# Service difficulty reports: N108DQ

A list on [N108DQ](https://openairdocs.org/aircraft/N108DQ.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 · 60 reports

- [SDR DALA2026020600859](https://openairdocs.org/sdr/DALA2026020600859.md): Light · damaged · Feb 3, 2026 · N108DQ · Airbus BD5001A10 · Emergency Lighting
  > FOUND DAMAGED ESCAPE PATH PHOTO LUMINESCENT STRIP AT 18AB - 20AB. REPLACED DAMAGED STRIP PER A220 AMM 33-56, OK FOR SERVICE. (LP# 8499319)
- [SDR DALA2025090206507](https://openairdocs.org/sdr/DALA2025090206507.md): Control Unit · faulted · Aug 27, 2025 · N108DQ · Airbus BD5001A10 · Landing Gear Position and Warning
  > ATB - DUE TO SEVERAL FLIGHT CONTROL AND LANDING GEAR FAULTS. DECLARED AN EMERGENCY AND RETURNED TO SLC. REMOVED AND REPLACED NR 2 LGSCU, OPS CHECK NORMAL. (LP# 7202625)
- [SDR DALA2025082106249](https://openairdocs.org/sdr/DALA2025082106249.md): Apu · odor · Aug 19, 2025 · N108DQ · Airbus BD5001A10 · Airborne Auxiliary Power Unit (APU) System
  > AT GATE ON APU, STRANGE NOISE + BURNING SMELL, RIGHT PACK OVHT, R PACK FAIL, + PACK FAULT R BYPASS VLV INOP SMELL DISSIPATED AFTER R PACK SHUTOFF. FOUND RT ACM HOUSING CRACKED AND FAN BLADE MISSING. REMOVED ACM PER A220 AMP 21-51-03, REMOVED HEAT EXCHANGER PER
- [SDR DALA2025082006225](https://openairdocs.org/sdr/DALA2025082006225.md): Power Supply · inoperative · Aug 16, 2025 · N108DQ · Airbus BD5001A10 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHTS SYSTEMS - OVERWING EMERGENCY LIGHTS LT OVERWING EMERGENCY LIGHT FAULT ON CMS. LT OWED LT REPLACED (2X), EPSU REPLACED (3X). SKYWISE REPORTING FAULT 3351F0006. EPSU 3 INTERNAL FAULT. INTERROGATE OMS, DOCUMENT AND RECORD FINDINGS. PERFO
- [SDR DALA2025081906217](https://openairdocs.org/sdr/DALA2025081906217.md): Power Supply · inoperative · Aug 13, 2025 · N108DQ · Airbus BD5001A10 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHTS SYSTEMS - OVERWING EMERGENCY LIGHTS MEL NUMBER ADDED FOR DISPATCH RELEASE, LOG RE DEFERRAL REQUIRED. EMER LIGHT FAULT. R/R EPSU 3 & BATTERY PER AMP 33-51. DURING RE-INSTALL OF CEILING FAP DISPLAYED LT OWEED EMERGENCY LIGHTS FAULT. REI
- [SDR DALA2025080705931](https://openairdocs.org/sdr/DALA2025080705931.md): Light · no test · Aug 5, 2025 · N108DQ · Airbus BD5001A10 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHTS SYSTEMS - OVERWING EMERGENCY LIGHTS MEL NUMBER ADDED FOR DISPATCH RELEASE, LOG RE DEFERRAL REQUIRED. EMER LIGHTS FAULT - LEFT HAND OWEED DOOR ON CMS PANEL. R/R EPSU 3 PER A220 EFIM SOLUTION ID# 1-14786. CHKS NML. MEL/PLACARD REMOVED.
- [SDR DALA2025080505880](https://openairdocs.org/sdr/DALA2025080505880.md): Power Supply · faulted · Jul 31, 2025 · N108DQ · Airbus BD5001A10 · Emergency Lighting
  > EMERGENCY LIGHTS FAULT, LT OVERWING EED DOOR FAULT ON CMS PANEL. REMOVED CEILING PANEL FOR EPSU 3 & 4. REPLACED EPSU 3 IAW AMP 33-51-01. FAULT CODE 3351F0006 PRESENT ON OMS CURRENT FAULTS. EMERGENCY LIGHTS OPS NORMAL BUT FAULT STILL PRESENT ON CMS. BATTER
- [SDR DALA2025080505872](https://openairdocs.org/sdr/DALA2025080505872.md): Light · inoperative · Jul 30, 2025 · N108DQ · Airbus BD5001A10 · Emergency Lighting
  > AFT LT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R LT OWEED EXTERNAL LIGHT IAW AMP 33-55. OPS TESTS NML.
