# Service difficulty reports: N125DU

A list on [N125DU](https://openairdocs.org/aircraft/N125DU.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 · 68 reports

- [SDR DALA2026091105093](https://openairdocs.org/sdr/DALA2026091105093.md): Engine · odor · Sep 9, 2026 · N125DU · Airbus BD5001A10 · Engine (Turbine/Turboprop)
  > DECLARED EMERGENCY DUE TO WAXY / ACIDIC SMELL IN FLIGHT DECK AND CABIN. SMELL DISSIPATED ONE PACKS WERE ISOLATED. #02 ENGINE REPLACED. (LP# 9170256, 1804448, 9170250; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026091005074](https://openairdocs.org/sdr/DALA2026091005074.md): Unknown · odor · Sep 8, 2026 · N125DU · Airbus BD5001A10 · Air Distribution System
  > DECLARED EMERGENCY AND DIVERTED TO RDU DUE TO ODOR IN THE MID CABIN. CARRIED OUT W/C 0550- 2001. REF A220 RD500-A-J79-00-00-00AAA-310A-A AND A-J49-91-00- 01AAA-311A-A. CARRIED WITH W/C 0550-2001 & 0550-6001. NO ODOR DETECTED. R/R RECIRCULATION FILTERS PER A2
- [SDR DALA2026061703627](https://openairdocs.org/sdr/DALA2026061703627.md): Slide · unraveled · Jun 13, 2026 · N125DU · Airbus BD5001A10 · Escape Slide
  > GIRT BAR STATUS INDICATOR DOES NOT SHOW FULL RED WHEN 1L DOOR IS ARMED. FOUND L1 DOOR EMERGENCY SLIDE PACKING BEGINNING TO UNRAVEL. R/R L1 ESCAPE SLIDE ASSEMBLY P/N: 68331-101 IAW AMDS CARD # 2563-4001. C/W RII PORTIONS OF L1 DOOR SLIDE CHANGE IAW AMDS 2563- 4
- [SDR DALA2025102107688](https://openairdocs.org/sdr/DALA2025102107688.md): Door Sill · no discrepancy · Oct 15, 2025 · N125DU · Airbus BD5001A10 · Standard Practices/Structures
  > ERA 622251-14 REV A HAS FOLLOW-ON INSPECTION FOR THE FORWARD CARGO DOOR SILL AREA. ACCOMPLISH SECTION II WITHIN 28,600 FC OR 50,050 FH. THEN EVERY 9,400 FC OR 16,450 FH THEREAFTER. ASSOCIATED ER/A 00-622251 ADDED FOR AC 8125. (LP# 1253477)
- [SDR DALA2026031301753](https://openairdocs.org/sdr/DALA2026031301753.md): Blade · corroded · Aug 29, 2025 · N125DU · Airbus BD5001A10 · Engine Thrust Reverser
  > ENGINE, INBD THRUST REVERSER, LOWER V BLADE SEGMENT HAS MULTIPLE SPOTS OF CORROSION. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0659:7830-2007-RH/003 00648. REMOVED AND INSTALLED #2 ENG I/B T/R REF. AMDS WORKCARD 7830-4003-02-LH. (LP# 1170203)
- [SDR DALA2026031301752](https://openairdocs.org/sdr/DALA2026031301752.md): Blade · corroded · Aug 29, 2025 · N125DU · Airbus BD5001A10 · Engine Thrust Reverser
  > NR 1 ENGINE, OTBD THRUST REVERSER, LOWER V BLADE SEGMENT HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND INSTALLED #2 ENG O/B T/R REF. AMDS WORKCARD 7830-4003-01-LH. PART REPLACED MATERIAL DIMENSIONS NOT REQUIRED. (LP# 1170211)
- [SDR DALA2025090206500](https://openairdocs.org/sdr/DALA2025090206500.md): Structure · damaged · Aug 29, 2025 · N125DU · Airbus BD5001A10 · Cargo/Baggage Doors
  > FWD CARGO DOOR, FWD LOWER CORNER DAMAGE. COMPLIED WITH ER/A 627697-14 PRI REV 0, ER/A 627697-14 PRI REV 1, ER/A 627697-14 PRI REV 2, ER/A 627697-14 PRI REV 3, ER/A 627697-14 PRI REV 4, ER/A 627697-14 PRI REV 5, AND FINAL ER/A 627697-14 REV A SECTION 1.
