# Service difficulty reports: N123DQ

A list on [N123DQ](https://openairdocs.org/aircraft/N123DQ.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 3 · 102 reports

- [SDR DALA2026092305317](https://openairdocs.org/sdr/DALA2026092305317.md): Wire · broken · Sep 17, 2026 · N123DQ · Airbus BD5001A10 · Light System Wiring
  > FWD SERVCE DOOR EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER A220 AMP 33-5 NO HELP. FOUND BROKEN WIRE GOING TO ASSEMBLY. SPLICED WIRE PER A220 ESPP 20-15 TEST OK THIS CLEARS MEL PLACARD REMOVED. (LP# 9474011; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026092305316](https://openairdocs.org/sdr/DALA2026092305316.md): Light · inoperative · Sep 17, 2026 · N123DQ · Airbus BD5001A10 · Emergency Lighting
  > FWD LEFT OVERWING EMERGENCY EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT IAW A220 AMP 33-55-02. OPS TEST GOOD. (LP# 9474010; AIRCRAFT WAS GROUNDED)
- [SDR DALA2026020900938](https://openairdocs.org/sdr/DALA2026020900938.md): Light · inoperative · Feb 6, 2026 · N123DQ · Airbus BD5001A10 · Emergency Lighting
  > FORWARD RT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT ASSEMBLY IAW AMP 33-55. OPS CHECKED GOOD. (LP# 7728279)
- [SDR DALA2026020900937](https://openairdocs.org/sdr/DALA2026020900937.md): Light · inoperative · Feb 6, 2026 · N123DQ · Airbus BD5001A10 · Emergency Lighting
  > FORWARD RT EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT ASSEMBLY IAW AMP 33-55. OPS CHECKED GOOD. (LP# 7728278)
- [SDR DALA2026020300806](https://openairdocs.org/sdr/DALA2026020300806.md): Door · iced · Jan 30, 2026 · N123DQ · Airbus BD5001A10 · Passenger/Crew Doors
  > FLIGHT ATTENDANTS ARE UNABLE TO DISARM DOOR 2L AFTER ARRIVAL AT DESTINATION. CLEARED OBSTRUCTION & ICE FROM DOOR 2L DRAINS, DOOR DISARMED & OPS CHECK NOW GOOD. OK FOR SVC. (LP# 7728258)
- [SDR DALA2025111208281](https://openairdocs.org/sdr/DALA2025111208281.md): Valve · faulted · Nov 9, 2025 · N123DQ · Airbus BD5001A10 · Pneumatic Indicating System
  > DECLARED EMERGENCY DUE TO "RT BLEED FAIL" MESSAGE WITH LEFT PACK ON MEL. REPLACED RT HIGH PRESSURE VALVE (HPV). (LP# 7670286)
- [SDR DALA2025032602235](https://openairdocs.org/sdr/DALA2025032602235.md): Skin · corroded · Mar 22, 2025 · N123DQ · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON FWD AND AFT WASTE BOX PREVIOUS REPAIR DOUBLER AT WASTE SERVICE DOOR OPENING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 063-0001:10-0653-8- 7228/001 00153 CMOR: REPAIRED PER PRI 602195-14 REV 0, PRI 602195-14 REV 1, PRI 602195-14 REV 2, AND F
- [SDR DALA2025032602234](https://openairdocs.org/sdr/DALA2025032602234.md): Striker · corroded · Mar 22, 2025 · N123DQ · Airbus BD5001A10 · Service Doors
  > CORROSION FOUND AROUND 3 HOLES ON AFT CORNER STRIKER, AFT RIGHT SERVICE DOOR. FOUND WORKING PRI FOR N/R 260 STEP 1 PART C. MARKED AREAS WITH BLACK MARKER. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 022-0001:5331-01297- 02B/002 00390 REPAIRED PER PRI 624617-14 R
- [SDR DALA2025032602231](https://openairdocs.org/sdr/DALA2025032602231.md): Scuff Plate · corroded · Mar 22, 2025 · N123DQ · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > FWD CARGO SILL, SCUFF PLATE ATTACH HOLE #1 CORRODED BEYOND LIMITS. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0499:5321-2015/002 00380 COMPLIED WITH ER/A 624684-14 REV ORIGINAL AND PRI REV 0. LINE 03 SHOULD STATE:
- [SDR DALA2025032602233](https://openairdocs.org/sdr/DALA2025032602233.md): Skin · corroded · Mar 21, 2025 · N123DQ · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AT AFT SERVICE DOOR AREA COVERED BY THE LOWER SILL SCUFF PLATE HAS CORROSION AROUND ATTACH FASTENER HOLES 2OL, 4OL, 5OL, 6OL, 8OL, 9OL,10OL, 11OL, 12OL, 13OL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 022-0001:5331-01297- 02B/001 00260 REPAIRED
- [SDR DALA2025032602232](https://openairdocs.org/sdr/DALA2025032602232.md): Scuff Plate · corroded · Mar 21, 2025 · N123DQ · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AT FORWARD SERVICE DOOR AREA COVERED BY THE LOWER SILL SCUFF PLATE HAS CORROSION AROUND ATTACH FASTENER HOLE 7OL, 8OL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 018-0001:5331-01297- 01B/001 00268 REPAIRED PER PRI 624621-14 REV 0, PRI 624621-14 R
- [SDR DALA2025031001816](https://openairdocs.org/sdr/DALA2025031001816.md): Seat Track · corroded · Mar 9, 2025 · N123DQ · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORROSION LBL 43.5 AT FRAME 74-72. -M-. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0575:5300-2016/004 00349 REPAIRED PER ERA 623167-14TR SECTION I. ERA SHOULD READ ERA 623167-14TR REV ORIG SECTION I (68
- [SDR DALA2025031001815](https://openairdocs.org/sdr/DALA2025031001815.md): Seat Track · corroded · Mar 9, 2025 · N123DQ · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORROSION LBL 23 AT FRAME 74-72. -M-. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0575:5300-2016/003 00348 REPAIRED PER ERA 623168-14TR SECTION I. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE
- [SDR DALA2025030901794](https://openairdocs.org/sdr/DALA2025030901794.md): Mount · corroded · Mar 8, 2025 · N123DQ · Airbus BD5001A10 · Fuselage, Equipment Attach Fittings
  > AIRCRAFT 8123, GALLEY G4 FWD HALF MOUNT FITTINGS CORRODED. CORRECTIVE ACTION: REPLACED FITTINGS W/REF TO SAFRAN CMM 25-30-17. (LP 0847834)
- [SDR DALA2025030601771](https://openairdocs.org/sdr/DALA2025030601771.md): Seat Track · corroded · Mar 5, 2025 · N123DQ · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT 8123, SEAT TRACKS FWD FUSELAGE - RH SIDE, INBOARD SEAT TRACK, FORWARD END, SHOWS EVIDENCE OF CORROSION. CORRECTIVE ACTION: REPLACED SEAT TRACK REF A220 ASRP 51-42-00 AND A220 DWG C02312600. (LP 0842670)
- [SDR DALA2025030601769](https://openairdocs.org/sdr/DALA2025030601769.md): Seat Track · corroded · Mar 4, 2025 · N123DQ · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT 8123, SEAT TRACK CORROSION RBL 23 AT FRAME 74-72. CORRECTIVE ACTION: REPLACED SEAT TRACK REF. A220 ASRP 51-42-00 AND A220 DWG C01342701 REV G. (LP 0840860)
- [SDR DALA2025030601768](https://openairdocs.org/sdr/DALA2025030601768.md): Seat Track · corroded · Mar 4, 2025 · N123DQ · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT 8123, SEAT TRACKS FWD FUSELAGE - RH SIDE, OUTBOARD SEAT TRACK, FORWARD END, SHOWS EVIDENCE OF CORROSION. CORRECTIVE ACTION: CORROSION CONTAINED WITH SPLICE REPAIR. ACCOMPLISHED SPLICE REPAIR PER ER/A 623174-14TR REV ORIGINAL. (LP 0840824)
- [SDR DALA2024122311956](https://openairdocs.org/sdr/DALA2024122311956.md): Duct · disconnected · Dec 21, 2024 · N123DQ · Airbus BD5001A10 · Air Distribution System
  > ON TAXI-IN SMOKE/ELECTRICAL ODOR THROUGHOUT THE AIRCRAFT, ALSO GOT A L PACK DISCHARGE DUCT DISCONNECTED INFO MESSAGE. C/W SMOKE/FUMES T/C 0550-2001, NTF, SUSPECT DUCT FOUND IN LOG 6562870 ALLOWED FOR PACK/AVIONICS EXHAUST INGESTION AND RECIRCULATION THROUGHOUT
- [SDR DALA2024122311955](https://openairdocs.org/sdr/DALA2024122311955.md): Cover · out of position · Dec 20, 2024 · N123DQ · Airbus BD5001A10 · Escape Slide