- [SDR DALA2025072905702](https://openairdocs.org/sdr/DALA2025072905702.md): Light · inoperative · Jul 27, 2025 · N108DQ · Airbus BD5001A10 · Emergency Lighting
  > CABIN CHIME 3 TIMES REPEATED WITH EMER LIGHTS FAULT - LH OWEED DOOR MSG ON CMS PANEL. FOUND FWD LT EXTERIOR OWEED LIGHT INOP. R/R FWD LT EXTERIOR OWEED LIGHT PER A220 AMP 33-55. OPS TEST GOOD. (LP# 6359832)
- [SDR DALA2025041002788](https://openairdocs.org/sdr/DALA2025041002788.md): Light · inoperative · Apr 7, 2025 · N108DQ · Airbus BD5001A10 · Emergency Lighting
  > EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE. ADDITIONAL LOCATIONS 19B, 20B - STRIP IS PRESENT BUT NOT ATTACHED TO THE FLOOR. / INTERIOR. INSTALLED STRIP AT SEAT 19/18B OPS CHECK GOOD. (LP# 0900476)
- [SDR DALA2025032602230](https://openairdocs.org/sdr/DALA2025032602230.md): Waste Box · corroded · Mar 21, 2025 · N108DQ · Airbus BD5001A10 · Fuselage Internal Mounting Structure
  > DURING DVI ON WASTE BOX AREA, FOUND CORROSION ON EXTERNAL SKIN SURFACE AT STGR35L, FR75+5 INCHES. ACCOMPLISHED CORROSION REMOVAL PER ERA 624822-14AD REV ORG ASSOCIATED ER/A 14-624822 ADDED FOR AC 8108. (LP# 0870328)
- [SDR DALA2025032502212](https://openairdocs.org/sdr/DALA2025032502212.md): Doubler · damaged · Mar 20, 2025 · N108DQ · Airbus BD5001A10 · Fuselage Main, Plate/Skin
  > TOILET SERVICE DOOR CUTOUT DOUBLER, FWD EDGE DAMAGED. WORK ACCOMPLISHED ON ER/A # 624822-14 AD REV - ORIGINAL ASSOCIATED ER/A 14-624822 ADDED FOR AC 8108. (LP# 0868332)
- [SDR DALA2025032502211](https://openairdocs.org/sdr/DALA2025032502211.md): Door Frame · corroded · Mar 20, 2025 · N108DQ · Airbus BD5001A10 · Fuselage Main, Structure
  > ***CORROSION*** ON AFT EQUIPMENT BAY DOOR CUTOUT FWD FRAME LOCATED AT BODY FRAME FR81, LBL 5, 2.5 INCHES ABOVE SKIN. C/W ER/A 624905-14 REV: ORG ASSOCIATED ER/A 14-624905 ADDED FOR AC 8108. CORRECTION ADDED: MONITOR CREATED ON LOG PAGE 0866845 TERMINATING 350
- [SDR DALA2025030901792](https://openairdocs.org/sdr/DALA2025030901792.md): Seat Track · corroded · Mar 8, 2025 · N108DQ · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT 8108, CORROSION ON CABIN SEAT TRACK UPPER SURFACE FR74 RBL 23. CORRECTIVE ACTION: REPLACED SEAT TRACK AT RBL 25 FR 57+10 TO FR 74 IA.W. A220 ASRP BD500A-J51-42-20-00AAA-078A-A AND DWG PLC01342701 REV -G. (LP 0847463)
- [SDR DALA2025030901791](https://openairdocs.org/sdr/DALA2025030901791.md): Seat Track · corroded · Mar 8, 2025 · N108DQ · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT 8108, CORROSION ON CABIN SEAT TRACK UPPER SURFACE FR74 LBL 43.5. CORRECTIVE ACTION: REPLACED SEAT TRACK AT LBL 43.5 FR 61 TO FR74 IAW A220 ASRP BD500-A-J51-42-06-00AAA-078A-A, BD500-A-J51-42-21-00AAA-078A AND DWG# C01342701 REV G. (LP 0847261)
- [SDR DALA2025030801790](https://openairdocs.org/sdr/DALA2025030801790.md): Seat Track · corroded · Mar 7, 2025 · N108DQ · Airbus BD5001A10 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT 8108, CORROSION ON CABIN SEAT TRACK UPPER SURFACE FR74 LBL 23. CORRECTIVE ACTION: REPLACED SEAT TRACK FROM FR 61-74 LBL 23 IAW DWG# C01342701 REV G, AND A220 ASRP BD500-A-J51-42-06-00AAA-078A-A AND BD500-A-J51-42-21-00AAA-078A-A.
