# Service difficulty reports: N124DU A list on [N124DU](https://openairdocs.org/aircraft/N124DU.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 · 87 reports - [SDR DALA2026091005072](https://openairdocs.org/sdr/DALA2026091005072.md): Skin · dented · Aug 28, 2026 · N124DU · Airbus BD5001A10 · Fuselage Main, Plate/Skin > ER/A 626742-14 REV B, FUSELAGE SKIN, FR 19-20 AND S32L - 33L DENTED. ACCOMPLISH SECTION IV WITHIN 52,500 FLIGHT HOURS OR 30,000 FLIGHT CYCLES FROM TIME OF SECT. III REPAIR AT 15,018 FH AND 6,946 FC (WITHIN AIRCRAFT TOTAL TIME OF 67,518 FH OR 36,946 FC), WHIC - [SDR DALA2026051302997](https://openairdocs.org/sdr/DALA2026051302997.md): Light · inoperative · May 11, 2026 · N124DU · Airbus BD5001A10 · Emergency Lighting > EXTERIOR EMERGENCY LIGHTS SYSTEMS - DOOR EMERGENCY LIGHTS. CORRECTIVE ACTION: R/R FWD L/H, AFT L/H, FWD R/H EXTERIOR EMERGENCY LTS PER A220 AMP 33 -55. OPS CHECK GOOD. PLACARDS REMOVED. (LP#8098296; AIRCRAFT WAS GROUNDED) - [SDR DALA2026051302996](https://openairdocs.org/sdr/DALA2026051302996.md): Light · faulted · May 11, 2026 · N124DU · Airbus BD5001A10 · Emergency Lighting > EXTERIOR EMERGENCY LIGHTS SYSTEMS - OVERWING EMERGENCY LIGHTS. REPLACED LT + RT FWD LIGHT ASSEMBLIES PER AMP 33-55. OPS CK GOOD. PANELS CLOSED. MEL CLEARED, PLACARD + TAB REMOVED. (LP# 8098295; AIRCRAFT WAS GROUNDED) - [SDR DALA2026030401498](https://openairdocs.org/sdr/DALA2026030401498.md): Oil System · overserviced · Mar 1, 2026 · N124DU · Airbus BD5001A10 · Turbine Engine Oil System > DIRTY SOCK SMELL NOTICED IN THE FLIGHT DECK ON FINAL APPROACH SLOWING FROM 170 TO B6 KIAS IT WAS A MOMENTARY STRONG SMELL THEN SLOWLY DISSIPATED. FILLED OUT ODOR FORM. WORKING ON W/C 0550-2001 TO STEP 8. WILL REQUIRE HP ENGINE RUN NEXT. (613097) FOUND #1 ENGIN - [SDR DALA2026030401500](https://openairdocs.org/sdr/DALA2026030401500.md): Filter · odor · Feb 27, 2026 · N124DU · Airbus BD5001A10 · Air Distribution System > DIRTY SOCK ODOR WAS NOTIFIED IN FLIGHT DECK AND BY AFT FA'S ON APPROACH SLOWING FROM 210-190 KNOTS. PILOTS DONNED MASKS. PERFORMED T/S OF SMOKE AND FUMES WITH PTRAK PER WC 0550-2001. NO DISCREPANCIES FOUND ON PERFORMING WC 0550-2003. PTRAK RESULTS SUBMITTED, N - [SDR DALA2025122309353](https://openairdocs.org/sdr/DALA2025122309353.md): Unknown · odor · Dec 19, 2025 · N124DU · Airbus BD5001A10 · Air Distribution System > SMKE - AFTER APU START AND PACKS ON, AN ACRID SMELL AND FA REPORTED SMOKE FILLED THE CABIN. TURNED OFF THE APU AND THE SMOKE/FUMES STOPPED. INSPECTED THE APU INTAKE AND RAN APU WITH SNIFFER TOOL AND FOUND NO CONTAMINATION OR SMELL. NO TROUBLE FOUND. REPLACED - [SDR DALA2025111208280](https://openairdocs.org/sdr/DALA2025111208280.md): Strut · discharged · Nov 8, 2025 · N124DU · Airbus BD5001A10 · Main Landing Gear Strut/Axle/Truck > DECLARED EMERGENCY FOR THE FLIGHT DUE TO WEIGHT ON WHEELS FAULT WITH POSSIBLE LOSS OF NOSE WHEEL STEERING. JACKED A/C. FOUND RT STRUT NOT FULLY EXTENDED. SERVICED RT STRUT, OPS CHECK GOOD. (LP# 8002764) - [SDR DALA2025102107686](https://openairdocs.org/sdr/DALA2025102107686.md): Light · faulted · Oct 16, 2025 · N124DU · Airbus BD5001A10 · Emergency Lighting > FAS REPORT EMERGENCY EXIT INTERIOR LOCATOR LIGHTS DID NOT ILLUMINATE ON LANDING. T/S PER A220 EFIM SOL.