N124DU

Service difficulty reports · 87

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR DALA2026091005072Skin · dentedER/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), WHICAug 28, 2026 · N124DU · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2026051302997Light · inoperativeEXTERIOR 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)May 11, 2026 · N124DU · Airbus BD5001A10 · Emergency LightingSDR DALA2026051302996Light · faultedEXTERIOR 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)May 11, 2026 · N124DU · Airbus BD5001A10 · Emergency LightingSDR DALA2026030401498Oil System · overservicedDIRTY 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 ENGINMar 1, 2026 · N124DU · Airbus BD5001A10 · Turbine Engine Oil SystemSDR DALA2026030401500Filter · odorDIRTY 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, NFeb 27, 2026 · N124DU · Airbus BD5001A10 · Air Distribution SystemSDR DALA2025122309353Unknown · odorSMKE - 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. REPLACEDDec 19, 2025 · N124DU · Airbus BD5001A10 · Air Distribution SystemSDR DALA2025111208280Strut · dischargedDECLARED 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)Nov 8, 2025 · N124DU · Airbus BD5001A10 · Main Landing Gear Strut/Axle/TruckSDR DALA2025102107686Light · faultedFAS 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)Oct 16, 2025 · N124DU · Airbus BD5001A10 · Emergency LightingSDR DALA2025101307464Landing Gear · faultedATB - RETURNED TO MLB DUE TO LEFT MLG GEAR INDICATION. R & R LEFT MLG ASSEMBLY PER AMDS 3210-4001-LH. (LP# 6995824)Oct 6, 2025 · N124DU · Airbus BD5001A10 · Landing Gear Position and WarningSDR DALA2025100607255Door Sill · corrodedAFT 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. ORISep 29, 2025 · N124DU · Airbus BD5001A10 · Fuselage Main, StructureSDR DALA2025100207156Scuff Plate · corrodedAFT 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, PERFORSep 28, 2025 · N124DU · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2025100207157Scuff Plate · corrodedFWD 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. PERFORMESep 27, 2025 · N124DU · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2025100207155Scuff Plate · corrodedAFT 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, Sep 27, 2025 · N124DU · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2025100207154Scuff Plate · corrodedAFT 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 Sep 27, 2025 · N124DU · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2025100207153Door Sill · corrodedFWD 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# 12213Sep 27, 2025 · N124DU · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2025100207152Support Strut · corrodedFWD 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 14-62913Sep 27, 2025 · N124DU · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2025100207151Scuff Plate · corrodedFWD 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 Sep 27, 2025 · N124DU · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2025100207150Scuff Plate · corrodedAFT 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-Sep 27, 2025 · N124DU · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2025100207149Scuff Plate · corrodedAFT 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--53-61Sep 27, 2025 · N124DU · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2025100207164Scuff Plate · corrodedAFT 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. (Sep 27, 2025 · N124DU · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2025093007109Scuff Plate · corrodedFWD 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 ESep 27, 2025 · N124DU · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2025093007108Scuff Plate · corrodedAFT 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 ESep 27, 2025 · N124DU · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2025093007107Scuff Plate · corrodedSCUFF 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 ANDSep 25, 2025 · N124DU · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2025093007106Scuff Plate · corrodedAFT 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 PERFSep 24, 2025 · N124DU · Airbus BD5001A10 · Fuselage Miscellaneous StructureSDR DALA2025090206502Seat Track · corrodedAFT 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)Aug 30, 2025 · N124DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025090206501Seat Track · corrodedAFT 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)Aug 30, 2025 · N124DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025090206494Seat Track · corrodedAFT 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# 11670Aug 27, 2025 · N124DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025090206493Seat Track · corrodedAFT 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)Aug 27, 2025 · N124DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025090206492Seat Track · corrodedFWD 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)Aug 27, 2025 · N124DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025090206489Seat Track · corrodedFWD 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)Aug 26, 2025 · N124DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025021001043Slat Track · wornUPON 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)Feb 7, 2025 · N124DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2025021001042Slat Track · damagedRH 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# Feb 7, 2025 · N124DU · Airbus BD5001A10 · Leading Edge DevicesSDR DALA2024112111128Control Unit · faultedSHIP 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)Nov 20, 2024 · N124DU · Airbus BD5001A10 · Landing Gear Brake SystemSDR DALA2023122710650Unknown · unknownR/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 UPPDec 23, 2023 · N124DU · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2023122710649Unknown · unknownR/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 FWDDec 23, 2023 · N124DU · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2023122710648Unknown · unknownR/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 UPPERDec 23, 2023 · N124DU · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2023122710647Unknown · unknownR/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 UPPERDec 23, 2023 · N124DU · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2023122710646Unknown · unknownR/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 TDec 23, 2023 · N124DU · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2023122710645Unknown · unknownR/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 TDec 23, 2023 · N124DU · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2023122710644Unknown · unknownR/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 UPPERDec 23, 2023 · N124DU · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2023122710643Unknown · unknownR/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 UPPERDec 23, 2023 · N124DU · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2023122710642Unknown · unknownR/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 UPPERDec 23, 2023 · N124DU · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2023122710641Unknown · unknownR/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 NDec 23, 2023 · N124DU · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2023122710640Unknown · unknownL/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 Dec 23, 2023 · N124DU · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2023122710639Unknown · unknownL/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 UPPEDec 23, 2023 · N124DU · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2023122710638Unknown · unknownL/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 TRACKDec 23, 2023 · N124DU · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2023122710637Unknown · unknownL/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 Dec 23, 2023 · N124DU · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2023122710636Unknown · unknownL/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 Dec 23, 2023 · N124DU · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2023122710635Unknown · unknownL/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 UPPERDec 23, 2023 · N124DU · Bombdr BD1001A10 · Leading Edge DevicesSDR DALA2023122710634Unknown · unknownL/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 Dec 23, 2023 · N124DU · Bombdr BD1001A10 · Leading Edge Devices
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