- [SDR DALA2025021801191](https://openairdocs.org/sdr/DALA2025021801191.md): Bracket · cracked · Feb 14, 2025 · N108DQ · Airbus BD5001A10 · Fuselage Miscellaneous Structure
  > CRACK ON FLOOR MOUNTING BEAM BRACKET AT FR15, RBL23, WL147. REMOVED, REPLACED AND INSTALLED NEW FLOOR MOUNTING BEAM BRACKET AT FR15, RBL 23,WL 147. IAW A220 ASRP BD500-A-J51-42-21-00AAA- 0784-A AND BOMBARDIER DATA SET NUMBER C01213300. (LP# 0811038)
- [SDR DALA2025010212126](https://openairdocs.org/sdr/DALA2025010212126.md): Unknown · odor · Dec 30, 2024 · N108DQ · Airbus BD5001A10 · Air Distribution System
  > FUME EVENT AFTER T/O. SMELL DEV. SHORTLY AFTER FULL PWR ON T/O. STARTED TO DISSIPATE AFTER APPROX 3-4 MIN AND GONE BY 10 MIN. "FA' REPORTED METALLIC SMELL IN FWD GALLEY, CHECKED OVEN AND NO REAL ISSUE THERE. SURVEY SUBMITTED. WORKING WORK CARD A220 0550-2001.
- [SDR DALA2024091208958](https://openairdocs.org/sdr/DALA2024091208958.md): Slat Track · corroded · Sep 9, 2024 · N108DQ · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR5 UPPER FWD SURFACE FOUND WITH CORROSION AND BLENDED PER AMDS W/C 5742-01028-02A, REQUIRES NDT INSPECTION TO CHECK FOR SIGNS OF CRACKS. LH SLAT TRACK NBR5 UPPER FWD SURFACE CORROSION BLENDED PER AMDS W/C 5742-01028-02A, PERFORMED HFEC NO CRACK
- [SDR DALA2024091208957](https://openairdocs.org/sdr/DALA2024091208957.md): Slat Track · corroded · Sep 9, 2024 · N108DQ · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR1 UPPER FWD SURFACE FOUND WITH CORROSION AND BLENDED PER AMDS W/C 5742-01028-02A, REQUIRES NDT INSPECTION TO CHECK FOR SIGNS OF CRACKS. LH SLAT TRACK NBR1 UPPER FWD SURFACE CORROSION BLENDED PER AMDS W/C 5742-01028-02A, PERFORMED HFEC NO CRACK
- [SDR DALA2024091208956](https://openairdocs.org/sdr/DALA2024091208956.md): Slat Track · corroded · Sep 9, 2024 · N108DQ · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR7 LOWER FWD I/B SURFACE FOUND WITH CORROSION AND BLENDED PER AMDS W/C 5742-01028-02B, REQUIRES NDT INSPECTION TO CHECK FOR SIGNS OF CRACKS. SLAT TRACK NBR7 LOWER FWD I/B SURFACE CORROSION BLENDED PER AMDS W/C 5742-01028-02B, PERFORMED HFEC NO
- [SDR DALA2024091208955](https://openairdocs.org/sdr/DALA2024091208955.md): Slat Track · corroded · Sep 9, 2024 · N108DQ · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR3 UPPER FWD SURFACE FOUND WITH CORROSION AND BLENDED PER AMDS W/C 5742-01028-02A, REQUIRES NDT INSPECTION TO CHECK FOR SIGNS OF CRACKS. RH SLAT TRACK NBR3 UPPER FWD SURFACE CORROSION BLENDED PER AMDS W/C 5742-01028-02B, PERFORMED HFEC NO CRACK
- [SDR DALA2024091208954](https://openairdocs.org/sdr/DALA2024091208954.md): Slat Track · corroded · Sep 9, 2024 · N108DQ · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR2 LOWER FWD O/B SURFACE FOUND WITH CORROSION AND BLENDED PER AMDS W/C 5742-01028-02B, REQUIRES NDT INSPECTION TO CHECK FOR SIGNS OF CRACKS. RH SLAT TRACK NBR2 LOWER FWD O/B SURFACE CORROSION BLENDED PER AMDS W/C 5742-01028-02B, PERFORMED HFEC
- [SDR DALA2024043004800](https://openairdocs.org/sdr/DALA2024043004800.md): Light · inoperative · Apr 27, 2024 · N108DQ · Airbus BD5001A10 · Emergency Lighting
  > DURING SERVICE CHECK FOUND LT AFT EXTERIOR EMERGENCY LIGHT INOP. R/R LEFT AFT EMERGENCY LIGHT PER A220 AMP 33-55. OPS CHECK GOOD. MEL AND PLACARDS AND M PROCEDURES REMOVED. OK FOR SVC. (LP# 4377426)
- [SDR DALA2024031803422](https://openairdocs.org/sdr/DALA2024031803422.md): None · none · Mar 14, 2024 · N108DQ · Airbus BD5001A10 · Passenger Compartment Equipment
  > HALON FIRE EXTINGUISHER DISCHARGED 26-20-01. REMOVED AND REPLACED FIRE BOTTLE AT 28AB PER A220 AMP 26-23. (LP# 5346759).