# 1-04874, RESET C/BS AND PERFORMED OPS CK OF INTERNAL EMERGENCY LIGHTING SYSTEM PER A220 AMP 33-52-00, OPS CK NML. OK TO CLOSE LOG. (LP# 6995876) - [SDR DALA2025101307464](https://openairdocs.org/sdr/DALA2025101307464.md): Landing Gear · faulted · Oct 6, 2025 · N124DU · Airbus BD5001A10 · Landing Gear Position and Warning > ATB - RETURNED TO MLB DUE TO LEFT MLG GEAR INDICATION. R & R LEFT MLG ASSEMBLY PER AMDS 3210-4001-LH. (LP# 6995824) - [SDR DALA2025100607255](https://openairdocs.org/sdr/DALA2025100607255.md): Door Sill · corroded · Sep 29, 2025 · N124DU · Airbus BD5001A10 · Fuselage Main, Structure > AFT CARGO, LWR DOOR CUTOUT, BETWEEN FR63-FR66, HAS CORROSION AROUND 6 OF THE FASTENER HOLES. REMOVED CORROSION ON AFT CARGO LOWER SILL, FOUND OUT OF LIMITS IAW A220 ASRP J51-21-06 AND J53-61-25. RESTORED FINISH AND PERFORMED ALL WORK IAW ERA 629474-14 REV. ORI - [SDR DALA2025100207156](https://openairdocs.org/sdr/DALA2025100207156.md): Scuff Plate · corroded · Sep 28, 2025 · N124DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure > AFT CARGO DOOR SCUFF PLATE FASTENER HOLES # 40L, 90L, AND UPPER HOLES 160L, 180L, 200L, HAS SIGNS OF CORROSION IN COUNTER SINK. REMOVED CORROSION ON AFT CARGO DOOR SCUFF PLATE AREA, FOUND OUT OF LIMITS IAW A220 ASRP J51-21-06, J53-61-01. RESTORE FINISH, PERFOR - [SDR DALA2025100207157](https://openairdocs.org/sdr/DALA2025100207157.md): Scuff Plate · corroded · Sep 27, 2025 · N124DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure > FWD PAX DOOR SCUFF PLATE FASTENER HOLES 50L, 60L, 70L, 80L, 90L, 100L, 110L, AND 120L HAVE EVIDENCE OF CORROSION. REMOVED CORROSION ON FWD PAS DOOR HOLES 50L, 20L, 60L, 70L, 80L, 90L, 100L, 110L, AND 120L FOUND OUT OF LIMITS IAW A220 ASRP J51--21-25. PERFORME - [SDR DALA2025100207155](https://openairdocs.org/sdr/DALA2025100207155.md): Scuff Plate · corroded · Sep 27, 2025 · N124DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure > AFT CARGO DOOR SCUFF PLATE FASTENER LOWER HOLES # 4OL, 9OL AND UPPER HOLES # 16OL, 18OL, 20OL HAS SIGNS OF CORROSION IN COUNTER SINK. REMOVED CORROSION ON AFT CARGO DOOR SCUFF PLATE AREA, FOUND OUT OF LIMITS IAW A220 ASRP J51-21-06, J53-61-01. RESTORE FINISH, - [SDR DALA2025100207154](https://openairdocs.org/sdr/DALA2025100207154.md): Scuff Plate · corroded · Sep 27, 2025 · N124DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure > AFT CARGO DOOR LOWER SCUFF PLATE FASTENER HOLES 20L, 30L, 40L, 50L, 60L, 70L, 80L, 90L, 100L, 110L, HAVE EVIDENCE OF CORROSION. REMOVED CORROSION ON AFT CARGO DOOR LOWER SCUFF PLATE AREA, FOUND OUT OF LIMITS IAW A220 ASRP J51-61-06, J53-21-01. RESTORED FINISH - [SDR DALA2025100207153](https://openairdocs.org/sdr/DALA2025100207153.md): Door Sill · corroded · Sep 27, 2025 · N124DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure > FWD CARGO DOOR LOWER SILL HAS EVIDENCE OF CORROSION. REMOVED CORROSION ON FWD CARGO DOOR LWR SILL, FOUND OUT OF LIMITS IAW ASRP J51-21-06, J53-21-25. RESTORE FINISH, PERFORMED ALL WORK IAW ERA 629095-14. ASSOCIATED