE BOX CORROSION REPAIR ON DOOR SKIN, WASTE BOX PAN, HINGE FITTINGS, HINGE ARMS, AND INTERNAL DOUBLER. SECTION I OF ER/A 6038 92-14 TIME LIMITED REPAIR, FOLLOW-ON ACTION IS REQUIRED. SECTION II OF ER/A 603892-14 REQUIRES REPEAT INSPECTIONS EVERY 850 FH UNTI
- [SDR DALA2022120107684](https://openairdocs.org/sdr/DALA2022120107684.md): None · none · Oct 17, 2022 · N129DU · Bombdr BD1001A10 · Standard Practices/Structures
  > ACCOMPLISH ER/A 602362-14 SECTION 01 AT THE NEXT C-CHECK OF THE AIRCRAFT. ACCOMPLISH ER/A 602362-14 SECTION 01 AT THE NEXT C-CHECK OF THE AIRCRAFT. ASSOCIATED ER/A 00-602362 ADDED FOR AC 8129. ACCOMPLISHED AND RECORDED WTBF MODIFICATION PER PRI 602362-14 REV 0
- [SDR DALA2021112307196](https://openairdocs.org/sdr/DALA2021112307196.md): None · none · Nov 20, 2021 · N129DU · Bombdr BD1001A10 · Smoke Detection
  > SMOKE DET FAILURE IN FLIGHT COMPLIED W/ ECL EQUIP BAY SMOKE DET FAIL. R/R SYS A SMOKE DET 1 (A328P1) PER A220 AMP 26-13. CLEANED INLET TUBING TO SMOKE DETECTORS WITH PRESSURIZED AIR NO DEBRIS NOTED. R/R SYS B SMOKE DET 2 PER A220 AMP 26-13 AND INLET TUBING OPS
- [SDR DALA2021040702060](https://openairdocs.org/sdr/DALA2021040702060.md): Apu · bird ingestion · Apr 5, 2021 · N129DU · Bombdr BD1001A10 · APU Core Engine
  > STRONG FUMES ON APU START UP. ALL OTHER PARAMETERS NORMAL. UPON INSPECTION OF ODOR IN THE CABIN FOUND BIRD REMAINS IN THE APU INLET. INSPECTED APU INLET AND RAN PACKS PER EFIM 1-8458. NO ODOR IN THE CABIN AND COCKPIT. C/W ODI PREVENTION SMOKE FUMES. AIRCRAFT O
- [SDR DALA2021052802969](https://openairdocs.org/sdr/DALA2021052802969.md): Skin · dented · Oct 2, 2020 · N129DU · Bombdr BD1001A10 · Cargo/Baggage Doors
  > DENT AT FWD CARGO DOOR MEASURES 2.7" WIDTH. 1.30" DEPTH, AND 1" IN HEIGHT. DENT DEFERRED TO MON PER ER/A 588-077-14 REV. ORIGINAL, AN INITIAL INSPECTION IS DUE AT 50 HOURS, PERMANANT REPAIR IN ACCORDANCE WITH THIS ER/ A IS DUE AT 1700 HOURS. ASSOCIATED ER/A 14
- [SDR DALA2020081322769](https://openairdocs.org/sdr/DALA2020081322769.md): Warning Message · false activation · Aug 11, 2020 · N129DU · Bombdr BD1001A10 · Landing Gear Brake System
  > DECLARED EMERGENCY LANDING FOR BRAKE ON CAUTION MESSAGE INFLIGHT AND ALTN BRAKE FAIL ADVISORY MSG.RTM REPORTING ALTN BRAKE FAIL, BRAKE ON CAUTION MSG,L BRAKE DEGRADED ADVISORY MSG. TROUBLESHOT FAULT CODES 3243F0217,3243F021,3243F0211.

## 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 = 'N129DU' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N129DU/reports

---
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