  > CHECK HARD COVER ON 2R DOOR EMER SLIDE. FOUND COVER BINDING ON DOOR SLIDE, SUSPECT BAD SLIDE. REMOVED 2R DOOR SLIDE AS PER A220 AMM 25-63. INSTALLED NEW SLIDE AS PER A220 WORK CARD 2563-4006, ALL CHECKS OK. REQUIRED INSPECTION COMPLIED WITH 202288 SLIDE, AFT S
- [SDR DALA2024121011577](https://openairdocs.org/sdr/DALA2024121011577.md): Unknown · odor · Dec 7, 2024 · N123DQ · Airbus BD5001A10 · Air Distribution System
  > DIRTY SOCK SMELL ON DEPARTURE DURING CLIMB. SMELL DISSIPATED AT CRUISE. C/W WORK CARD 0550-2001 ISOLATE SMOKE AND FUMES IN COCKPIT/CABIN. NOTE: #1 ENG ON MEL 36-12-00A. PRSOV AND HPV LOCKED CLOSED. NO FINDINGS NOTED. #1 ENG SUSPECTED SOURCE. C/W A220 EFIM SO
- [SDR DALA2024121011575](https://openairdocs.org/sdr/DALA2024121011575.md): Bleed Air Sys · odor · Dec 6, 2024 · N123DQ · Airbus BD5001A10 · Air Distribution System
  > FUME /DIRTY SOCK SMELL ON T/O DISSIPATED QUICKLY RETURNED ON FINAL APPROACH. PERFORMED A220 NO GO ODI PREVENTION ATA 2172-SMOKE /FUMES IN THE CABIN PERFORMED STEP 1:AMDS WORKCARD 0550-2001 STILL REQUIRES STEP 12 TO BE COMPLETED.FOUND SOURCE OF SMELL COMING F
- [SDR DALA2024092009269](https://openairdocs.org/sdr/DALA2024092009269.md): Slat Track · no discrepancy · Sep 19, 2024 · N123DQ · Airbus BD5001A10 · Propeller System
  > RH SLAT TRACT NBR 5 UPPER FWD SURFACE (2 LOCATIONS) REQUIRES NDT INSPECTION PER AMDS W/C 5742-01028-02B. PERFORMED EDDY CURRENT INSPECTION IAW ANDTP BD500-A-J51-01-20- 01AAA-353A-A. NO DEFECTS NOTED. (LP# 0565092)
- [SDR DALA2024092009268](https://openairdocs.org/sdr/DALA2024092009268.md): Slat Track · no discrepancy · Sep 19, 2024 · N123DQ · Airbus BD5001A10 · Standard Practices/Structures
  > LH SLAT TRACK NBR 3 LOWER AFT SURFACE REQUIRES NDT INSPECTION PER AMDS W/C 5742-01028-02A. PERFORMED EDDY CURRENT INSPECTION IAW ANDTP BD500-A-J51-01-20- 01AAA-353A-A. NO DEFECTS NOTED. (LP# 0565088)
- [SDR DALA2024092009267](https://openairdocs.org/sdr/DALA2024092009267.md): Slat Track · no discrepancy · Sep 19, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 2 LOWER AFT SURFACE REQUIRES NDT INSPECTION PER AMDS W/C 5742-01028-02A. PERFORMED EDDY CURRENT INSPECTION IAQ AND TP BD500-A-J51-01-20- 01AAA-353A-A NO DEFECTS NOTED. (LP# 0565077)
- [SDR DALA2024081308074](https://openairdocs.org/sdr/DALA2024081308074.md): Module · faulted · Aug 11, 2024 · N123DQ · Airbus BD5001A10 · Tire
  > SHIP 8123 -ATO- DUE TO "RT BRAKE FAIL" MESSAGE. CORRECTIVE ACTION: REPLACED TIRE PRESSURE MODULE. (LP# 6073953)
- [SDR DALA2024053005634](https://openairdocs.org/sdr/DALA2024053005634.md): Unknown · odor · May 29, 2024 · N123DQ · Airbus BD5001A10 · Air Distribution System
  > FAINT DIRTY SOCK SMELL FROM 4,000 FT.-8000 FT. DISSIPATED AFTER 1-2 MIN. T/S PER AMDS WORKCARD NUMBER 0550-2001 (ISOLATE SMOKE AND FUMES IN COCKPIT AND/OR CABIN) STEPS 1-4 COMPLETED (ER 955691). C/W STEPS 5 TO 8 (EC 741818). DURING HIGH PWR ENG RUN OIL SMELL N
- [SDR DALA2024040904237](https://openairdocs.org/sdr/DALA2024040904237.md): Valve · faulted · Apr 6, 2024 · N123DQ · Airbus BD5001A10 · Compressor Bleed Valve
  > SHIP 8123 - DIV - TO ATL DUE TO "R BLEED FAIL" MESSAGE. CORRECTIVE ACTION: DEFERRED RIGHT BLEED PER MEL 36-12-01B. LATER, REPLACED RIGHT PRSOV VALVE. (LP 0280826)
- [SDR DALA2024021302021](https://openairdocs.org/sdr/DALA2024021302021.md): Light · inoperative · Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Emergency Lighting
  > R4 EMERGENCY LIGHT INOP. REMOVED AND REPLACED R2 EXTERIOR EMERGENCY LIGHT ASSEMBLY IAW A220 AMP 33-55-02. OPS CK GOOD. (LP# 5558752)
