# Service difficulty reports: N301DU

A list on [N301DU](https://openairdocs.org/aircraft/N301DU.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 · 62 reports

- [SDR DALA2026092205308](https://openairdocs.org/sdr/DALA2026092205308.md): Door Frame · corroded · Sep 16, 2026 · N301DU · Airbus BD5001A11 · Fuselage Main, Structure
  > DURING H CHECK IN MSP, MAINTENANCE WAS ACCOMPLISHING EO WORKCARD 5331-01297-02C (SB BD500-530010 ISSUE 004). DURING MODIFICATION, THE AFT CARGO DOOR SURROUND STRUCTURE C01343028- 103 LOWER SILL WAS FOUND WITH CORROSION. THE CORROSION FOUND IS ON THE OUTER SURF
- [SDR DALA2026092205307](https://openairdocs.org/sdr/DALA2026092205307.md): Door Frame · corroded · Sep 16, 2026 · N301DU · Airbus BD5001A11 · Fuselage Main, Structure
  > AFT SERVICE DOOR SURROUND - FR76 DOOR FRAME HAS SEVERAL HOLES WITH CORROSION. -M- REFERENCE SSI: 53-61-24-03. NO PRESENCE OF BLUE PAINT FROM PREVIOUS REPAIR. ACCOMPLISHED TASKS FOR ER/A 636471-14 PRI REV. 0, ER/A 636471-14 PRI REV. 1, ER/A636471-14 PRI REV. 2
- [SDR DALA2026092205306](https://openairdocs.org/sdr/DALA2026092205306.md): Door Frame · corroded · Sep 16, 2026 · N301DU · Airbus BD5001A11 · Fuselage Main, Structure
  > AFT SERVICE DOOR SURROUND - FR74 DOOR FRAME HAS SEVERAL HOLES WITH CORROSION. -M- REFERENCE SSI: 53-61-24-03. NO PRESENCE OF BLUE PAINT FROM PREVIOUS REPAIR. ACCOMPLISHED TASKS FOR ER/A 636471-14 PRI REV. 0, ER/A 636471-14 PRI REV. 1, ER/A 636471-14 PRI REV.
- [SDR DALA2026092205305](https://openairdocs.org/sdr/DALA2026092205305.md): Skin · corroded · Sep 16, 2026 · N301DU · Airbus BD5001A11 · Fuselage Main, Plate/Skin
  > EVIDENCE OF CORROSION FOUND AT AFT WTB FUSELAGE SKIN, AIRCRAFT CENTERLINE. (M)(P) REF CORROSION SSI: 53-50-02-05. COMPLIED WITH ER/A 636443-14 PRI REV 0, ER/A 636443-14 PRI REV 1, ER/A 636443-14 PRI REV 2, AND FINAL ER/A 636443-14 REV ORIGINAL SECTION I. NOM
- [SDR DALA2026092205304](https://openairdocs.org/sdr/DALA2026092205304.md): Stringer · damaged · Sep 16, 2026 · N301DU · Airbus BD5001A11 · Fuselage Main, Longeron/Stringer
  > WHILE REMOVING DAMAGED SKIN IAW PRI 636395-14, STR 36L BETWEEN FR 34-35 DAMAGED BY CUTOFF WHEEL. COMPLIED WITH ER/A 636395-14 REV 0 PRI REV 0, REV 1, REV 2, REV 3, REV 4, AND FINAL ER/A 636395-14 REV ORIGINAL SECTION I. (LP# 1815437; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026092205303](https://openairdocs.org/sdr/DALA2026092205303.md): Skin · corroded · Sep 16, 2026 · N301DU · Airbus BD5001A11 · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON BOTTOM SKIN AT FWD EDGE OF WTBF, BETWEEN STR36L. COMPLIED WITH ER/A 636395-14 REV 0 PRI REV 0, REV 1, REV 2, REV 3, REV 4, AND FINAL ER/A 636395-14 REV ORIGINAL SECTION I. (LP# 1815433; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026092205302](https://openairdocs.org/sdr/DALA2026092205302.md): Door Sill · damaged · Sep 15, 2026 · N301DU · Airbus BD5001A11 · Fuselage Main, Structure
