# Service difficulty reports: N126DU

A list on [N126DU](https://openairdocs.org/aircraft/N126DU.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 · 59 reports

- [SDR DALA2026010400047](https://openairdocs.org/sdr/DALA2026010400047.md): Engine · contaminated · Dec 29, 2025 · N126DU · Airbus BD5001A10 · Engine (Turbine/Turboprop)
  > DIRTY SOCK SMELL BRIEFLY AT 10000 FT DURING CLIMB DIRTY SOCK SMELL RETURNED BRIEFLY AT 25000 FT DURING DECENT AT 10000 FTB WITH ENGINES AT IDLE SMELL RETURNED GOT STRONG UNTILL POWER INCREASED ABOVE IDDLE, THEN DISSIPATED SMELL NOTED IN FWD GALLEY - NO SMELL M
- [SDR DALA2025122309352](https://openairdocs.org/sdr/DALA2025122309352.md): Unknown · odor · Dec 18, 2025 · N126DU · Airbus BD5001A10 · Air Distribution System
  > CHEMICAL SMELL IN AFT GALLEY AFTER T/O. DESCRIBED AS PLASTIC TYPE ODOR. ON LANDING TURNED INTO DIRTY SOCK ODOR AND REPORTED STRONG BY FA'S. ALSO REPORTING MILD HEADACHES. NO ODORS IN FLT DECK. C/W ER/A 613840-14TR REV B SEC II. WATER WASH DUE WITHIN 5 DAYS. TH
- [SDR DALA2025090206506](https://openairdocs.org/sdr/DALA2025090206506.md): Pan · corroded · Sep 1, 2025 · N126DU · Airbus BD5001A10 · Fuselage Main, Structure
  > CORROSION ON WASTE BOX PAN ASSEMBLY INTERNAL SIDE OF AIRCRAFT. C/W ER/A 602871-14AD REV-A. ASSOCIATED ER/A 14-602871. (LP# 1176621)
- [SDR DALA2025090206495](https://openairdocs.org/sdr/DALA2025090206495.md): Threshold · corroded · Aug 27, 2025 · N126DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > ***CORROSION*** AFT RH SERVICE DOOR THRESHOLD SILL FLOOR PANEL, CORROSION I/B, AFT FASTENER HOLE FR76. REMOVED AND REPLACED AFT SERVICE DOOR FLOOR PANEL IAW A220 AMP BD500-A-J53-00-47-14AAA-720A-A J. (LP# 1167346)
- [SDR DALA2025090206487](https://openairdocs.org/sdr/DALA2025090206487.md): Light · inoperative · Aug 25, 2025 · N126DU · Airbus BD5001A10 · Emergency Lighting
  > LH AFT FUSELAGE EXTERNAL EMER LIGHT INOP. REMOVED AND INSTALLED NEW LH AFT FUSELAGE EXTERNAL EMERGENCY LIGHT, OP CHECK GOOD, I.A.W A220 AMP BD500-A-J33-55-02-01AAA- 720A-A. (LP# 1163012)
- [SDR DALA2025090206486](https://openairdocs.org/sdr/DALA2025090206486.md): Light · inoperative · Aug 25, 2025 · N126DU · Airbus BD5001A10 · Emergency Lighting
  > RH AFT FUSELAGE EXTERNAL EMER LIGHT INOP. REMOVED AND INSTALLED NEW RH AFT FUSELAGE EXTERNAL EMERGENCY LIGHT I.A.W A220 AMP BD500-A-J33-55-02-01AAA-720A-A. OP CHECK GOOD. (LP# 1163004)
- [SDR DALA2025090206485](https://openairdocs.org/sdr/DALA2025090206485.md): Light · inoperative · Aug 25, 2025 · N126DU · Airbus BD5001A10 · Emergency Lighting
  > RH FWD OVERWING EXTERNAL EMER LIGHT INOP. REMOVED AND INSTALLED NEW EMERGENCY LIGHT, OP CHECK GOOD I.A.W A220 AMP BD500-A-J33-55-02-02AAA-720-A. (LP# 1162987)
- [SDR DALA2025082506309](https://openairdocs.org/sdr/DALA2025082506309.md): Door Sill · corroded · Aug 20, 2025 · N126DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > CORROSION FWD CARGO DOOR LWR SILL HAS CORROSION AROUND FASTENER HOLES 1, 2, 4, 5, 6, 7, 9, 11, 13, 15, 16, 18, AND 19. C/W ER/A 628608-14 REV ORIGINAL ASSOCIATED ER/A 14-628608 ADDED FOR AC 8126. (LP# 1154272)
