# Service difficulty reports: N131DU

A list on [N131DU](https://openairdocs.org/aircraft/N131DU.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 · 92 reports

- [SDR DALA2026051302995](https://openairdocs.org/sdr/DALA2026051302995.md): Warning Message · false activation · May 12, 2026 · N131DU · Airbus BD5001A10 · Door Warning System
  > WING SLIDE CAUTION MESSAGE CAME ON DURING TAXI- MSG INFO- 52 WING SLIDE- LT OWEE SLIDE INOP. FOUND L/H OVERWING SLIDE PRESSURE LOW REF A220 AMP 25-63. R/R L/ H OVERWING SLIDE REF A220 W/C # 2563-4002(621049). C/W RII OF W/ C A220 2563-4002 VERIFIED CABLE INSTA
- [SDR DALA2026020300804](https://openairdocs.org/sdr/DALA2026020300804.md): Vent · clogged · Jan 28, 2026 · N131DU · Airbus BD5001A10 · Buffet/Galleys
  > BURNING ELECTRICAL SMELL DURING CRUISE IN AFT PART OF FORWARD GALLEY BY DOOR 1R. TURNED OFF CIRCUIT BREAKERS. SMELL DISSIPATED. AFTER LANDING THERE IS STILL A TRACE OF THE SMELL. UPON ARRIVAL TO A/C NO SMELL NOTED. PERFORMED OPS CHECKS OF OVEN AND COFFEE MAKER
- [SDR DALA2025102407822](https://openairdocs.org/sdr/DALA2025102407822.md): Door Sill · corroded · Oct 17, 2025 · N131DU · Airbus BD5001A10 · Fuselage Main, Structure
  > 1 REPORTED BY LINARES 00705131 MSP 17OCT25 ENTR 00532877 W FWD PAX DOOR - CORROSION NOTED AROUND MULTIPLE HOLES ALONG LOWER SILL AND SILL FLOOR (M)(P) LOG-PAGE UPDATED @ 17OCT25 1800 UTC 02 CORR BY REYNOLDS 00390101 MSP 17OCT25 ATA 5331 RII: N ENTR 00532877 W
- [SDR DALA2025102407814](https://openairdocs.org/sdr/DALA2025102407814.md): Skin · corroded · Oct 17, 2025 · N131DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > FWD PAX DOOR - CORROSION NOTED ADJACENT TO LOWER SKIN HOLES 14OL, 13OL,10OL, AND 2OL. SSI:53-21-23-02 (M) SEE NR FOR ADDITIONAL INFORMATION 031-0001:5331-01297- 01A/001 00340 COMPLIED WITH PRI 629106-14 REV 0, 1, 2 AND ER/A 629106-14 REV O SECTION 1. SEE LOG
- [SDR DALA2025102407813](https://openairdocs.org/sdr/DALA2025102407813.md): Skin · corroded · Oct 17, 2025 · N131DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > DURING H-CHECK IN MSP, MAINTENANCE WAS ACCOMPLISHING EO WORKCARD 5331-01297-01B (SB BD500-530010 ISSUE 004). DURING MODIFICATION, MAINTENANCE REPORTED CORROSION ON THE FWD RH SERVICE DOOR SCUFF PLATE AND DISCOVERED CORROSION COMMON TO SEVERAL OF THE FASTENER
- [SDR DALA2025102407812](https://openairdocs.org/sdr/DALA2025102407812.md): Frame · corroded · Oct 17, 2025 · N131DU · Airbus BD5001A10 · Fuselage Main, Frame
  > INSPECT FORWARD SERVICING AREA PASSENGER COMPARTMENT, WITH GALLEY AND LAVATORY REMOVED. FRAME 17 AFT HOLE 5, 7, 8 HAVE CORROSION. LOG-PAGE UPDATED @ 17OCT25 1937 UTC 02 CORR BY GILMORE 00473815 MSP 17OCT25 ATA 5321 RII: N ENTR 00532877 W SUMMARY SEE NR FOR ADD
- [SDR DALA2025102407811](https://openairdocs.org/sdr/DALA2025102407811.md): Door Sill · corroded · Oct 17, 2025 · N131DU · Airbus BD5001A10 · Fuselage Main, Structure