ER/A 14-629095 ADDED FOR AC 8124. (LP# 12213 - [SDR DALA2025100207152](https://openairdocs.org/sdr/DALA2025100207152.md): Support Strut · corroded · Sep 27, 2025 · N124DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure > FWD CARGO DOOR, LOWER SILL, FWD AND AFT SUPPORT STRUTS HAVE EVIDENCE OF CORROSION. REMOVED CORROSION ON FWD CARGO DOOR LWR SILL, FOUND OUT OF LIMITS IAW ASRP J51-21--06 & J53-21-25 RESTORED FINISH PREFORMED ALL WORK IAW ERA 629138-14. ASSOCIATED ER/A 14-62913 - [SDR DALA2025100207151](https://openairdocs.org/sdr/DALA2025100207151.md): Scuff Plate · corroded · Sep 27, 2025 · N124DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure > FWD PAX DOOR SCUFF PLATE FASTENER HOLE NR 80L HAS SIGNS OF CORROSION IN COUNTER SINK. REMOVED CORROSION ON FWD PAX DOOR HOLE NR 80L, FOUND OUT OF LIMITS IAW ASRP 51-21--06 & 53-21-25 PREFORMED WORK I& RESTORED FINISH & PRIMED IAW ERA 629281-14. ASSOCIATED - [SDR DALA2025100207150](https://openairdocs.org/sdr/DALA2025100207150.md): Scuff Plate · corroded · Sep 27, 2025 · N124DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure > AFT SERVICE DOOR SCUFF PLATE FASTENER HOLE NR 60L HAS SIGNS OF CORROSION IN COUNTER SINK. REMOVED CORROSION ON AFT SERVICE DOOR SCUFF PLATE FASTENER HOLE NR 60, FOUND OUT OF LIMITS IAW ASRP 51-21--06 & 53-61-01 PREFORMED WORK I& RESTORED FINISH IAW ERA 629154- - [SDR DALA2025100207149](https://openairdocs.org/sdr/DALA2025100207149.md): Scuff Plate · corroded · Sep 27, 2025 · N124DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure > AFT SERVICE DOOR SCUFF PLATE FASTENER HOLES 10L, 20L, 30L, 50L, 60L, 70L, 100L, AND 140L HAVE EVIDENCE OF CORROSION. REMOVED CORROSION ON ON THE SCUFF PLATE FASTENER HOLES 10L, 20L, 30L, 50L, 60L, 70L, 100L, AND 140L. FOUND OUT OF LIMITS IAW ASRP J21--53-61 - [SDR DALA2025100207164](https://openairdocs.org/sdr/DALA2025100207164.md): Scuff Plate · corroded · Sep 27, 2025 · N124DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure > AFT PAX DOOR SCUFF PLATE FASTENER HOLE NR 110L HAS SIGNS OF CORROSION IN COUNTER SINK. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW ASRP 51-21-06 & 53-61-01. PERFORMED WORK AND RESTORED FINISH IAW ERA 629725-14. ASSOCIATED ER/A 14-629725 ADDED FOR AC 8124. ( - [SDR DALA2025093007109](https://openairdocs.org/sdr/DALA2025093007109.md): Scuff Plate · corroded · Sep 27, 2025 · N124DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure > FWD CARGO DOOR, LOWER SCUFF PLATE FASTENENER HOLES 21OL, 20OL, AND 13OL HAVE EVIDENCE OF CORROSION. REMOVED CORROSION ON FWD CARGO LOWER SCUFF PLATE AREA, FOUND TO BE OUT OF LIMITS IAW A220 ASRP 51-21-06 & 53-61-01. PERFORMED ALL WORK & RESTORED FINISH IAW E - [SDR DALA2025093007108](https://openairdocs.org/sdr/DALA2025093007108.md): Scuff Plate · corroded · Sep 27, 2025 · N124DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure > AFT PAX DOOR SCUFF PLATE FASTENER HOLES 6OL, 10OL, AND 11OL HAVE EVIDENCE OF CORROSION. REMOVED CORROSION ON AFT PAX DOOR SCUFF PLATE HOLES 6OL, 10OL, & 11OL, FOUND OUT OF LIMITS IAW A220 ASRP 51-21-06, 53-61-01. PERFORMED WORK AND RESTORED FINISH IAW A220 E - [SDR