- [SDR DALA2025090206499](https://openairdocs.org/sdr/DALA2025090206499.md): Floor Support · corroded · Aug 29, 2025 · N125DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON FLOOR SUPPORT BEAM GALLEY MOUNT NUT PLATE HOLE AT LBL40 BETWEEN FR76 AND FR78. REPAIRED BEAM PER ERA 628436-14 REV 0, 1, 2 AND PER ERA 628436- 14 REV. B.
- [SDR DALA2025090206498](https://openairdocs.org/sdr/DALA2025090206498.md): Waste Box · corroded · Aug 29, 2025 · N125DU · Airbus BD5001A10 · Fuselage Main, Structure
  > AFT LOWER FUSELAGE LAV WASTE BOX HAS CORROSION ON AFT RECESSED DOOR FLANGE. COMPLIED WITH PRI 602523-14 REV 0 AND ER/A 602523-02523-14 REV 0 AND ER/A 602523-14 REV A SECTION IV.
- [SDR DALA2025090206491](https://openairdocs.org/sdr/DALA2025090206491.md): Floor Support · corroded · Aug 26, 2025 · N125DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON FLOOR SUPPORT BEAM GALLEY MOUNT NUT PLATE HOLE AT LBL40 BETWEEN FR76 AND FR78. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0193:2060-1007/006 00670 REPAIRED BEAM PER ERA 628436-14 PRI REV 0,1 AND
- [SDR DALA2025090206490](https://openairdocs.org/sdr/DALA2025090206490.md): Fitting · corroded · Aug 26, 2025 · N125DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON FLOOR FITTING AFTER REMOVAL OF FLOOR ANGLE AT FR74 O/B OF LBL 43.5. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0193:2060-1007/008 00672 CORROSION LEVEL 2, LOGBOOK ENTRY REQUIRED. CORROSION CONTA
- [SDR DALA2026031301754](https://openairdocs.org/sdr/DALA2026031301754.md): Blade · corroded · Aug 15, 2025 · N125DU · Airbus BD5001A10 · Engine Thrust Reverser
  > ENGINE, INBD THRUST REVERSER, LOWER V BLADE SEGMENT HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED NO.1 ENGINE I/B T/R LOWER V BLADE SEGMENT PER GRAPW1500BA-A-78-30-00. (LP# 1145500)
- [SDR DALA2025081105979](https://openairdocs.org/sdr/DALA2025081105979.md): Floor Support · corroded · Aug 10, 2025 · N125DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > R/H FLOOR SILL STRINGER 22 JUST AFT OF R2 DOOR SILL CORRODED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0193:2060-1007/003 00667 REMOVED AND REPLACED FLOOR SILL STRINGER REF A220 ASRP 51 -41-02 AND A220 ASRP 51-23-00. (LP# 1135120)
- [SDR DALA2025081105978](https://openairdocs.org/sdr/DALA2025081105978.md): Floor Support · corroded · Aug 9, 2025 · N125DU · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > L/H FLOOR SILL STRINGER 22 JUST AFT OF L2 DOOR SILL CORRODED ON FASTENER HOLE. BLENDED AND CHECKED LIMITS REF A220 ASRP 53-00-00-00AAA-661A-A. REMOVED.005" OF MATERIAL. NOMINAL THICKNESS IS.080" AND WITHIN LIMITS, REF A220 ASRP 53-00-00-00AAA-661A-A. (LP# 11
- [SDR DALA2026031101706](https://openairdocs.org/sdr/DALA2026031101706.md): Seat Track · corroded · Aug 5, 2025 · N125DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AFT FUSELAGE SEAT TRACK CORROSION RBL 43.5 AT FRAMES 62, 67, AND 74. SSI: 53-61-43-01. NO EVIDENCE OF PREVIOUS RE-WORK OR REPAIR NOTED. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0584:5300-2015/001 00301 REPLACED SEAT TRACK AT FR 62-62 PER AIRBUS DRAWING C0
- [SDR DALA2025080705929](https://openairdocs.org/sdr/DALA2025080705929.md): Seat Track · corroded · Aug 5, 2025 · N125DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AFT FUSELAGE SEAT TRACK CORROSION LBL 43.5 AT FRAMES 71-74. SSI: 53-61-43-01. NO EVIDENCE OF PREVIOUS RE-WORK OR REPAIR NOTED. REPLACED SEAT TRACK REF A220 ER/A 623167-14TR. REF NR: 304. SHOULD STATE ERA 623167-14TR REV ORIG.