  > DURING H-CHECK IN MSP, MAINTENANCE WAS ACCOMPLISHING EO WORKCARD 5331-01297-01C (SB BD500-530010 ISSUE 004). DURING MODIFICATION, THE FWD CARGO DOOR SURROUND STRUCTURE C02313004-005 LOWER SILL, AND C02312110 BOTTOM SKIN WERE FOUND CORRODED AFTER SCUFF PLATE
- [SDR DALA2025102407805](https://openairdocs.org/sdr/DALA2025102407805.md): Frame · corroded · Oct 17, 2025 · N131DU · Airbus BD5001A10 · Fuselage Main, Frame
  > INSPECT FORWARD SERVICING AREA PASSENGER COMPARTMENT, WITH GALLEY AND LAVATORY REMOVED. FRAME 20 FWD SIDE OF FRAME HOLE 1, 4, 5, 6, 7, 8. HAVE CORROSION. LOG-PAGE UPDATED @ 17OCT25 1934 UTC 02 CORR BY GILMORE 00473815 MSP 17OCT25 ATA 5321 RII: N ENTR 00532877
- [SDR DALA2026031101710](https://openairdocs.org/sdr/DALA2026031101710.md): Seat Track · corroded · Oct 15, 2025 · N131DU · Airbus BD5001A10 · Wing, Attach Fittings
  > FWD FUSELAGE SEAT TRACK CORROSION LBL 23.0 AT FRAME 22. SSI: 53- 21-43-01. NO EVIDENCE OF PREVIOUS RE-WORK OR REPAIR NOTED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0571:5321-2021/004 00306 ACCOMPLISHED PRI 629312-14 REV 0, REV 1, REV 2, AND ERA 629321-14
- [SDR DALA2026031101709](https://openairdocs.org/sdr/DALA2026031101709.md): Seat Track · corroded · Oct 6, 2025 · N131DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > FWD FUSELAGE SEAT TRACK CORROSION RBL 23.0 AT FRAME 20. SSI: 53- 21-43-01. NO EVIDENCE OF PREVIOUS RE-WORK OR REPAIR NOTED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0571:5321-2021/002 00304 COMPLIED WITH PRI 629359-14 REVISION 0 AND ER/A 629359-14 REVISIO
- [SDR DALA2026031101708](https://openairdocs.org/sdr/DALA2026031101708.md): Seat Track · corroded · Sep 30, 2025 · N131DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AFT FUSELAGE SEAT TRACK CORROSION RBL 43.5 AT FRAME 72 AND EXTENDING UNDER NICKEL MAT. SSI: 53-61-43-01. NO EVIDENCE OF PREVIOUS RE-WORK OR REPAIR NOTED. COMPLIED WITH PRI 629430-14 REVISION 0 AND ER/A 629430-14 REVISION ORIGINAL. (LP# 1227036)
- [SDR DALA2026031101707](https://openairdocs.org/sdr/DALA2026031101707.md): Seat Track · corroded · Sep 30, 2025 · N131DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > FWD FUSELAGE SEAT TRACK CORROSION LBL 43.5 AT FRAME 22. SSI: 53- 21-43-01. NO EVIDENCE OF PREVIOUS RE-WORK OR REPAIR NOTED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0571:5321-2021/005 00307 COMPLIED WITH PRI 629427-14 REVISION 0 AND ER/A 629427-14 REVISIO
- [SDR DALA2025100607256](https://openairdocs.org/sdr/DALA2025100607256.md): Panel · cracked · Sep 30, 2025 · N131DU · Airbus BD5001A10 · Escape Slide
  > RIGHT OVERWING EMERGENCY EXIT DOOR SLIDE (OWEED) PANEL TE (DAMAGED) CRACKS AND DELAMINATED. REMOVED AND REPLACED RT OWEED SLIDE PER AMDS 2563-4005. (LP# 1226999)