- [SDR DALA2024021302020](https://openairdocs.org/sdr/DALA2024021302020.md): Slat Track · corroded · Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 10 LOWER FWD HAS EVIDENCE OF CORROSION AND SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 1008 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N ENTR
- [SDR DALA2024021302019](https://openairdocs.org/sdr/DALA2024021302019.md): Slat Track · corroded · Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 8 UPPER FWD HAS EVIDENCE OF CORROSION AND SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 1000 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N ENTR
- [SDR DALA2024021201902](https://openairdocs.org/sdr/DALA2024021201902.md): Slat Track · corroded · Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 10 UPPER AFT HAS EVIDENCE OF CORROSION AND SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 1012 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N ENTR
- [SDR DALA2024021201901](https://openairdocs.org/sdr/DALA2024021201901.md): Slat Track · corroded · Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 9 UPPER AFT O/B HAS EVIDENCE OF CORROSION AND SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 1005 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N E
- [SDR DALA2024021201900](https://openairdocs.org/sdr/DALA2024021201900.md): Slat Track · corroded · Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 7 UPPER AFT HAS EVIDENCE OF CORROSION AND SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0955 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N ENTR
- [SDR DALA2024021201899](https://openairdocs.org/sdr/DALA2024021201899.md): Slat Track · corroded · Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 7 LOWER FWD HAS EVIDENCE OF CORROSION AND SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0951 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N ENTR
- [SDR DALA2024021201898](https://openairdocs.org/sdr/DALA2024021201898.md): Slat Track · corroded · Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 6 UPPER FWD HAS EVIDENCE OF CORROSION AND SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0948 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N ENTR
- [SDR DALA2024021201897](https://openairdocs.org/sdr/DALA2024021201897.md): Slat Track · corroded · Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 6 LOWER AFT HAS EVIDENCE OF CORROSION AND SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0941 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N ENTR
- [SDR DALA2024021201896](https://openairdocs.org/sdr/DALA2024021201896.md): Slat Track · corroded · Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 5 UPPER FWD HAS EVIDENCE OF CORROSION AND SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0937 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N ENTR
- [SDR DALA2024021201895](https://openairdocs.org/sdr/DALA2024021201895.md): Slat Track · corroded · Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 5 LOWER I/B FWD HAS EVIDENCE OF CORROSION AND SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0930 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N E
- [SDR DALA2024021201894](https://openairdocs.org/sdr/DALA2024021201894.md): Slat Track · corroded · Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 5 LOWER AFT HAS EVIDENCE OF CORROSION AND SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0923 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N ENTR
- [SDR DALA2024021201893](https://openairdocs.org/sdr/DALA2024021201893.md): Slat Track · corroded · Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 4 UPPER AFT HAS EVIDENCE OF CORROSION AND SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0919 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N ENTR