- [SDR DALA2025082506308](https://openairdocs.org/sdr/DALA2025082506308.md): Seat Track · corroded · Aug 20, 2025 · N126DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON PASSENGER CABIN SEAT TRACK RBL 44 FR 74. REMOVED AND REPLACED CABIN SEAT TRACK RBL 44 FR 74 REP A220 ASRP BD 500-A-J51-42-20-00AAA-78A AND DWG# C01342701 REV -G. (LP# 1154136)
- [SDR DALA2025082506307](https://openairdocs.org/sdr/DALA2025082506307.md): Seat Track · corroded · Aug 20, 2025 · N126DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON PASSENGER CABIN SEAT TRACK LBL 22 FR 74. REMOVED AND REPLACED SEAT TRACK AT LBL 23 BETWEEN FR 62 TO FR 74 I.A.W. A220 ASRP BD500-A-J51-42-20-00AAA-078A-A AND BOMBARDIER DWG# C01342701 REV G. (LP# 1153498)
- [SDR DALA2025082106245](https://openairdocs.org/sdr/DALA2025082106245.md): Floor Panel · corroded · Aug 18, 2025 · N126DU · Airbus BD5001A10 · Fuselage Floor Panel
  > AFT SERVICE ENTRY DOOR LOWER FLOOR PANEL CORRODED. REMOVED FLOOR PANEL AFT SERVICE DOOR DAMAGED AND INSTALLED NEW FLOOR PANEL AFT SERVICE DOOR I.A.W A220 AMP BD500-A-AJ53-00-47- 14AAA-720A-A. (LP# 1150576)
- [SDR DALA2025082006224](https://openairdocs.org/sdr/DALA2025082006224.md): Seat Track · corroded · Aug 16, 2025 · N126DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON PASSENGER CABIN SEAT TRACK RBL 22 FR 74. REMOVED DAMAGED SEAT TRACK FROM PASSENGER CABIN RBL 22 BETWEEN FR 62 TO FR 74 AND REPLACED PER A220 ASRP BD500-A-J51-42-21- 00AAA-078A-A AND BOMBARDIER PL C01342701 REV-G. (LP# 1146804)
- [SDR DALA2025082006223](https://openairdocs.org/sdr/DALA2025082006223.md): Seat Track · corroded · Aug 16, 2025 · N126DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON PASSENGER CABIN SEAT TRACK RBL 44 BETWEEN FR20 TO FR22. REMOVED DAMAGED SEAT TRACK ON PASSENGER CABIN AT RBL 44 FROM FR 20 TO FR 30 AND REPLACED PER A220 ASRP BD500-A-J51-42-21-00AAA- 078A-A AND BOMBARDIER PL C02312600 REV-E. (LP# 1146767)
- [SDR DALA2025081906216](https://openairdocs.org/sdr/DALA2025081906216.md): Support · gouged · Aug 15, 2025 · N126DU · Airbus BD5001A10 · Aerodynamic Fairings
  > THREE GOUGES ON WTBF SUPPORT STRUCTURE AT FR38, BETWEEN RBL25 AND RBL30. REMOVED AND REPLACED WING TO BODY SUPPORT P/N: C02381124-002, PO:1049347 IAW A220 ASRP BD500-A-J51-42-21-00AAA-078A-A. AT FR 38 RH SIDE BETWEEN RBL 25 AND RBL 30. (LP# 1145374)
- [SDR DALA2025081906211](https://openairdocs.org/sdr/DALA2025081906211.md): Seat Track · corroded · Aug 14, 2025 · N126DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON PASSENGER CABIN SEAT TRACK RBL 22 BETWEEN FR20 TO FR 22. REMOVED AND REPLACED SEAT TRACK AT RBL 23 FR20-30 IAW BOMBARDIER DWG C02312600 REV E. (LP# 1142990)