- [SDR DALA2025093007110](https://openairdocs.org/sdr/DALA2025093007110.md): Door Sill · corroded · Sep 26, 2025 · N131DU · Airbus BD5001A10 · Fuselage Main, Structure
  > AFT PASSENGER DOOR SILL HAS 6 LOCATIONS WITH SURFACE CORROSION AT OR NEAR THE SILL/ CORNER STRIKER FASTENER HOLES. HOLES 2, 3, 4, 11, 12, 14 COUNTING FWD TO AFT FROM FR 74- FR76. AREAS ARE MARKED AND SEE PHOTO FOR REFERENCE. SSI: 53-61-23-02. COMPLETE: REMOV
- [SDR DALA2025093007111](https://openairdocs.org/sdr/DALA2025093007111.md): Panel · delaminated · Sep 25, 2025 · N131DU · Airbus BD5001A10 · Escape Slide
  > LEFT OVERWING EMERGENCY EXIT DOOR SLIDE PANEL TE NUT PLATE MOUNTING SURFACE (DELAMINATED). REMOVED AND REPLACED OWEED SLIDE PER AMDS 2563-4002. (1217547)
- [SDR DALA2025092507001](https://openairdocs.org/sdr/DALA2025092507001.md): Seat Track · corroded · Sep 20, 2025 · N131DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AFT FUSELAGE SEAT TRACK CORROSION RBL 23.0 AT FRAME 72 AND EXTENDING UNDER NICKEL MAT. NO EVIDENCE OF PREVIOUS RE-WORK OR REPAIR NOTED. REMOVED AND REPLACED TRACK REF A220 ASRP 51-77-00. (LP# 1209371)
- [SDR DALA2025092507000](https://openairdocs.org/sdr/DALA2025092507000.md): Seat Track · corroded · Sep 20, 2025 · N131DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AFT FUSELAGE SEAT TRACK CORROSION LBL 43.5 AT FRAMES 71-72 AND EXTENDING UNDER NICKEL MAT. SSI: 53-61-43-01. NO EVIDENCE OF PREVIOUS RE-WORK OR REPAIR NOTED. (M)(P). REMOVED AND REPLACED TRACK REF A220 ASRP 51-77-00.
- [SDR DALA2025070805081](https://openairdocs.org/sdr/DALA2025070805081.md): Engine · leaking · Jul 8, 2025 · N131DU · Airbus BD5001A10 · Engine (Turbine/Turboprop)
  > SHIP 8131 RETURNED TO SEA DUE TO DIRTY SOCK SMELL IN COCKPIT AND CABIN. CORRECTIVE ACTION: C/W W/C 0550-2001 & DETERMINED SOURCE TO BE #1 ENGINE. C/W W/C 0550-6001 AND W/C 0550-2003. FOUND NO EVIDENCE OF OIL CONTAMINATION. BOTH RECIRCULATION FILTERS REPLACED.
- [SDR DALA2025040802747](https://openairdocs.org/sdr/DALA2025040802747.md): Slat Track · corroded · Apr 4, 2025 · N131DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK #7 RACK TEETH #2 HAS EVIDENCE OF CORROSION AND NO PREVIOUS REWORK. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W ERA 625504-14AD REV O AND PRI 625504-14AD REV O. (LP# 0894319)
- [SDR DALA2025040802741](https://openairdocs.org/sdr/DALA2025040802741.md): Slat Track · no discrepancy · Apr 2, 2025 · N131DU · Airbus BD5001A10 · Standard Practices/Structures
  > RH SLAT TRACK #10 REQUIRES EDDY CURRENT INSPECTION TO BLENDED AREAS, CHECK FOR SIGNED OF CRACKS. UPPER FWD SURFACE. PERFORMED HFEEC ON RH SLAT TRACK #10 UPPER FWD SURFACE PER A220 ANDTP J51-01-20. QC5257 453307. (LP# 0890757)
- [SDR DALA2025030501719](https://openairdocs.org/sdr/DALA2025030501719.md): Engine · odor · Mar 3, 2025 · N131DU · Airbus BD5001A10 · Engine (Turbine/Turboprop)