  > FWD CARGO DOOR SURROUND STRUCTURE, LWR SILL AREA (AREA COVERED BY SCUFF PLATES), SKIN PANEL, SILL. COMPLIED WITH ER/A 636422-14 PRI REV 0 AND FINAL ER/A 636422-14 REV ORIGINAL SECTION I PERMANENT REPAIR. PART REPLACED. (LP# 1814859; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026092205301](https://openairdocs.org/sdr/DALA2026092205301.md): Waste Box · corroded · Sep 15, 2026 · N301DU · Airbus BD5001A11 · Fuselage Main, Structure
  > WASTE BOX RIGHT SIDE INNER LIP HAS CORROSION. -M- REF. CORROSION SSI: 53-61-56-02. COMPLIED WITH ER/A 611850-14 ER/A REV A PRI REV 0, 1, AND ERA 611850-14 REV A. ORIGINAL THICKNESS.125'. MATERIAL REMOVED.034". REMAINING THICKNESS.091". (LP# 1814774; AIRCRA
- [SDR DALA2026092205300](https://openairdocs.org/sdr/DALA2026092205300.md): Waste Box · corroded · Sep 15, 2026 · N301DU · Airbus BD5001A11 · Fuselage Main, Structure
  > WASTE BOX FWD RIGHT CORNER HAS CORROSION MULTIPLE PLACES AND SURROUNDING RIGHT HINGE FITTING. -M- -P- REF. CORROSION SSI: 53- 61-56-02. COMPLIED WITH ER/A 611850-14 ER/A REV A PRI REV 0, 1, AND ERA 611850-14 REV A. ORIGINAL THICKNESS.125'. MATERIAL REMOVED.
- [SDR DALA2026091605181](https://openairdocs.org/sdr/DALA2026091605181.md): Longeron · corroded · Sep 8, 2026 · N301DU · Airbus BD5001A11 · Aerodynamic Fairings
  > ER/A 636601-14 CORROSION REPAIR TO WING TO BODY FAIRING LH LONGERON BETWEEN FR 40 TO FR 48 REQUIRES FOLLOW ON ACTION. ACCOMPLISH 636601-14 SECT II REP INSPECTION WITHIN EVERY 1000 FLIGHT HOURS FROM SECT I ACCOMPLISHMENT. ACCOMPLISH SECT III PERMANENT REPAIR WI
- [SDR DALA2026091105088](https://openairdocs.org/sdr/DALA2026091105088.md): Frame · corroded · Sep 8, 2026 · N301DU · Airbus BD5001A11 · Fuselage Main, Frame
  > CORROSION R/H SIDE FRAME PART # C02382152-102 AT MULTIPLE LOWER PANEL FASTENER HOLES. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0537:2090-2001/007 00307 REMOVED AND REPLACED FRAME PER REF A220 ASRP 51-42-00. (LP# 1800973; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026091105087](https://openairdocs.org/sdr/DALA2026091105087.md): Slide · no test · Sep 7, 2026 · N301DU · Airbus BD5001A11 · Escape Slide
  > WHILE PERFORMING AMDS 2561-9005-CHECK, THE LH OWEED SLIDE FAILED DEPLOYMENT WITH BOTH NORMAL OPERATION AND BY PULLING THE BACKUP T-HANDLE. SLIDE MPN IS 68332-103, S/N: 28430, AND DATE OF MFG: MAY 2023. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR
- [SDR DALA2026091005075](https://openairdocs.org/sdr/DALA2026091005075.md): Seat Track · corroded · Sep 6, 2026 · N301DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach Fittings
  > FR74 RT INBD SEAT TRACK INSERT CORRODED. SEE INFORMATION 001-0585:5300-2016/004 00428. REMOVED AND REPLACED SEAT TRACK IAW ASRP 51-40-00. (LP# 1799083; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026090204954](https://openairdocs.org/sdr/DALA2026090204954.md): Threshold · corroded · Aug 31, 2026 · N301DU · Airbus BD5001A11 · Fuselage Miscellaneous Structure