DALA2025093007107](https://openairdocs.org/sdr/DALA2025093007107.md): Scuff Plate · corroded · Sep 25, 2025 · N124DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure > SCUFF PLATE FASTENER HOLE ON FWD SERVICE DOOR, 14OL, 12OL, 11OL, 10OL, 9OL, 7OL, 6OL, 5OL, AND 4OL, HAVE EVIDENCE OF CORROSION. REMOVED CORROSION ON FWD SERVICE DOOR SCUFF PLATE AREA, FOUND OUT OF LIMITS IAW A220 ASRP J51-21-06, J53-21-05. RESTORE FINISH AND - [SDR DALA2025093007106](https://openairdocs.org/sdr/DALA2025093007106.md): Scuff Plate · corroded · Sep 24, 2025 · N124DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure > AFT CARGO DOOR, UPPER SCUFF PLATE FASTENER HOLES 16OU, 17OU, 18OU, 19OU, 20OU, AND 24OU HAVE EVIDENCE OF CORROSION. REMOVED CORROSION ON AFT CARGO DOOR UPPER SCUFF PLATE AREA, FOUND OUT OF LIMITS IAW A220 ASRP J51-21-06 AND J53-61-01. RESTORE FINISH AND PERF - [SDR DALA2025090206502](https://openairdocs.org/sdr/DALA2025090206502.md): Seat Track · corroded · Aug 30, 2025 · N124DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings > AFT CABIN, LT OTBD SEAT TRACK, AFT MOST TRACK, HAS EVIDENCE OF CORROSION. REMOVED CORROSION ON AFT CABIN SEAT TRACK, FOUND OUT OF LIMITS IAW ASRP J51-21-06, J53-61-49. REMOVED AND REPLACED LT OTBD SEAT TRACK IAW ASRP J51-42-20. (LP# 1172888) - [SDR DALA2025090206501](https://openairdocs.org/sdr/DALA2025090206501.md): Seat Track · corroded · Aug 30, 2025 · N124DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings > AFT CABIN, RT INBD SEAT TRACK, AFT MOST TRACK, HAS EVIDENCE OF CORROSION. REMOVED CORROSION ON SEAT TRACK, FOUND OUT OF LIMITS IAW ASRP J51-21-06, J53-51-49. REMOVED AND REPLACED RT INBD SEAT TRACK IAW ASRP J51-42-20. (LP# 1172881) - [SDR DALA2025090206494](https://openairdocs.org/sdr/DALA2025090206494.md): Seat Track · corroded · Aug 27, 2025 · N124DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings > AFT CABIN, LH I/B SEAT TRACK, AFT MOST TRACK, HAS EVIDENCE OF CORROSION. REMOVED CORROSION ON AFT CABIN L/H I/B SEAT TRACK, AREA FOUND OUT OF LIMITS IAW A220 ASRP J51-21-06, J53-61-49. REMOVED AND REPLACED L/H I/B SEAT TRACK IAW A220 ASRP J51-42-20. (LP# 11670 - [SDR DALA2025090206493](https://openairdocs.org/sdr/DALA2025090206493.md): Seat Track · corroded · Aug 27, 2025 · N124DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings > AFT CABIN, RH O/B SEAT TRACK, AFT MOST TRACK, HAS EVIDENCE OF CORROSION. CORRODED AREA OF AFT CABIN R/H O/B SEAT TRACK FOUND OUT OF LIMITS IAW A220 ASRP J53-61-49. REMOVED AND REPLACED R/H O/B SEAT TRACK IAW A220 ASRP J51-42-20. (LP# 1167044) - [SDR DALA2025090206492](https://openairdocs.org/sdr/DALA2025090206492.md): Seat Track · corroded · Aug 27, 2025 · N124DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings > FWD CABIN, RH O/B SEAT TRACK, FWD MOST TRACK, HAS EVIDENCE OF CORROSION. AFFECTED AREA ON FWD CABIN R/H O/B SEAT TRACK FOUND OUT OF LIMITS IAW A220 ASRP J53-21-49. REMOVED AND REPLACED R/H O/B SEAT TRACK IAW A220 ASRP J51-42-20. (LP# 1167038) - [SDR DALA2025090206489](https://openairdocs.org/sdr/DALA2025090206489.md): Seat Track · corroded · Aug 26, 2025 · N124DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings > FWD CABIN, RH I/B SEAT TRACK, FWD MOST TRACK, HAS EVIDENCE OF CORROSION. REMOVED CORROSION FOUND WITHOUT LIMITS. REMOVED AND REPLACED SEAT TRACK FWD R/H I/B FR20 TO 30 I.A.W. A220 ASRP J53-21-49 ASRP J51-40-11 JS1,42,20 AND JS1-21-06. (L/P# 1165377) - [SDR DALA2025021001043](https://openairdocs.org/sdr/DALA2025021001043.md): Slat Track · worn · Feb 7, 2025 · N124DU · Airbus BD5001A10 · Leading Edge Devices > UPON INSPECTION OF RACK AND PINION ON LH NBR 10 TRACK FOUND UNIDENTIFIED WEAR. COMPLIED WITH ER/A 624192-14AD REV. ORIGINAL SECTION IV: TIME LIMITED REPAIR I AND PRI 624192-14AD REV. 0 ASSOCIATED ER/A 14-624192 ADDED FOR AC 8124. (LP# 0800727) - [SDR DALA2025021001042](https://openairdocs.org/sdr/DALA2025021001042.md): Slat Track · damaged · Feb 7, 2025 · N124DU · Airbus BD5001A10 · Leading Edge Devices > RH SLAT TRACK NBR 4 UPPER AFT SURFACE REQUIRES NDT INSPECTION PER AMDS W/C 5742-01028-02B. ACCOMPLISHED EDDY CURRENT INSPECTION OF RH #4 SLAT TRACK BLENDED AFT UPPER SURFACE REF ANDTP 51-01-20-01AAA-353A-A. NO CRACK INDICATIONS NOTED AT THIS TIME QC5364. (LP# - [SDR DALA2024112111128](https://openairdocs.org/sdr/DALA2024112111128.md): Control Unit · faulted · Nov 20, 2024 · N124DU · Airbus BD5001A10 · Landing Gear Brake System > SHIP 8124 - DIV - DIVERTED TO JFK AND DECLARED EMERGENCY DUE TO AUTO BRAKE FAIL AND NORM BRAKE FAIL MESSAGES. FLIGHT LANDED SAFELY AND TAXIED TO THE GATE. CORRECTIVE ACTION: REPLACED #1 AND #2 BDCU. (LP# 6670478) - [SDR DALA2023122710650](https://openairdocs.org/sdr/DALA2023122710650.md): Unknown · unknown · Dec 23, 2023 · N124DU · Bombdr BD1001A10 · Leading Edge Devices > R/H SLAT TRACK NBR 10 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED R/H SLAT TRACK NBR 10 UPP - [SDR DALA2023122710649](https://openairdocs.org/sdr/DALA2023122710649.md): Unknown · unknown · Dec 23, 2023 · N124DU · Bombdr BD1001A10 · Leading Edge Devices > R/H SLAT TRACK NBR 8 UPPER SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED R/H SLAT TRACK NBR 8 UPPER FWD - [SDR DALA2023122710648](https://openairdocs.org/sdr/DALA2023122710648.md): Unknown · unknown · Dec 23, 2023 · N124DU · Bombdr BD1001A10 · Leading Edge Devices > R/H SLAT TRACK NBR 7 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED R/H SLAT TRACK NBR 7 UPPER - [SDR DALA2023122710647](https://openairdocs.org/sdr/DALA2023122710647.md): Unknown · unknown · Dec 23, 2023 · N124DU · Bombdr BD1001A10 · Leading Edge Devices > R/H SLAT TRACK NBR 6 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED R/H SLAT TRACK NBR 6 UPPER - [SDR DALA2023122710646](https://openairdocs.org/sdr/DALA2023122710646.md): Unknown · unknown · Dec 23, 2023 · N124DU · Bombdr BD1001A10 · Leading Edge Devices > R/H SLAT TRACK NBR 5 UPPER AFT AND LOWER AFT SURFACES HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED R/H SLAT T - [SDR DALA2023122710645](https://openairdocs.org/sdr/DALA2023122710645.md): Unknown · unknown · Dec 23, 2023 · N124DU · Bombdr BD1001A10 · Leading Edge Devices > R/H SLAT TRACK NBR 4 UPPER AFT AND LOWER AFT SURFACES HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED R/H SLAT T - [SDR