- [SDR DALA2025080705925](https://openairdocs.org/sdr/DALA2025080705925.md): Seat Track · corroded · Aug 1, 2025 · N125DU · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AFT GALLEY CENTER F/A SEAT MOUNTING FLANGE CORRODED. REMOVED AND REPLACED FLOOR FITTINGS WITH REF CMM 25-30-18.
- [SDR DALA2025052704044](https://openairdocs.org/sdr/DALA2025052704044.md): Sign · burned out · May 24, 2025 · N125DU · Airbus BD5001A10 · Emergency Lighting
  > FOUND RT OVER WING EMERGENCY SIGN IN CABIN BURNT OUT. R/R EMERGENCY LIGHT LIGHT PER THE A220 AMP 33-54. OPS CHK GOOD. (LP#7054031)
- [SDR DALA2025021901227](https://openairdocs.org/sdr/DALA2025021901227.md): Engine · odor · Feb 15, 2025 · N125DU · Airbus BD5001A10 · Engine (Turbine/Turboprop)
  > FUMES DETECTED IN THE COCKPIT ON ARRIVAL PHASE AROUND 6,000 FEET. T/S PER A220 AMDS WORKCARD 0550-2001 FOUND LT ENGINE OVER SERVICED WITH OIL (27.4 QTS) ISOLATED ODOR TO LEFT ENGINE DURING IDLE RUN. SERVICED OIL SYSTEM TO PROPER LEVELS PER A220 AMP BD500-A-J79
- [SDR DALA2025012300567](https://openairdocs.org/sdr/DALA2025012300567.md): Unknown · odor · Jan 19, 2025 · N125DU · Airbus BD5001A10 · Air Distribution System
  > POTENTIAL ODOR EVENT. LITE "DIRTY SOCK" SMELL ON T/O TO ABOUT 10,000 FT. NOTHING VISIBLE ON THE FLIGHT DESK. MASK NOT DEPLOYED. ATTEMPTED TO ISOLATE SMELL PER W/C 0550-2002. RAN ENGINES AT HIGH POWER & APU UNDER DIFFERENT SETTINGS. NO UNUSUAL ODORS NOTED. PERF
- [SDR DALA2025010600113](https://openairdocs.org/sdr/DALA2025010600113.md): Unknown · unknown · Jan 2, 2025 · N125DU · Airbus BD5001A10 · Standard Practices/Structures
  > DTE, ER/A 612109-14AD REV B REQUIRES STAGE 3 DTA APPROVAL. A220-100 / FUSELAGE / REAR BARREL / FR70 TO FR72 AND STR23L TO STR25L / DENT. ER/A 612109-14AD REV B REQUIRES STAGE 3 DTA APPROVAL ON OR BEFORE 30,000 FLIGHT CYCLES FROM SECTION III REPAIR EMBODIMENT O
- [SDR DALA2024100809786](https://openairdocs.org/sdr/DALA2024100809786.md): Slat Track · corroded · Oct 4, 2024 · N125DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK #4 PINION TEETH (2EA) HAS EVIDENCE OF CORROSION. REF 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. COMPLIED WITH PRI #621381-14 REV 0, NO CRACKS FOUND (854489) AND ER/A 621381-14 REV ORIGINAL MATCHES. (LP# 059
- [SDR DALA2024100809785](https://openairdocs.org/sdr/DALA2024100809785.md): Slat Track · corroded · Oct 4, 2024 · N125DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK #4 RACK TEETH (2EA) HAS EVIDENCE OF CORROSION. REF 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. COMPLIED WITH PRI #621381-14 REV 0, NO CRACKS FOUND (854489) AND ER/A 621381-14 REV ORIGINAL MATCHES. (LP# 05925
- [SDR DALA2024100809784](https://openairdocs.org/sdr/DALA2024100809784.md): Slat Track · no discrepancy · Oct 4, 2024 · N125DU · Airbus BD5001A10 · Standard Practices/Structures