  > LEFT AFT PAX DOOR THRESHOLD PANEL, AFT INBD CORNER WAS CORRODED. REMOVED AND REPLACED THE THRESHOLD PANEL IAW ASRP 51-40-00. (LP# 1786990; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026090104932](https://openairdocs.org/sdr/DALA2026090104932.md): Frame · corroded · Aug 29, 2026 · N301DU · Airbus BD5001A11 · Aerodynamic Fairings
  > CORROSION ON AFT WING TO BODY FAIRING FRAME AT MULTIPLE LOWER PANEL FASTENER HOLES. REMOVED AND REPLACED THE FAIRING FRAME IAW 51-77-00. (LP# 1783796; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026090104931](https://openairdocs.org/sdr/DALA2026090104931.md): Frame · corroded · Aug 29, 2026 · N301DU · Airbus BD5001A11 · Aerodynamic Fairings
  > CORROSION ON AFT WING TO BODY FAIRING FRAME AT MULTIPLE LOWER PANEL FASTENER HOLES. REMOVED AND REPLACED THE FAIRING FRAME IAW 51-77-00. (LP# 1783791; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026082704867](https://openairdocs.org/sdr/DALA2026082704867.md): Frame · corroded · Aug 24, 2026 · N301DU · Airbus BD5001A11 · Fuselage Main, Frame
  > CORROSION ON RT SIDE FRAME AT MULTIPLE LOWER PANEL FASTENER AREAS. WORKED WITH NR 303 FOR REMOVAL AND REPLACEMENT OF LONGERON. (LP# 1774104; AIRCRAFT WAS GROUNDED)
- [SDR DALA2025112508590](https://openairdocs.org/sdr/DALA2025112508590.md): Longeron · cracked · Nov 23, 2025 · N301DU · Airbus BD5001A11 · Fuselage Main, Longeron/Stringer
  > WORKING AMDS 5352-01038-01A W/P 2967182 STEP 10D FOUND LONGERON P/N C02383111-001 CRACKED MID LENGTH ADJ TO TIE ROD IN THE VICINITY OF LBL 40.0. REMOVED LONGERON P/N C2383111-001 VICINITY OF LBL 40.0 RH 177277. INSTALLED LONGERON, PER WORK CARD 5352-01038-07A.
- [SDR DALA2025112508591](https://openairdocs.org/sdr/DALA2025112508591.md): Control Unit · malfunctioned · Nov 22, 2025 · N301DU · Airbus BD5001A11 · Landing Gear Brake System
  > R BRAKE FAIL CAUTION MESSAGE OCCURRED AFTER DROPPING LANDING GEAR FOR LANDING. AFTER LANDING, THE RIGHT BRAKE SEEMED TO GRAB WHEN NOT DEPRESSING RIGHT BRAKE PEDAL. DUE TO HISTORY, SUSPECT BDCU 2 REQUIRES REPLACEMENT. REMOVED AND REPLACED BDCU 2 PER A220 AMP 32
- [SDR DALA2025042403228](https://openairdocs.org/sdr/DALA2025042403228.md): Slat Track · corroded · Apr 17, 2025 · N301DU · Airbus BD5001A11 · Leading Edge Devices
  > FOUND RH SLAT TRACK #4 RACK TOOTH #1 AND #2, HAS EVIDENCE OF CORROSION AFT SURFACE AND PREVIOUS REWORK, 5742-01028-02B. LIAISON ENGINEERING REQUIRED BEFORE FURTHER FLIGHT. PERFORMED HFEC PER STEP 7 OF PRI 620906-14AD REV 0. REF A220 ANDTP 51-01-20. NO CRACK I
- [SDR DALA2025042103106](https://openairdocs.org/sdr/DALA2025042103106.md): Slat Track · corroded · Apr 16, 2025 · N301DU · Airbus BD5001A11 · Leading Edge Devices