DALA2023122710644](https://openairdocs.org/sdr/DALA2023122710644.md): Unknown · unknown · Dec 23, 2023 · N124DU · Bombdr BD1001A10 · Leading Edge Devices > R/H SLAT TRACK NBR 4 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED R/H SLAT TRACK NBR 4 UPPER - [SDR DALA2023122710643](https://openairdocs.org/sdr/DALA2023122710643.md): Unknown · unknown · Dec 23, 2023 · N124DU · Bombdr BD1001A10 · Leading Edge Devices > R/H SLAT TRACK NBR 2 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED R/H SLAT TRACK NBR 2 UPPER - [SDR DALA2023122710642](https://openairdocs.org/sdr/DALA2023122710642.md): Unknown · unknown · Dec 23, 2023 · N124DU · Bombdr BD1001A10 · Leading Edge Devices > R/H SLAT TRACK NBR 2 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED R/H SLAT TRACK NBR 2 UPPER - [SDR DALA2023122710641](https://openairdocs.org/sdr/DALA2023122710641.md): Unknown · unknown · Dec 23, 2023 · N124DU · Bombdr BD1001A10 · Leading Edge Devices > R/H SLAT TRACK NBR 1 UPPER FWD AND AFT SURFACES HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED R/H SLAT TRACK N - [SDR DALA2023122710640](https://openairdocs.org/sdr/DALA2023122710640.md): Unknown · unknown · Dec 23, 2023 · N124DU · Bombdr BD1001A10 · Leading Edge Devices > L/H SLAT TRACK NBR 3 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 3 UPPER - [SDR DALA2023122710639](https://openairdocs.org/sdr/DALA2023122710639.md): Unknown · unknown · Dec 23, 2023 · N124DU · Bombdr BD1001A10 · Leading Edge Devices > L/H SLAT TRACK NBR 11 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 11 UPPE - [SDR DALA2023122710638](https://openairdocs.org/sdr/DALA2023122710638.md): Unknown · unknown · Dec 23, 2023 · N124DU · Bombdr BD1001A10 · Leading Edge Devices > L/H SLAT TRACK NBR 10 UPPER AND LOWER AFT SURFACES HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED LH SLAT TRACK - [SDR DALA2023122710637](https://openairdocs.org/sdr/DALA2023122710637.md): Unknown · unknown · Dec 23, 2023 · N124DU · Bombdr BD1001A10 · Leading Edge Devices > L/H SLAT TRACK NBR 8 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 8 UPPER - [SDR DALA2023122710636](https://openairdocs.org/sdr/DALA2023122710636.md): Unknown · unknown · Dec 23, 2023 · N124DU · Bombdr BD1001A10 · Leading Edge Devices > L/H SLAT TRACK NBR 7 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 7 UPPER - [SDR DALA2023122710635](https://openairdocs.org/sdr/DALA2023122710635.md): Unknown · unknown · Dec 23, 2023 · N124DU · Bombdr BD1001A10 · Leading Edge Devices > L/H SLAT TRACK NBR 6 UPPER AFT SURFACES HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED LH SLAT TRACK NBR 6 UPPER - [SDR DALA2023122710634](https://openairdocs.org/sdr/DALA2023122710634.md): Unknown · unknown · Dec 23, 2023 · N124DU · Bombdr BD1001A10 · Leading Edge Devices > L/H SLAT TRACK NBR 5 UPPER AND LOWER AFT SURFACES HAVE EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED LH SLAT TRACK Next page: https://openairdocs.org/aircraft/N124DU/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 = 'N124DU' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N124DU/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.