- [SDR DALA2024021201892](https://openairdocs.org/sdr/DALA2024021201892.md): Slat Track · corroded · Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 4 UPPER I/B AFT HAS EVIDENCE OF CORROSION AND SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0914 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N E
- [SDR DALA2024021201891](https://openairdocs.org/sdr/DALA2024021201891.md): Slat Track · corroded · Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 4 LOWER FWD HAS EVIDENCE OF CORROSION AND SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0910 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N ENTR
- [SDR DALA2024021201890](https://openairdocs.org/sdr/DALA2024021201890.md): Slat Track · corroded · Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 3 UPPER FWD HAS EVIDENCE OF CORROSION AND NO SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0909 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N EN
- [SDR DALA2024021201889](https://openairdocs.org/sdr/DALA2024021201889.md): Slat Track · corroded · Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 2 UPPER FWD HAS EVIDENCE OF CORROSION AND SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0907 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N ENTR
- [SDR DALA2024021201888](https://openairdocs.org/sdr/DALA2024021201888.md): Slat Track · corroded · Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 2 LOWER O/B FWD HAS EVIDENCE OF CORROSION AND SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0905 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N E
- [SDR DALA2024021201887](https://openairdocs.org/sdr/DALA2024021201887.md): Slat Track · corroded · Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 2 LOWER AFT HAS EVIDENCE OF CORROSION AND SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0903 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N ENTR
- [SDR DALA2024021201886](https://openairdocs.org/sdr/DALA2024021201886.md): Slat Track · corroded · Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 1 LOWER AFT HAS EVIDENCE OF CORROSION AND NO SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0900 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N EN
- [SDR DALA2024021201885](https://openairdocs.org/sdr/DALA2024021201885.md): Slat Track · corroded · Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 1 UPPER AFT HAS EVIDENCE OF CORROSION AND NO SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0859 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N EN
- [SDR DALA2024021201884](https://openairdocs.org/sdr/DALA2024021201884.md): Slat Track · corroded · Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 1 UPPER FWD HAS EVIDENCE OF CORROSION AND NO SIGNS OF PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0857 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N EN
- [SDR DALA2024021201883](https://openairdocs.org/sdr/DALA2024021201883.md): Slat Track · corroded · Feb 7, 2024 · N123DQ · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 7 PINION TEETH HAS EVIDENCE OF WEAR. LIAISON ENGINEERING SUPPORT REQUIRED BEFORE FURTHER FLT. LOG-PAGE UPDATED @ 07FEB24 0853 UTC 02 CORR BY EASTMAN 01895233 IAH 07FEB24 ATA 5742 RII: N ENTR 01895233 W REPAIRED R/H SLAT TRACK NBR 7 PINION TE

Next page: https://openairdocs.org/aircraft/N123DQ/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 = 'N123DQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N123DQ/reports

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