  > SHIP 8131 -ATB- RETURNED BOS DUE TO DIRTY SOCK SMELL ON CLIMB OUT. CORRECTIVE ACTION: T/S PER ODI WORKCARDS. C/C/O BORESCOPE INSP OF ENGINES. FOUND SLIGHT STAINING ON NBR 2 ENGINE HPC BLADES. ENGINE CHANGED. (LP# 6481648, 0837145, 0837812, 6481657)
- [SDR DALA2025030501717](https://openairdocs.org/sdr/DALA2025030501717.md): Filter · odor · Feb 28, 2025 · N131DU · Airbus BD5001A10 · Air Distribution System
  > MOMENTARY MOIST TYPE SMELL ON CLIMB OUT. DISSIPATED QUICKLY. MOMENTARY SULPHUR TYPE SMELL ON INITIAL THRUST REDUCTION FOR DESCENT. DISSIPATED QUICKLY. NO SMELLS AFTER LANDING. PERFORMED TROUBLESHOOTING OF SMELL OF SMOKE OR FUMES IN THE COCKPIT/CABIN IAW AMDS
- [SDR DALA2025021001041](https://openairdocs.org/sdr/DALA2025021001041.md): Light · inoperative · Feb 5, 2025 · N131DU · Airbus BD5001A10 · Emergency Lighting
  > FOUND LT FWD OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED LT FWD OVERWING EMERGENCY LIGHT PER A220 AMP 33-55, OPS CHECK GOOD. (LP# 6772569)
- [SDR DALA2025012900711](https://openairdocs.org/sdr/DALA2025012900711.md): Power Unit · contaminated · Jan 23, 2025 · N131DU · Airbus BD5001A10 · Electrical Power System
  > AFT FLIGHT ATTENDANT REPORTED PLASTIC RUBBER BURNING SMELL ON DESCENT. IT WENT AWAY THEN FORWARD FLIGHT ATTENDANT HAD SIMILAR SMELL, AND IT WENT AWAY. I SMELLED SLIGHT SMELL FOR OF FEW MOMENTS IN THE COCKPIT AND IT WENT AWAY. UPON OPENING L1 THE SMELL WAS PRES
- [SDR DALA2024121011578](https://openairdocs.org/sdr/DALA2024121011578.md): Oil System · leaking · Dec 9, 2024 · N131DU · Airbus BD5001A10 · Turbine Engine Oil System
  > SHIP 8131 -ATB- PERFORMED AN AIR TURN BACK TO JAX DUE TO LEFT ENGINE OIL QUANTITY LOW INDICATION. CORRECTIVE ACTION: ENGINE REPLACED. (LP# 0701574)
- [SDR DALA2024102810434](https://openairdocs.org/sdr/DALA2024102810434.md): Unknown · odor · Oct 26, 2024 · N131DU · Airbus BD5001A10 · Air Distribution System
  > FUMES NOTED IN FLIGHT DECK AND FWD CABIN DURING DESCENT. ALT 15000' CHEMICAL SMELL. PERFORMED SMOKE AND FUMES IN COCKPIT CHK PER W/C 0550-2001. NO DEFECTS NOTED. R/R RECIRCULATION FILTERS IAW A220 AMP 21-22. RE-PERFORMED SMOKE AND FUMES IN COCKPIT CHK PER W/C
- [SDR DALA2024101510106](https://openairdocs.org/sdr/DALA2024101510106.md): Shutoff Valve · faulted · Oct 9, 2024 · N131DU · Airbus BD5001A10 · Air Distribution System
  > F/A REPORTED ODOR IN CABIN. T/S TO NBR 1 ENGINE. R/R PRSOV IAW A220 AMP 36-11. "M" PROCEDURE REVERSED OPS TEST NORMAL. (LP# 6417756)
- [SDR DALA2024101109976](https://openairdocs.org/sdr/DALA2024101109976.md): Engine · odor · Oct 9, 2024 · N131DU · Airbus BD5001A10 · Engine (Turbine/Turboprop)
  > FA ADVISED FUMES IN REAR OF AIRCRAFT WHEN CONFIGURING FOR APPROACH. FUMES HAD A CHEMICAL SMELL AND MADE THEM FEEL LIGHT HEADED. T/S PER A220 SMOKE AND FUMES W/C 0550-2001. NO FAULTS IN OMS. FOUND OIL SMELL W/ #1 ENG AS BLEED SOURCE. #1 ENG HAS HISTORY OF HOC.