- [SDR DALA2024020601598](https://openairdocs.org/sdr/DALA2024020601598.md): Light · inoperative · Feb 1, 2024 · N108DQ · Airbus BD5001A10 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHTS SYSTEMS - DOOR EMERGENCY LIGHT - 1R EXTERIOR EMERGENCY LIGHT INOP. REPLACED R1 EXTERNAL EMERGENCY LIGHT PER A220 AMP 33-55-02. TESTS OK. CLEARED MEL/REMOVED PLACARDS. (LP# 4359281)
- [SDR DALA2024020601594](https://openairdocs.org/sdr/DALA2024020601594.md): Slat Track · corroded · Feb 1, 2024 · N108DQ · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 6 UPPER 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 UPPER AFT SURFACE IAW PRI 607660- 14AD REV 0 AND ERA REV C
- [SDR DALA2024020601593](https://openairdocs.org/sdr/DALA2024020601593.md): Slat Track · corroded · Feb 1, 2024 · N108DQ · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 4 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 4 LOWER AFT SURFACE IAW PRI 607660- 14AD REV 0 AND ERA REV C
- [SDR DALA2024020601592](https://openairdocs.org/sdr/DALA2024020601592.md): Slat Track · corroded · Feb 1, 2024 · N108DQ · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 7 UPPER 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 UPPER AFT SURFACE IAW PRI 607660- 14AD REV 0 AND ERA REV C M
- [SDR DALA2024020601591](https://openairdocs.org/sdr/DALA2024020601591.md): Slat Track · corroded · Jan 31, 2024 · N108DQ · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 5 LOWER HAS EVIDENCE OF CORROSION & PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED R/H SLAT TRACK #5 LOWER FWD SURFACE PER ERA 607659-14AD REV C AND PRI REV 0 MATCHED. (LP# 018090
- [SDR DALA2024020601590](https://openairdocs.org/sdr/DALA2024020601590.md): Slat Track · corroded · Jan 31, 2024 · N108DQ · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 5 UPPER FWD HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED R/H SLAT TRACK #5 UPPER FWD SURFACE PER ERA 607659-14AD REV C AND PRI REV 0 MATCHED. (LP#
- [SDR DALA2024020601589](https://openairdocs.org/sdr/DALA2024020601589.md): Slat Track · corroded · Jan 31, 2024 · N108DQ · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 8 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED R/H SLAT TRACK #8 UPPER AFT SURFACE PER ERA 607659- 14AD REV C AND PRI REV 0 MATCH
- [SDR DALA2024020601588](https://openairdocs.org/sdr/DALA2024020601588.md): Slat Track · corroded · Jan 31, 2024 · N108DQ · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 7 UPPER FWD SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED R/H SLAT TRACK #7 UPPER FWD SURFACE PER ERA 607659-14AD REV C AND PRI REV 0 MATCH
- [SDR DALA2024020601587](https://openairdocs.org/sdr/DALA2024020601587.md): Slat Track · corroded · Jan 31, 2024 · N108DQ · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 6 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED R/H SLAT TRACK #6 LOWER AFT SURFACE PER ERA 607659-14AD REV C AND PRI REV 0 MATCHE
- [SDR DALA2024020601586](https://openairdocs.org/sdr/DALA2024020601586.md): Slat Track · corroded · Jan 31, 2024 · N108DQ · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 6 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED R/H SLAT TRACK #6 UPPER AFT SURFACE PER ERA 607659- 14AD REV C AND PRI REV 0 MATCH