- [SDR DALA2025081906209](https://openairdocs.org/sdr/DALA2025081906209.md): Seat Track · corroded · Aug 12, 2025 · N126DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > MULTIPLE SPOTS OF CORROSION ON PASSENGER CABIN SEAT TRACK AT LBL 44 BTW FR 67 TO FR 74. REMOVED AND INSTALLED REPLACEMENT PASSENGER CABIN SEAT TRACK LBL 44 FR 62 TO FR 74 PER A220 ASRP BD 500 - A - J51 - 42 -20 - 00AAA - 078A -A AND BOMBARDIER DWG # C01342701
- [SDR DALA2025012900710](https://openairdocs.org/sdr/DALA2025012900710.md): Unknown · odor · Jan 24, 2025 · N126DU · Airbus BD5001A10 · Air Distribution System
  > IN DESCENT FA'S COMPLAINED ABOUT STINKY SOCK SMELL IN AFT GALLEY. ENG/APU OILS & HYD LEVELS CHK OK. UNABLE TO ISOLATE. IDENTIFY FUMES IN REF TO AMDS WORKCARD 0550-2001. (LP# 6679984, 0775652)
- [SDR DALA2024091909193](https://openairdocs.org/sdr/DALA2024091909193.md): Slat Track · worn · Sep 18, 2024 · N126DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK #4 I/B UPPER AND O/B LOWER SIDE ROLLERS SEIZED. REMOVED LH SLAT TRACK #4 I/B UPPER AND O/B LOWER SIDE ROLLERS PER A220 AMP 27-81-02. INSTALLED SLAT TRACK #4 I/B UPPER AND O/B LOWER SIDE ROLLERS PER A220 AMP 27-81-02 STEPS 1A - 1C. COMPLETED S
- [SDR DALA2024091909192](https://openairdocs.org/sdr/DALA2024091909192.md): Slat Track · worn · Sep 18, 2024 · N126DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 4 UPPER FWD SURFACE REQUIRES NDT INSPECTION PER AMDS W/C 5742-01028-02A. LOG-PAGE UPDATED @ 18SEP24 0153 UTC 02 CORR BY HENDRICK 02372882 IAH 18SEP24 ATA 5742 ENTR 02420359 W LOG-PAGE UPDATED @ 18SEP24 0153 UTC 03 CORR BY MCDONALD 00750016 IA
- [SDR DALA2024091909191](https://openairdocs.org/sdr/DALA2024091909191.md): Slat Track · worn · Sep 18, 2024 · N126DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 4PINION TEETH (2EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 18SEP24 0147 UTC 02 CORR BY HARMON 02420359 IAH 18SEP24 ATA 5742 RII
- [SDR DALA2024091909190](https://openairdocs.org/sdr/DALA2024091909190.md): Slat Track · worn · Sep 18, 2024 · N126DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 4 RACK TEETH (2EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 18SEP24 0139 UTC 02 CORR BY HARMON 02420359 IAH 18SEP24 ATA 5742 RII:
- [SDR DALA2024091909189](https://openairdocs.org/sdr/DALA2024091909189.md): Slat Track · worn · Sep 18, 2024 · N126DU · Airbus BD5001A10 · Leading Edge Devices
  > LH WING NBR 4 SLAT TRACK FOUND EXCESSIVE ROLLER WEAR MARKS. LOG-PAGE UPDATED @ 18SEP24 0125 UTC 02 CORR BY AYALA AGUI 00917586 IAH 18SEP24 ATA 5742 ENTR 02420359 W LOG-PAGE UPDATED @ 18SEP24 0125 UTC 03 CORR BY MCDONALD 00750016 IAH 18SEP24 ATA 5742 RII: Y ENT
- [SDR DALA2024091709092](https://openairdocs.org/sdr/DALA2024091709092.md): Slat Track · no discrepancy · Sep 16, 2024 · N126DU · Airbus BD5001A10 · Leading Edge Devices
  > RH #10 SLAT TRACK UPPER AFT O/B REQUIRE NDT INSPECTION PER AMDS 5742-01028-02B. PERFORMED EDDY CURRENT INSPECTION IAW A220 ANDTP BD500-4-J51-01- 20-01AAA-353A-A. NO CRACKS NOTED.