  > FOUND LH SLAT TRACK #6 RACK TOOTH #2, HAS EVIDENCE OF CORROSION AFT SURFACE WITH NO PREVIOUS REWORK, 5742-01028-02A. LIAISON ENGINEERING REQUIRED BEFORE FURTHER FLIGHT. PERFORMED HFEC PER STEP 8 OF PRI. REF A220 ANDTP 51-01-20. NO CRACK INDICATIONS NOTED. COMP
- [SDR DALA2025042103105](https://openairdocs.org/sdr/DALA2025042103105.md): Slat Track · corroded · Apr 16, 2025 · N301DU · Airbus BD5001A11 · Leading Edge Devices
  > FOUND LH SLAT TRACK #4 PINION TOOTH #1 AND #2, HAS EVIDENCE OF CORROSION LWR SURFACE WITH NO PREVIOUS REWORK, 5742-01028-02A. LIAISON ENGINEERING REQUIRED BEFORE FURTHER FLIGHT. PERFORMED HFEC PER STEP 8 OF PRI. REF A220 ANDTP 51-01-20. NO CRACK INDICATIONS NO
- [SDR DALA2025042103104](https://openairdocs.org/sdr/DALA2025042103104.md): Slat Track · corroded · Apr 16, 2025 · N301DU · Airbus BD5001A11 · Leading Edge Devices
  > FOUND LH SLAT TRACK #6 PINION TOOTH #2, HAS EVIDENCE OF CORROSION LWR SURFACE WITH NO PREVIOUS REWORK, 5742-01028-02A. PERFORMED HFEC PER STEP 8 OF PRI. REF A220 ANDTP 51-01-20. NO CRACK INDICATIONS NOTED. QC5350. COMPLIED WITH ER/A 620942-14AD REV B AND PRI 6
- [SDR DALA2024101109974](https://openairdocs.org/sdr/DALA2024101109974.md): Frame · cracked · Oct 10, 2024 · N301DU · Airbus BD5001A11 · Fuselage Main, Frame
  > CRACK FOUND ON WQTBF FRAME FORWARD OF RH WHEEL BIN REMOVED 194DB PANEL FOR ACCESS. AND REMOVED ONE HI-LOK FASTENER FOR EASE OF MEASURING THE CRACK (412863) ER/A ISSUED FOR CRACK AND STOP-DRILL, BUT UNABLE TO ACCOMPLISH DUE TO LACK OF CLEARANCE. ER/A CANCELLED
- [SDR DALA2024100209611](https://openairdocs.org/sdr/DALA2024100209611.md): Rack · corroded · Oct 1, 2024 · N301DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK #4 RACK TEETH (2EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. PERFORMED NDT PER PRI 620942-14 REV 0 STEP 7. C/W RII. (LP# 0586615)
- [SDR DALA2024100209610](https://openairdocs.org/sdr/DALA2024100209610.md): Pinion · corroded · Oct 1, 2024 · N301DU · Airbus BD5001A11 · Leading Edge Devices
  > LG SLAT TRACK#4 PINION TEETH (2EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. PERFORMED NDT PER PRI 620942-14 REV 0 STEP 7. C/W II. (LP# 0586605)
- [SDR DALA2024100209609](https://openairdocs.org/sdr/DALA2024100209609.md): Pinion · corroded · Oct 1, 2024 · N301DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK #11 RACK TEETH (2EA) HAS EVIDENCE OF CORROSION REF 5742-01028-02B. PERFORMED NDT PER PRI 620942-14 REV 0 STEP 7. C/W RII. (LP# 0586594)
- [SDR DALA2024100209608](https://openairdocs.org/sdr/DALA2024100209608.md): Pinion · corroded · Oct 1, 2024 · N301DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK #4 PINION TEETH (2EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. PERFORMED NDT PER PRI 620906-14 REV 0 STEP 7. C/W RII. (LP# 0586574)