- [SDR DALA2024091609038](https://openairdocs.org/sdr/DALA2024091609038.md): Slat Track · corroded · Sep 12, 2024 · N131DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 11 LWR AFT SURFACE FOUND WITH CORROSION AND BLENDED PER AMDS W/C 5742-01028-02A, REQUIRES NDT INSPECTION FOR SIGNS OF CRACKS. PERFORMED EDDY CURRENT INSPECTION IAW ANDTP 51-01-20-01AAA- 353A-A NO DEFECTS NOTED. (LP# 0551977)
- [SDR DALA2024091609037](https://openairdocs.org/sdr/DALA2024091609037.md): Slat Track · corroded · Sep 12, 2024 · N131DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 7 LWR INB SURFACE FOUND WITH CORROSION AND BLENDED PER AMDS W/C 5742-01028-02A, REQUIRES NDT INSPECTION FOR SIGNS OF CRACKS. PERFORMED EDDY CURRENT INSPECTION IAW ANDTP 51-01-20-01AAA- 353A-A NO DEFECTS NOTED. (LP# 0551974)
- [SDR DALA2024091609036](https://openairdocs.org/sdr/DALA2024091609036.md): Slat Track · corroded · Sep 12, 2024 · N131DU · 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 FOR SIGNS OF CRACKS. PERFORMED EDDY CURRENT INSPECTION IAW ANDTP 51-01-20-01AAA- 353A-A NO DEFECTS NOTED. (LP# 0551972)
- [SDR DALA2024091609035](https://openairdocs.org/sdr/DALA2024091609035.md): Slat Track · corroded · Sep 12, 2024 · N131DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 4 UPPER AFT SURFACE FOUND WITH CORROSION AND BLENDED PER AMDS W/C 5742-01028-02A, REQUIRES NDT INSPECTION FOR SIGNS OF CRACKS. PERFORMED EDDY CURRENT INSPECTION IAW ANDTP 51-01-20-01AAA- 353A-A NO DEFECTS NOTED. (LP# 0551971)
- [SDR DALA2024091609034](https://openairdocs.org/sdr/DALA2024091609034.md): Slat Track · corroded · Sep 12, 2024 · N131DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 6 UPPER AFT SURFACE FOUND WITH CORROSION AND BLENDED PER AMDS W/C 5742-01028-02B, REQUIRES NDT INSPECTION FOR SIGNS OF CRACKS. PERFORMED EDDY CURRENT INSPECTION IAW ANDTP 51-01-20-01AAA- 353A-A NO DEFECTS NOTED. (LP# 0551970)
- [SDR DALA2024091609033](https://openairdocs.org/sdr/DALA2024091609033.md): Slat Track · corroded · Sep 12, 2024 · N131DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 5 UPPER FWD SURFACE FOUND WITH CORROSION AND BLENDED PER AMDS W/C 5742-01028-02B, REQUIRED NDT INSPECTION FOR SIGNS OF CRACKS. PERFORMED EDDY CURRENT INSP IAW ANDTP 51-01-20-01AAA-353A-A NO DEFECTS NOTED. (LP# 0551956)
- [SDR DALA2024091609032](https://openairdocs.org/sdr/DALA2024091609032.md): Slat Track · corroded · Sep 12, 2024 · N131DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 2 LOWER AFT SURFACE FOUND WITH CORROSION AND BLENDED PER AMDS W/C 5742-01028-02B, REQUIRED NDT INSPECTION FOR SIGNS OF CRACKS. PERFORMED EDDY CURRENT INSPECTION IAW ANDTP 51-01-20-01AAA- 353A-A NO DEFECTS NOTED. (LP# 0551952)
- [SDR DALA2024090608788](https://openairdocs.org/sdr/DALA2024090608788.md): Light · inoperative · Sep 3, 2024 · N131DU · Airbus BD5001A10 · Emergency Lighting
  > ON SVC CHECK FOUND 1R DOOR EXTERNAL EMERGENCY LIGHT INOP. R/R 1R EXTERNAL EMERGENCY LIGHT PER A220 AMP 33-55. OPS CHECK GOOD. (LP# 5721704)
- [SDR DALA2024021502207](https://openairdocs.org/sdr/DALA2024021502207.md): Skin · corroded · Feb 12, 2024 · N131DU · Airbus BD5001A10 · Leading Edge Devices
  > L/H SLAT NBR 10 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 12FEB24 2023 UTC 02 CORR BY SMITH 02161591 IAH 12FEB24 ATA 5742 RII: N ENTR
- [SDR DALA2024021402186](https://openairdocs.org/sdr/DALA2024021402186.md): Slat Track · corroded · Feb 12, 2024 · N131DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 9 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 9 LOWER AFT SURFACE IAW ER/A 608500- 14AD REV A AND PRI 608500-14AD REV 0 MATCHED. (LP# 0199041)
- [SDR DALA2024021402185](https://openairdocs.org/sdr/DALA2024021402185.md): Slat Track · corroded · Feb 12, 2024 · N131DU · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 5 LOWER FWD I/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED R/H SLAT TRACK NBR 5 LOWER FWD I/B SIDE IAW ER/A 608500 -14AD REV A AND PRI 608500-14AD REV 0 MATCHED. (LP# 0199040)