  > RH WING #5 SLAT TRACK LOWER AFT SURFACE REQUIRES NDT INSP. PER AMDS W/C 5742-01028-02B. ACCOMPLISHED EDDY CURRENT INSPECTION PER A220 ANDTP 51-01-353. NO CRACKS FOUND. (LP# 0592280)
- [SDR DALA2024100809783](https://openairdocs.org/sdr/DALA2024100809783.md): Slat Track · no discrepancy · Oct 4, 2024 · N125DU · Airbus BD5001A10 · Standard Practices/Structures
  > RH WING #4 SLAT TRACK UPPER FWD SURFACE REQUIRES NDT INSP. PER AMDS W/C 5742-01028-02B. ACCOMPLISHED EDDY CURRENT INSPECTION PER A220 ANDTP 51-01-353. NO CRACKS FOUND. (LP# 0592273)
- [SDR DALA2024100809782](https://openairdocs.org/sdr/DALA2024100809782.md): Slat Track · no discrepancy · Oct 4, 2024 · N125DU · Airbus BD5001A10 · Leading Edge Devices
  > RH WING #3 SLAT TRACK UPPER FWD SURFACE REQUIRES NDT INSP. PER AMDS W/C 5742-01028-02B. ACCOMPLISHED EDDY CURRENT INSP. IAW A220 ANDTP 51-01-353. NO CRACKS FOUND. (LP# 0592263)
- [SDR DALA2024100809781](https://openairdocs.org/sdr/DALA2024100809781.md): Slat Track · no discrepancy · Oct 4, 2024 · N125DU · Airbus BD5001A10 · Standard Practices/Structures
  > RH WING #2 SLAT TRACK UPPER FWD SURFACE REQUIRES NDT INSP. PER AMDS W/C 5742-01028-02A. ACCOMPLISHED EDDY CURRENT INSP. PER A220 ANDTP 1-01-353. NO CRACKS FOUND. (LP# 0592252)
- [SDR DALA2024100809780](https://openairdocs.org/sdr/DALA2024100809780.md): Slat Track · no discrepancy · Oct 4, 2024 · N125DU · Airbus BD5001A10 · Standard Practices/Structures
  > LH WING #1 SLAT TRACK LOWER AFT SURFACE REQUIRES NDT INSP. PER AMDS W/C 5742-01028-02A. ACCOMPLISHED EDDY CURRENT INSP. PER A220 ANDTP 1-01-353. (LP# 0592245)
- [SDR DALA2024081408143](https://openairdocs.org/sdr/DALA2024081408143.md): Control Lever · faulted · Aug 10, 2024 · N125DU · Airbus BD5001A10 · Landing Gear Selector
  > ON SELECTION OF GEAR DOWN, HEARD A LOUD "CLUNK" NOISE, FOLLOWED BY "GEAR FAIL" CTN MSG. RAN QRH, VERIFIED GEAR DOWN & LOCKED, PROCEEDED TO AN UNEVENTFUL LANDING. T/S PER A220 EFIM SOULUTION ID # 1-14918. R/R LANDING GEAR CONTROL LEVER PER A220 AMM 32-31. OPS T
- [SDR DALA2024052105389](https://openairdocs.org/sdr/DALA2024052105389.md): Unknown · fumes · May 16, 2024 · N125DU · Airbus BD5001A10 · Air Distribution System
  > 'DIRTY SOCK' ODOR/FUMES ON BOTH FLIGHTS. PERFORMED HIGH POWER ENGINE RUN AFTER BOROSCOPES. NO FUMES NOTED. SNIFFER TEST RESULT 0.0 REF CARD 0550-2001 (703365). PERF ECS DECONTAMINATION POST SMOKE/FUME EVENT WORKCARD UP TO STEP 27. NDS FINAL TEST FOR ODOR(3521
- [SDR DALA2024032703852](https://openairdocs.org/sdr/DALA2024032703852.md): Warning Message · illuminated · Mar 19, 2024 · N125DU · Airbus BD5001A10 · Escape Slide
  > WING SLIDE CAUTION MESSAGE DURING PUSHBACK. PLACARDED AND DEFERRED OVERWING SLIDE CONDITION IND INOP. OPERATE AS PER MEL 25-63-02; R&R LT OVERWING SLIDE PER WORKCARD 2563-4002. NO WING SLIDE CAUTION MESSAGE PRESENT. MEL & PLACARDS REMOVED. NO "M" PROCEDURES.