- [SDR DALA2024100209607](https://openairdocs.org/sdr/DALA2024100209607.md): Pinion · corroded · Oct 1, 2024 · N301DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK #11 PINION TEETH (2EA) HAS EVIDENCE OF CORROSION REF 5742-01028-02B. PERFORMED NDT PER PRI 620906-14 REV 0 STEP 7. C/W RII. (LP# 0586563)
- [SDR DALA2024040904235](https://openairdocs.org/sdr/DALA2024040904235.md): Slat Track · corroded · Apr 6, 2024 · N301DU · Airbus BD5001A11 · 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 608864- 14AD REV B AND PRI 608864-14AD REV 0 MATCHED. (LP# 0280970)
- [SDR DALA2024040904234](https://openairdocs.org/sdr/DALA2024040904234.md): Slat Track · corroded · Apr 6, 2024 · N301DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 4 PINION HAS EVIDENCE OF CORROSION IN 2 LOCATIONS AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 4 PINION IN 2 LOCATION IAW ER/A 608864-14AD REV B AND PRI 608864-14AD REV 0 MATCHED. (LP# 0280965)
- [SDR DALA2024040904233](https://openairdocs.org/sdr/DALA2024040904233.md): Slat Track · corroded · Apr 6, 2024 · N301DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-011028-02A. REPAIRED LH SLAT TRACK NBR 5 UPPER FWD SURFACE IAW ER/A 608864- 14AD REV B AND PRI 608863-14AD REV 0 MATCHED. (LP# 0280964)
- [SDR DALA2024040904232](https://openairdocs.org/sdr/DALA2024040904232.md): Slat Track · corroded · Apr 6, 2024 · N301DU · Airbus BD5001A11 · 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 608864- 14AD REV B AND PRI 608864-14AD REV 0 MATCHED. (LP# 0280949)
- [SDR DALA2024040904231](https://openairdocs.org/sdr/DALA2024040904231.md): Slat Track · corroded · Apr 6, 2024 · N301DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 4 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 4 LOWER AFT SURFACE IAW ER/A 608864- 14AD REV B AND PRI 608864-14AD REV 0 MATCHED. (LP# 0280932)
- [SDR DALA2024040904230](https://openairdocs.org/sdr/DALA2024040904230.md): Slat Track · corroded · Apr 6, 2024 · N301DU · Airbus BD5001A11 · 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 608864- 14AD REV B AND PRI 608864-14AD REV 0 MATCHED. (LP# 0280924)
- [SDR DALA2024040904229](https://openairdocs.org/sdr/DALA2024040904229.md): Slat Track · corroded · Apr 6, 2024 · N301DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 FWD RACK TEETH HAVE EVIDENCE OF CORROSION IN 2 LOCATIONS AND PREVIOUS REWORK, REF 5742-011028-02B. REPAIRED RH SLAT TRACK NBR 4 FWD RACK TEETH IN 2 LOCATIONS IAW ER/A 608863-14AD REV B AND PRI 608863-14AD REV 0 MATCHED. (LP# 0280918)
- [SDR DALA2024040904228](https://openairdocs.org/sdr/DALA2024040904228.md): Slat Track · corroded · Apr 6, 2024 · N301DU · Airbus BD5001A11 · Leading Edge Devices
  > LH SLAT TRACK NBR 1 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION IN 2 LOCATIONS AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 1 UPPER FWD SURFACE IN 2 LOCATIONS IAW ER/A 608864-14AD REV B AND PRI 608864-14AD REV 0 MATCHED.