- [SDR DALA2024021402184](https://openairdocs.org/sdr/DALA2024021402184.md): Slat Track · corroded · Feb 12, 2024 · N131DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 11 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 12FEB24 2202 UTC 02 CORR BY SPURLIN 02405497 IAH 12FEB24 ATA 5742 RII:
- [SDR DALA2024021402183](https://openairdocs.org/sdr/DALA2024021402183.md): Slat Track · corroded · Feb 12, 2024 · N131DU · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED R/H SLAT TRACK NBR 5 UPPER FWD SURFACE IAW ER/A 608500- 14AD REV A AND PRI 608500-14AD REV 0 MATCHED. (LP# 0199038)
- [SDR DALA2024021402182](https://openairdocs.org/sdr/DALA2024021402182.md): Slat Track · corroded · Feb 12, 2024 · N131DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 10 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 10 UPPER FWD SURFACE IAW ER/A 608500- 14AD REV A AND PRI 608500-14AD REV 0 MATCHED. (LP# 0199037)
- [SDR DALA2024021402181](https://openairdocs.org/sdr/DALA2024021402181.md): Slat Track · corroded · Feb 12, 2024 · N131DU · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 5 LOWER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED R/H SLAT TRACK NBR 5 LOWER FWD SURFACE IAW ER/A 608500- 14AD REV A AND PRI 608500-14AD REV 0 MATCHED. (LP# 0199035)
- [SDR DALA2024021402180](https://openairdocs.org/sdr/DALA2024021402180.md): Slat Track · corroded · Feb 12, 2024 · N131DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 9 UPPER AFT O/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 12FEB24 2157 UTC 02 CORR BY SPURLIN 02405497 IAH 12FEB24 ATA 5742 RII:
- [SDR DALA2024021402179](https://openairdocs.org/sdr/DALA2024021402179.md): Slat Track · corroded · Feb 12, 2024 · N131DU · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 4 LOWER FWD O/B SIDE HAS EVIDENCE OF CORROSION AND NO PREVIOUS REWORK REF 5742-01028-02B. REPAIRED R/H SLAT TRACK NBR 4 LOWER FWD O/B SIDE IAW ER/A 608500 -14AD REV A AND PRI 608500-14AD REV 0 MATCHED. (LP# 0199028)
- [SDR DALA2024021402178](https://openairdocs.org/sdr/DALA2024021402178.md): Slat Track · corroded · Feb 12, 2024 · N131DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 9 LOWER FWD I/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 9 LOWER FWD I/B SIDE IAW ER/A 608500- 14AD REV A AND PRI 608500-14AD REV 0 MATCHED. (LP# 0199025)
- [SDR DALA2024021402177](https://openairdocs.org/sdr/DALA2024021402177.md): Slat Track · corroded · Feb 12, 2024 · N131DU · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 4 UPPER AFT I/B SIDE HAS EVIDENCE OF CORROSION AND NO PREVIOUS REWORK REF 5742-01028-02B. REPAIRED R/H SLAT TRACK NBR 4 UPPER AFT I/B SIDE IAW ER/A 608500 -14AD REV A AND PRI 608500-14AD REV 0 MATCHED. (LP# 0199019)
- [SDR DALA2024021402176](https://openairdocs.org/sdr/DALA2024021402176.md): Slat Track · corroded · Feb 12, 2024 · N131DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 8 LOWER FWD I/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 8 LOWER FWD I/B SIDE IAW ER/A 608500- 14AD REV A AND PRI 608500-14AD REV 0 MATCHED. (LP# 0199017)
- [SDR DALA2024021402175](https://openairdocs.org/sdr/DALA2024021402175.md): Slat Track · corroded · Feb 12, 2024 · N131DU · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 4 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION IN TWO SEPERATE LOCATIONS AND NO PREVIOUS REWORK REF 5742-01028 -02B. REPAIRED R/H SLAT TRACK NBR 4 LOWER AFT AT TWO SEPARATE LOCATIONS IAW ER/A 608500-14AD REV A AND PRI 608500-14AD REV 0 MATC
- [SDR DALA2024021402174](https://openairdocs.org/sdr/DALA2024021402174.md): Slat Track · corroded · Feb 12, 2024 · N131DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 7 LOWER FWD I/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 7 LOWER FWD I/B SIDE IAW ER/A 608500- 14AD REV A AND PRI 608500-14AD REV 0 MATCHED. (LP# 0199012)

Next page: https://openairdocs.org/aircraft/N131DU/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 = 'N131DU' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N131DU/reports

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