- [SDR DALA2024091709091](https://openairdocs.org/sdr/DALA2024091709091.md): Slat Track · no discrepancy · Sep 16, 2024 · N126DU · Airbus BD5001A10 · Leading Edge Devices
  > RH #10 SLAT TRACK UPPER AFT I/B REQUIRE NDT INSPECTION PER AMDS 5742-01028-02B. PERFORMED EDDY CURRENT INSPECTION IAW A220 ANDTP BD500-4-J51-01- 20-01AAA-353A-A. (LP# 0560037)
- [SDR DALA2024091709090](https://openairdocs.org/sdr/DALA2024091709090.md): Slat Track · no discrepancy · Sep 16, 2024 · N126DU · Airbus BD5001A10 · Leading Edge Devices
  > RH #8 SLAT TRACK LOWER FWD EDGE REQUIRE NDT INSPECTION PER AMDS 5742-01028-02B. PERFORMED EDDY CURRENT INSPECTION IAW A220 ANDTP BD500-4-J51-01- 20-01AAA-353A-A. NO CRACKS NOTED. (LP# 0560033)
- [SDR DALA2024091709089](https://openairdocs.org/sdr/DALA2024091709089.md): Slat Track · no discrepancy · Sep 16, 2024 · N126DU · Airbus BD5001A10 · Leading Edge Devices
  > RH #5 SLAT TRACK LOWER AFT EDGE REQUIRE NDT INSPECTION PER AMDS 5742-01028-02B. PERFORMED EDDY CURRENT INSPECTION IAW A220 ANDTP BD500-4-J51-01- 20-01AAA-353A-A. NO CRACKS NOTED. (LP# 0560030)
- [SDR DALA2024091709088](https://openairdocs.org/sdr/DALA2024091709088.md): Slat Track · no discrepancy · Sep 16, 2024 · N126DU · Airbus BD5001A10 · Leading Edge Devices
  > RH #5 SLAT TRACK LOWER FWD EDGE REQUIRE NDT INSPECTION PER AMDS 5742-01028-02B. PERFORMED EDDY CURRENT INSPECTION IAW A220 ANDTP BD500-4-J51-01- 20-01AAA-353A-A. NO CRACKS NOTED. (LP# 0560025)
- [SDR DALA2024091709087](https://openairdocs.org/sdr/DALA2024091709087.md): Slat Track · no discrepancy · Sep 16, 2024 · N126DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 5 LOWER FWD SURFACE REQUIRES NDT INSPECTION PER AMDS W/C 5742-01-28-02A. PERFORMED EDDY CURRENT INSPECTION IAW A220 ANDTP BD500-4-J51-01- 20-01AAA-353A-A. NO CRACKS NOTED. (LP# 0559977)
- [SDR DALA2024091709086](https://openairdocs.org/sdr/DALA2024091709086.md): Slat Track · no discrepancy · Sep 16, 2024 · N126DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 7 UPPER FWD SURFACE REQUIRES NDT INSPECTION PER AMDS W/C 5742-01-28-02A LOG-PAGE. PERFORMED EDDY CURRENT INSPECTION IAW A220 ANDTP BD500-4-J51-01- 20-01AAA-353A-A. NO CRACKS NOTED.