- [SDR DALA2024031803420](https://openairdocs.org/sdr/DALA2024031803420.md): Slat Track · corroded · Mar 15, 2024 · N125DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 7 LOWER FWD IB SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 7 LOWER FWD IB SIDE IAW ER/A 606942- 14AD REV B AND PRI 606942-14AD REV 0 MATCHED. (LP# 0245354)
- [SDR DALA2024031803419](https://openairdocs.org/sdr/DALA2024031803419.md): Slat Track · corroded · Mar 15, 2024 · N125DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 3 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. L REPAIRED LH SLAT TRACK NBR 3 UPPER AFT SURFACE IAW ER/A 606942- 14AD REV B AND PRI 606942-14AD REV 0 MATCHED. (LP# 0245353)
- [SDR DALA2024031803418](https://openairdocs.org/sdr/DALA2024031803418.md): Slat Track · corroded · Mar 15, 2024 · N125DU · Airbus BD5001A10 · 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 606942-14AD REV B AND PRI 606942-14AD REV 0 MATCHED. (LP# 0245352)
- [SDR DALA2024031803417](https://openairdocs.org/sdr/DALA2024031803417.md): Slat Track · corroded · Mar 15, 2024 · N125DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 11 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 11 UPPER AFT SURFACE IAW ER/A 606942-14AD REV B AND PRI 606942-14AD REV 0 MATCHED. (LP# 0245336)
- [SDR DALA2024031803416](https://openairdocs.org/sdr/DALA2024031803416.md): Slat Track · corroded · Mar 15, 2024 · N125DU · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 6 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02A. REPAIRED LH SLAT TRACK NBR 6 UPPER FWD SURFACE IAW ER/A 606942- 14AD REV B AND PRI 606942-14AD REV 0 MATCHED. (LP# 0245326)
- [SDR DALA2024031803415](https://openairdocs.org/sdr/DALA2024031803415.md): Slat Track · corroded · Mar 15, 2024 · N125DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 1 LOWER FWD IB SIDE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 1 LOWER FWD IB SIDE IAW ER/A 606941-14AD REV D AND PRI 606941-14AD REV 0 MATCHED. (LP# 0245307)
- [SDR DALA2024031803414](https://openairdocs.org/sdr/DALA2024031803414.md): Slat Track · corroded · Mar 15, 2024 · N125DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 4 UPPER AFT SURFACE IAW ER/A 606941-14AD REV D AND PRI 606941-14AD REV 0 MATCHED. (LP# 0245302)
- [SDR DALA2024031803413](https://openairdocs.org/sdr/DALA2024031803413.md): Slat Track · corroded · Mar 15, 2024 · N125DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 6 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 6 UPPER AFT SURFACE IAW ER/A 606941-14AD REV D AND PRI 606941-14AD REV 0 MATCHED. (LP# 0245299)
- [SDR DALA2024031803412](https://openairdocs.org/sdr/DALA2024031803412.md): Slat Track · corroded · Mar 15, 2024 · N125DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 4 LOWER AFT SURFACE IAW ER/A 606941-14AD REV D AND PRI 606941-14AD REV 0 MATCHED. (LP# 0245295)
- [SDR DALA2024031803411](https://openairdocs.org/sdr/DALA2024031803411.md): Slat Track · corroded · Mar 15, 2024 · N125DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 1 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B.