- [SDR DALA2024020601585](https://openairdocs.org/sdr/DALA2024020601585.md): Slat Track · corroded · Jan 31, 2024 · N108DQ · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 5 LOWER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED R/H SLAT TRACK #5 LOWER AFT SURFACE PER ERA 607659-14AD REV C AND PRI REV 0 MATCHE
- [SDR DALA2024020601584](https://openairdocs.org/sdr/DALA2024020601584.md): Slat Track · corroded · Jan 31, 2024 · N108DQ · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 5 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED R/H SLAT TRACK #5 UPPER AFT SURFACE PER ERA 607659- 14AD REV C AND PRI REV 0 MATCH
- [SDR DALA2024020601583](https://openairdocs.org/sdr/DALA2024020601583.md): Slat Track · corroded · Jan 31, 2024 · N108DQ · Airbus BD5001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 4 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLT. REPAIRED R/H SLAT TRACK #4 UPPER AFT SURFACE PER ERA 607659-14AD REV C AND PRI REV 0 MATCHE
- [SDR DALA2023122710655](https://openairdocs.org/sdr/DALA2023122710655.md): Unknown · unknown · Dec 24, 2023 · N108DQ · Airbus BD5001A10 · Air Distribution System
  > WITH ENGINE STARTED ON TAXI-OUT FLT ATTENDANT REPORTED "WET LAUNDRY SMELL" IN AFT FUSELAGE AND AFT GALLEY. SMELL DISSIPATED AFTER ABOUT 2 MINUTES. CALLED ATL RADIO AND MCC ADVISED WE RETURN TO GATE. C/W WORK CARD 0550-6001 ENG SOURCE SMOKE AND OIL FUMES. NO DE
- [SDR DALA2023122910726](https://openairdocs.org/sdr/DALA2023122910726.md): Unknown · unknown · Dec 23, 2023 · N108DQ · Airbus BD5001A10 · Air Distribution System
  > AFTER LANDING IN LGA "DIRTY SOCK" FUMES SMELL DURING TAXI IN. AFTER APU ONLINE SMELL BEGAN TO DISSIPATE. NO ODOR NOTED IN CABIN. C/W ECS DECONTAMINATION WORK CARD 0550-2003. NO OIL RESIDUE OR ANY CONTAMINATION FOUND. (LP# 5002254)
- [SDR DALA2023122710652](https://openairdocs.org/sdr/DALA2023122710652.md): Unknown · unknown · Dec 21, 2023 · N108DQ · Airbus BD5001A10 · Air Distribution System
  > DURING TAXI OUT FWD FA SMELLED DIRTY SOCK SMELL, NOT REPORTED TO F.O. ON CLIMB OUT SMELL SENSED IN FD AND FWD GALLEY BUT DISSIPATED QUICKLY. ON APPROACH WITH POWER ADVANCING SMELL RETURNED TO FO IN CABIN. STARTED APU IMMEDIATELY AND SMELL DISSIPATED. SMOKE /FU
- [SDR DALA2023121110112](https://openairdocs.org/sdr/DALA2023121110112.md): Unknown · unknown · Dec 10, 2023 · N108DQ · Airbus BD5001A10 · Emergency Lighting
  > FOUND ON SVC CHK FORWARD SVC DOOR UPPER EMERGENCY LIGHT INOP. FOUND FSD OVERDOOR EMERGENCY LIGHT PANEL HAD 0 VOLTAGE TO LIGHT AND DOWN WASH LIGHT. R/R FSD OVERDOOR EMERGENCY LIGHT PANEL ASSY (MPN 8149203-115 S/N UKN) IAW 33-52. PERFORMED OPS CHK OF EPSU SYSTEM
- [SDR DALA2023072506002](https://openairdocs.org/sdr/DALA2023072506002.md): Unknown · unknown · Jul 22, 2023 · N108DQ · Bombdr BD1001A10 · Leading Edge Devices
  > PER AMDS 5742-01028-02A.LH WING SLAT TRACK #7 HAS CORROSION ON FWD INBD UPPER SIDE. SURFACE PREVIOUSLY REWORKED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 003-0001:5742-01028-02A/003 00003 REPAIRED SLAT TRACK PER AMD