- [SDR DALA2024091709085](https://openairdocs.org/sdr/DALA2024091709085.md): Slat Track · unknown · Sep 16, 2024 · N126DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 8 LOWER FWD SURFACE REQUIRES NDT INSPECTION PER AMDS W/C 5742-01-28-02A LOG-PAGE. PERFORMED EDDY CURRENT INSPECTION IAW A220 ANDTP BD500-4-J51-01- 20-01AAA-353A-A.
- [SDR DALA2024022302541](https://openairdocs.org/sdr/DALA2024022302541.md): Slat Track · corroded · Feb 19, 2024 · N126DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 5 UPPER AFT O/B SIDE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. MEASURED LH SLAT TRACK NBR 5 UPPER AFT O/B SIDE IAW ER/A 608364- 14AD REV B AND PRI 60836
- [SDR DALA2024022302540](https://openairdocs.org/sdr/DALA2024022302540.md): Slat Track · corroded · Feb 19, 2024 · N126DU · 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. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. MEASURED LH SLAT TRACK NBR 4 UPPER AFT I/B SIDE IAW ER/A 608364- 14AD REV B AND PRI 60836
- [SDR DALA2024022302539](https://openairdocs.org/sdr/DALA2024022302539.md): Slat Track · corroded · Feb 19, 2024 · N126DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 11 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 11 LOWER AFT SURFACE IAW ER/A 608364- 14AD REV B AND PRI
- [SDR DALA2024022302538](https://openairdocs.org/sdr/DALA2024022302538.md): Slat Track · corroded · Feb 19, 2024 · N126DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 10 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 10 LOWER AFT SURFACE IAW ER/A 608364- 14AD REV B AND PRI
- [SDR DALA2024022302537](https://openairdocs.org/sdr/DALA2024022302537.md): Slat Track · corroded · Feb 19, 2024 · N126DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 9 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 9 LOWER AFT SURFACE IAW ER/A 608364- 14AD REV B AND PRI
- [SDR DALA2024022302536](https://openairdocs.org/sdr/DALA2024022302536.md): Slat Track · corroded · Feb 19, 2024 · N126DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 8 LOWER FWD I/B SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 8 LOWER FWD I/B SIDE IAW ER/A 608364- 14AD REV B AND
- [SDR DALA2024022302535](https://openairdocs.org/sdr/DALA2024022302535.md): Slat Track · corroded · Feb 19, 2024 · N126DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 7 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 7 LOWER AFT SURFACE IAW ER/A 608364- 14AD REV B AND PRI
- [SDR DALA2024022302534](https://openairdocs.org/sdr/DALA2024022302534.md): Slat Track · corroded · Feb 19, 2024 · N126DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 6 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 6 LOWER AFT SURFACE IAW ER/A 608364- 14AD REV B AND PRI
- [SDR DALA2024022302533](https://openairdocs.org/sdr/DALA2024022302533.md): Slat Track · corroded · Feb 19, 2024 · N126DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 5 UPPER FWD SURFACE IAW ER/A 608364- 14AD REV B AND PRI 6
- [SDR DALA2024022302532](https://openairdocs.org/sdr/DALA2024022302532.md): Slat Track · corroded · Feb 19, 2024 · N126DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 3 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 3 LOWER AFT SURFACE IAW ER/A 608364- 14AD REV B AND PRI
- [SDR DALA2024022302531](https://openairdocs.org/sdr/DALA2024022302531.md): Slat Track · corroded · Feb 19, 2024 · N126DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 3 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 3 UPPER FWD SURFACE IAW ER/A 608364- 14AD REV B AND PRI 6