- [SDR DALA2024040904227](https://openairdocs.org/sdr/DALA2024040904227.md): Slat Track · corroded · Apr 6, 2024 · N301DU · Airbus BD5001A11 · 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 608863- 14AD REV B AND PRI 608863-14AD REV 0 MATCHED. (LP# 0280907)
- [SDR DALA2024040904226](https://openairdocs.org/sdr/DALA2024040904226.md): Slat Track · corroded · Apr 6, 2024 · N301DU · Airbus BD5001A11 · 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 608863- 14AD REV B AND PRI 608863-14AD REV 0 MATCHED. (LP# 0280903)
- [SDR DALA2024040904225](https://openairdocs.org/sdr/DALA2024040904225.md): Slat Track · corroded · Apr 6, 2024 · N301DU · Airbus BD5001A11 · 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 608863- 14AD REV B AND PRI 608863-14AD REV 0 MATCHED. (LP# 0280901)
- [SDR DALA2024040904224](https://openairdocs.org/sdr/DALA2024040904224.md): Slat Track · corroded · Apr 6, 2024 · N301DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 PINION HAS EVIDENCE OF CORROSION IN 2 LOCATIONS AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 4 PINION IN 2 LOCATIONS IAW ER/A 608863-14AD REV B AND PRI 608863-14AD REV 0 MATCHED. (LP# 0280910)
- [SDR DALA2024040904223](https://openairdocs.org/sdr/DALA2024040904223.md): Slat Track · corroded · Apr 6, 2024 · N301DU · Airbus BD5001A11 · 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 608863- 14AD REV B AND PRI 608863-14AD REV 0 MATCHED. (LP# 0280894)
- [SDR DALA2024040904222](https://openairdocs.org/sdr/DALA2024040904222.md): Slat Track · corroded · Apr 6, 2024 · N301DU · Airbus BD5001A11 · 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 FWD SURFACE IAW ER/A 608863-14AD REV B AND PRI 608863-14AD REV 0 MATCHED. (LP# 0280887)
- [SDR DALA2024040904221](https://openairdocs.org/sdr/DALA2024040904221.md): Slat Track · corroded · Apr 6, 2024 · N301DU · Airbus BD5001A11 · Leading Edge Devices
  > RH SLAT TRACK NBR 1 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 06APR24 2204 UTC 02 CORR BY CARPINTERO 01711729 IAH 06APR24 ATA 5742
- [SDR DALA2024040204035](https://openairdocs.org/sdr/DALA2024040204035.md): Brake Assy · failed · Mar 27, 2024 · N301DU · Airbus BD5001A11 · Landing Gear Brake System
  > SHIP 8301 - MISC / DE - DUE TO "RT BRAKE DEGRADED" ADVISORY MESSAGE. CORRECTIVE ACTION: R/R #3 AND #4 MLG BRAKE ASSEMBLIES. R/R #4 EMCU. (LP# 5798435, 5798432)
- [SDR DALA2024012601200](https://openairdocs.org/sdr/DALA2024012601200.md): Seat Track · corroded · Jan 25, 2024 · N301DU · Bombdr BD1001A10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK, LBL 23 CORRODED AT AFT END. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0005:2500-2647/108 00207 COMPLIED WITH PRI 614686-14 REV 0, 01 AND ER/A 614686-14 REV O. ALL CORRODED PARTS WERE REMOVED AND NEW P
- [SDR DALA2024012601207](https://openairdocs.org/sdr/DALA2024012601207.md): Cover · unknown · Jan 24, 2024 · N301DU · Bombdr BD1001A10 · Fuselage Structure (General)
  > THE AFT FLOOR MOUNT COVERS FOR LAV C ARE RAISED.SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0005:2500-2647/065 00076 COMPLIED WITH PRI 614686-14 REV 0, REV 01, REV02, REV03, REV04, REV05, REV06, REV07 AND ER/A 6146
- [SDR DALA2024012601199](https://openairdocs.org/sdr/DALA2024012601199.md): Seat Track · corroded · Jan 24, 2024 · N301DU · Bombdr BD1001A10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK, RBL 43.5 CORRODED AT AFT END. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0005:2500-2647/106 00205 COMPLIED WITH PRI 614686-14 REV 0, REV 01, REV02, REV03, REV04, REV05, REV06, REV07 AND ER/A 614686-14
- [SDR DALA2024012601198](https://openairdocs.org/sdr/DALA2024012601198.md): Seat Track · corroded · Jan 24, 2024 · N301DU · Bombdr BD1001A10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK, RBL 23 CORRODED AT AFT END. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0005:2500-2647/107 00206 COMPLIED WITH PRI 614686-14 REV 0, REV 01, REV02, REV03, REV04, REV05, REV06, REV07 AND ER/A 614686-14 RE
- [SDR DALA2024012601197](https://openairdocs.org/sdr/DALA2024012601197.md): Seat Track · corroded · Jan 24, 2024 · N301DU · Bombdr BD1001A10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK, LBL 43.5 CORRODED AT AFT END. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0005:2500-2647/109 00208 COMPLIED WITH PRI 614686-14 REV 0, REV 01, REV02, REV03, REV04, REV05, REV06, REV07 AND ER/A 614686-14

Next page: https://openairdocs.org/aircraft/N301DU/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 = 'N301DU' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N301DU/reports

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