- [SDR DALA2023072506001](https://openairdocs.org/sdr/DALA2023072506001.md): Unknown · unknown · Jul 22, 2023 · N108DQ · Bombdr BD1001A10 · Leading Edge Devices
  > PER AMDS 5742-01028-02B. RH WING SLAT TRACK #4 HAS DAMAGE ON UPPER INBD SIDE AND LOWER OUTBD SIDE SURFACE, SLAT HAS BEEN PREVIOUSLY REWORKED. CEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFOR MATION 002-0001:5742-01028-02B/006 0001
- [SDR DALA2023072506000](https://openairdocs.org/sdr/DALA2023072506000.md): Unknown · unknown · Jul 22, 2023 · N108DQ · Bombdr BD1001A10 · Leading Edge Devices
  > PER AMDS 5742-01028-02B. RH WING SLAT TRACK #4 HAS CORROSION ON LOWER AFT. SURFACE PREVIOUSLY REWORKED. 002-0001:5742-01028-02B/005 00012 REPAIRED SLAT TRACK PER AMDS 5742-0102 8-02B, PRI 607659-14AD REV A PRI REV 0, REV 1 AND ER/A 607659-14AD REV A. (LP# 2879
- [SDR DALA2023072505999](https://openairdocs.org/sdr/DALA2023072505999.md): Unknown · unknown · Jul 22, 2023 · N108DQ · Bombdr BD1001A10 · Leading Edge Devices
  > PER AMDS 5742-01028-02B. RH WING SLAT TRACK #10 HAS CORROSION ON LOWER AFT FWD. SURFACE PREVIOUSLY REWORKED. 002-0001:5742-01028-02B/004 00009 REPAIRED SLAT TRACK PER AMDS 5742-0102 8-02B, PRI 607659-14AD REV A PRI REV 0, REV 1 AND ER/A 607659-14AD REV A. (LP#
- [SDR DALA2023072505998](https://openairdocs.org/sdr/DALA2023072505998.md): Unknown · unknown · Jul 22, 2023 · N108DQ · Bombdr BD1001A10 · Leading Edge Devices
  > PER AMDS 5742-01028-02B. RH WING SLAT TRACK #8 HAS CORROSION ON LOWER AFT INBD AFT SIDE. SURFACE PREVIOUSLY REWORKED. 002-0001:5742-01028-02B/003 00008 REPAIRED SLAT TRACK PER AMDS 5742-0102 8-02B, PRI 607659-14AD REV A PRI REV 0, REV 1 AND ER/A 607659-14AD RE
- [SDR DALA2023072505997](https://openairdocs.org/sdr/DALA2023072505997.md): Unknown · unknown · Jul 22, 2023 · N108DQ · Bombdr BD1001A10 · Leading Edge Devices
  > PER AMDS 5742-01028-02B. RH WING SLAT TRACK #4 HAS CORROSION ON UPPER AFT. SURFACE PREVIOUSLY REWORKED. 002-0001:5742-01028-02B/002 00007 REPAIRED SLAT TRACK PER AMDS 5742-0102 8-02B, PRI 607659-14AD REV A PRI REV 0, REV 1 AND ER/A 607659-14AD REV A. (LP# 2879
- [SDR DALA2023072505996](https://openairdocs.org/sdr/DALA2023072505996.md): Unknown · unknown · Jul 22, 2023 · N108DQ · Bombdr BD1001A10 · Leading Edge Devices
  > PER AMDS 5742-01028-02B. RH WING SLAT TRACK #2 HAS CORROSION ON LOWER AFT. SURFACE PREVIOUSLY REWORKED. 002-0001:5742-01028-02B/001 00006 REPAIRED SLAT TRACK PER AMDS 5742-0102 8-02B, PRI 607659-14AD REV A PRI REV 0, REV 1 AND ER/A 607659-14AD REV A. (LP# 2879
- [SDR DALA2023072505995](https://openairdocs.org/sdr/DALA2023072505995.md): Unknown · unknown · Jul 22, 2023 · N108DQ · Bombdr BD1001A10 · Leading Edge Devices
  > PER AMDS 5742-01028-02A.LH WING SLAT TRACK #11 HAS CORROSION ON LOWER FWD. SURFACE PREVIOUSLY REWORKED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 003-0001:5742-01028-02A/005 00005 REPAIRED SLAT TRACK PER AMDS 5741-01

Next page: https://openairdocs.org/aircraft/N108DQ/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 = 'N108DQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N108DQ/reports

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