- [SDR DALA2024022302530](https://openairdocs.org/sdr/DALA2024022302530.md): Slat Track · corroded · Feb 19, 2024 · N126DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 2 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 2 UPPER FWD SURFACE IAW ER/A 608364- 14AD REV B AND PRI 60
- [SDR DALA2024022302529](https://openairdocs.org/sdr/DALA2024022302529.md): Slat Track · corroded · Feb 19, 2024 · N126DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 1 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION IN 2 AREAS AND PREVIOUS REWORK, REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 1 UPPER FWD SURFACE IN 2 AREAS IAW ER /A 608364
- [SDR DALA2024022302528](https://openairdocs.org/sdr/DALA2024022302528.md): Slat Track · corroded · Feb 19, 2024 · N126DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 5 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. LIAISON ENGINEERING WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NBR 5 UPPER FWD SURFACE IAW ER/A 608363- 14AD REV B AND PRI 608363-14A
- [SDR DALA2024022302527](https://openairdocs.org/sdr/DALA2024022302527.md): Slat Track · corroded · Feb 19, 2024 · N126DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. LIAISON ENGINEERING WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NBR 4 UPPER AFT SURFACE IAW ER/A 608363- 14AD REV B AND PRI 608363-14A
- [SDR DALA2024022302526](https://openairdocs.org/sdr/DALA2024022302526.md): Slat Track · corroded · Feb 19, 2024 · N126DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 3 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. LIAISON ENGINEERING WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NBR 3 UPPER FWD SURFACE IAW ER/A 608363- 14AD REV B AND PRI 608363-14A
- [SDR DALA2024022302525](https://openairdocs.org/sdr/DALA2024022302525.md): Slat Track · corroded · Feb 19, 2024 · N126DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 2 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. LIAISON ENGINEERING WILL BE REQUIRED BEFORE FURTHER FLIGHT. REPAIRED RH SLAT TRACK NBR 2 UPPER FWD SURFACE IAW ER/A 608363- 14AD REV B AND PRI 608363-14AD
- [SDR DALA2024022302524](https://openairdocs.org/sdr/DALA2024022302524.md): Slat Track · corroded · Feb 19, 2024 · N126DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 1 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. LIAISON ENGINEERING WILL BE REQUIRED BEFORE FURTHER FLIGHT. LOG-PAGE UPDATED @ 19FEB24 0121 UTC 02 CORR BY SPURLIN 02405497 IAH 19FEB24 ATA 5742 RII: N ENT
- [SDR DALA2023110709155](https://openairdocs.org/sdr/DALA2023110709155.md): Unknown · unknown · Nov 6, 2023 · N126DU · Airbus BD5001A10 · Air Distribution System
  > ACRID SMELL IN FLIGHT DECK AND CABIN AREA. SMELL WENT AWAY WHEN I TURNED OFF APU BLEED. PREV TECHS FOUND APU OVERSERVICED & CORRECTED SERVICING. EXTERNAL GVI OF ENGINES, AIRFRAME & APU NO LEAKS NOTED. RAN ENGINES WITH CART, NO APU. NO SMELL. ACCOMPLISHED W/C 0
- [SDR DALA2023050103361](https://openairdocs.org/sdr/DALA2023050103361.md): Unknown · unknown · Apr 28, 2023 · N126DU · Airbus BD5001A10 · Leading Edge Devices
  > ERA608364-14AD SECTION I ISSUED FOR CORROSION FINDINGS ON LH WING SLAT TRACKS 1-11. FOLLOW ON ACTION REQUIRED. ACCOMPLISH SECTION II EVERY 850FH FROM SECTION I UNTIL SECTION III. SECTION III REQUIRED PRIOR TO 8500FH FROM SECTION I. ASSOCIATED AA 5742-01028 ADD

Next page: https://openairdocs.org/aircraft/N126DU/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 = 'N126DU' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N126DU/reports

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