- [SDR DALA2024031803410](https://openairdocs.org/sdr/DALA2024031803410.md): Slat Track · corroded · Mar 15, 2024 · N125DU · Airbus BD5001A10 · 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 606941-14AD REV D AND PRI 606941-14AD REV 0 MATCHED. (LP# 0245290)
- [SDR DALA2024031803409](https://openairdocs.org/sdr/DALA2024031803409.md): Slat Track · corroded · Mar 15, 2024 · N125DU · Airbus BD5001A10 · 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 606941-14AD REV D AND PRI 606941-14AD REV 0 MATCHED. (LP# 0245288)
- [SDR DALA2024031803408](https://openairdocs.org/sdr/DALA2024031803408.md): Slat Track · corroded · Mar 15, 2024 · N125DU · Airbus BD5001A10 · 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 606941-14AD REV D AND PRI 606941-14AD REV 0 MATCHED. (LP# 0245286)
- [SDR DALA2024031803407](https://openairdocs.org/sdr/DALA2024031803407.md): Slat Track · corroded · Mar 15, 2024 · N125DU · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 6 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK, REF 5742-01028-02B. REPAIRED RH SLAT TRACK NBR 6 UPPER FWD SURFACE IAW ER/A 606941-14AD REV D AND PRI 606941-14AD REV 0 MATCHED. (LP# 0245285)
- [SDR DALA2024011100501](https://openairdocs.org/sdr/DALA2024011100501.md): Unknown · unknown · Jan 9, 2024 · N125DU · Bombdr BD1001A10 · Fuselage Miscellaneous Structure
  > LOWER WTBF- CLIP CRACKED AT FORWARD LOWER RT. CORNER OF MID AVIONICS COMPARTMENT ACCESS CUTOUT. REMOVED AND REPLACED WTBF CLIP PER A220 ASRP 51-42-06. (LP# 0147223)
- [SDR DALA2024011100500](https://openairdocs.org/sdr/DALA2024011100500.md): Unknown · unknown · Jan 9, 2024 · N125DU · Bombdr BD1001A10 · Aerodynamic Fairings
  > WTBF LONGERON CRACKED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 012-0001:5110-2001/002 00004 REMOVED AND REPLACED WTBF LONGERON PER AMDS WC 5352-01038-07A. (LP# 0147007)
- [SDR DALA2023101808573](https://openairdocs.org/sdr/DALA2023101808573.md): Unknown · unknown · Oct 12, 2023 · N125DU · Bombdr BD1001A10 · Air Conditioning System
  > PARKED AT GATE WE STARTED SMELLING A HOT OIL ODOR THROUGH THE VENTS WITH APU RUNNING ONLY. C/W WORK CARD ODI. REPLACED RECIRCULATION FILTERS PER WORK CARD 0550-2003. NO ODORS/ DEFECTS NOTED. NO GO ODI PREVENTION ATA 2172 C/W. RAN APU WITH PACKS FULL HOT FOR 2
- [SDR DALA2024011600667](https://openairdocs.org/sdr/DALA2024011600667.md): Skin · damaged · Sep 13, 2023 · N125DU · Bombdr BD1001A10 · Fuselage Main, Plate/Skin
  > ON ARRIVAL ACS FOUND DAMAGE FWD OF L2 DOOR. FOUND DENT/GOUGE FWD OF L2 DOOR BETWEEN FRAMES 70 AND 72, AND STRINGERS 23L AND 25L. DENT MEASURES 5 INCHES VERTICALLY WITH.5 INCH WIDTH. PERFORMED DVI PER A220 AND TP 51-10-01-01AAA- 018A-A BOTH INTERNALLY AND EXTE
- [SDR DALA2023091407570](https://openairdocs.org/sdr/DALA2023091407570.md): Unknown · unknown · Sep 13, 2023 · N125DU · Bombdr BD1001A10 · Passenger/Crew Doors
  > ATTEMPTED TO REOPEN 1L TO BOARD PAX. DOOR JAMMED. RE-SEQUENCED FWD PASSENGER DOOR REF A220 AMP 52-00. PERFORMED OPS TEST OF MODE SELECT HANDLE MECHANISM REF A220 AMP 52-11. OPS NML. (LP# 4958560)

Next page: https://openairdocs.org/aircraft/N125DU/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 = 'N125DU' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N125DU/reports

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