# Service difficulty reports: N385DZ A list on [N385DZ](https://openairdocs.org/aircraft/N385DZ.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR DALA2026061203555](https://openairdocs.org/sdr/DALA2026061203555.md): Control Unit · smoke · Jun 12, 2026 · N385DZ · Airbus A321211 · Landing Gear Brake System > DIV- TO CLT DUE TO CREW REPORT OF LIGHT SMOKE IN THE COCKPIT AND CABIN WITH AN ASSOCIATED BSCU 2 ECAM FAULT. REPLACED BSCU. - [SDR DALA2025121109054](https://openairdocs.org/sdr/DALA2025121109054.md): Power Supply · inoperative · Dec 10, 2025 · N385DZ · Airbus A321211 · Emergency Lighting > WHILE CONDUCTING EMERGENCY LIGHT TEST, FOUND FAULT EPSU (15WL) MID L. FOUND RECEPTACLE DAMAGED/SHORTED AT 7260VC2 CAUSING EPSU AT 15WL TO BLOW INTERNAL FUSE. REPLACED EPSU 14WL PER A321 AMM 33-51-38. CHECKS NORMAL. REPLACED RECEPTACLE 726OVC2. REPLACED EPS - [SDR DALA2025051603786](https://openairdocs.org/sdr/DALA2025051603786.md): Skin · dented · May 10, 2025 · N385DZ · Airbus A321211 · Leading Edge Devices > SHIP 3085 DENT SLAT 5 LOCATED 23 INCHES FROM IB EDGE RH WING. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON SLAT 5 LOCATED 23 INCHES FROM IB EDGE RH WING AS PER A321 SRM 57-40-00 (0958346) - [SDR DALA2025051503751](https://openairdocs.org/sdr/DALA2025051503751.md): Skin · not reported · May 9, 2025 · N385DZ · Airbus A321211 · Fuselage Main, Plate/Skin > SHIP 3085 PERFORM ER/A 626152-14AD ON EXTERNAL SKIN FROM FR47 TO FR70 BETWEEN STR 23LH AND STR 23RH AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 626152-14AD REV ORIGINAL MATCHES WITH ALL STEPS ON PRI 626152-14AD REV 0 IT HAS BEEN VALIDATED. PERFORM - [SDR DALA2025051503750](https://openairdocs.org/sdr/DALA2025051503750.md): Bushing · migrated · May 9, 2025 · N385DZ · Airbus A321211 · Fuselage Main, Structure > SHIP 3085 MIGRATED BUSHING KEEL BEAM FWD LUG LH MLG DOOR ACTUATOR. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON LH MLG DOOR KEEL BEAM ACTUATOR FITTING FWD LUG AS PER ER/A # 626022-14AD REV. ORIGINAL SECTION I HAS BEEN COMPLIED WITH. (0957647) - [SDR DALA2025050803564](https://openairdocs.org/sdr/DALA2025050803564.md): Seat Track · corroded · May 2, 2025 · N385DZ · Airbus A321211 · Fuselage, Seat/Cargo Attach Fittings > SHIP 3085 CORROSION SEAT TRACK +Y1292 AT LEVEL FR66 AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED SEAT TRACK Y1292 LOC BTW FR64 TO FR66 AFT GALLEY AREA AS PER A321 SRM 51-72-11 (0945752) - [SDR DALA2025043003339](https://openairdocs.org/sdr/DALA2025043003339.md): Floor Support · corroded · Apr 28, 2025 · N385DZ · Airbus A321211 · Fuselage Miscellaneous Structure > SHIP 3085 CORROSION LOWER SILL BTW FR 67 TO FR 68 STR 23R AT AFT GALLEY AREA. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTION ON LOWER SILL BTW FR 67 TO FR 68 STR 23R AT AFT GALLEY AREA AS PER A321 SRM 53-41-14 (0938252) - [SDR DALA2025043003338](https://openairdocs.org/sdr/DALA2025043003338.md): Floor Support · corroded · Apr 28, 2025 · N385DZ · Airbus A321211 · Fuselage Miscellaneous Structure > SHIP 3085 CORROSION LOWER SILL BTW FR67 TO FR68 AT LEVEL STR 23L PASSENGER CABIN. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON LOWER SILL BTW FR 67 TO FR 68 STR 23L AT AFT GALLEY AREA AS PER A321 SRM 53-41-14 (0938237) - [SDR DALA2025042803298](https://openairdocs.org/sdr/DALA2025042803298.md): Shear Plate · cracked · Apr 25, 2025 · N385DZ · Airbus A321211 · Fuselage Miscellaneous Structure > SHIP 3085 CRACK SHEAR PLATE BTW FR 69 TO FR 70 STR 23R AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED SHEAR PLATE AND FASTENERS LOCATED BTW FR 69 TO FR 70 STR 23R AT AFT GALLEY AREA AS PER A321 SRM 51-42-11 (0933226) - [SDR DALA2025042803296](https://openairdocs.org/sdr/DALA2025042803296.md): Bearing · migrated · Apr 25, 2025 · N385DZ · Airbus A321211 · Elevator Miscellaneous Structure > SHIP 3085 MIGRATED BEARING HINGE 4 ON RH ELEVATOR. CORRECTIVE ACTION: REPLACED HINGE FITTING #4 ON RH ELEVATOR AS PER A320 FAM AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. (0932798) - [SDR DALA2023052504158](https://openairdocs.org/sdr/DALA2023052504158.md): Unknown · unknown · May 18, 2023 · N385DZ · Airbus A321211 · Emergency Lighting > FOUND SEAT-MOUNTED EXERGENCY EXIT LIGHT AT 17C INOP. T/S PER A321 AWM 33-51 FOUND PIN ON CONNECTER BY LIGHT PUSHED BACK. (LP# 9648676) - [SDR DALA2023030701685](https://openairdocs.org/sdr/DALA2023030701685.md): None · none · Mar 3, 2023 · N385DZ · Airbus A321211 · Landing Gear Position and Warning > IN FO ONLY DURING LANDING GEAR EXTENSION ON APPROACH NOSE GEAR DOWN ANNUNCIATION LIGHT DID NOT INDICATE GREEN. BULB DID NOT TEST, WE TAPPED ON LIGHT AND IT DID NOT LIGHT. AFTER GO AROUND THE LIGHT TESTED NORMAL NEXT APPROACH AND LANDING NORMAL. LDG GEAR INDICA - [SDR DALA2022072005014](https://openairdocs.org/sdr/DALA2022072005014.md): Computer · installed · Jul 16, 2022 · N385DZ · Airbus A321211 · Central Maintenance Computer > C/W ER/A 600868-14 REV ORIG SEC I - A/C 3085 FOMAX 3 UPGRADE AND ACMS LOAD B 2.5 UPGRADE. C/W ER/A 600868-14 REV ORIG SEC I - A/C 3085 FOMAX 3 UPGRADE AND ACMS LOAD B 2.5 UPGRADE. C/W ER/A 600868-14 REV ORIG. FOMAX UPGRADE AND FDIMU S/W LOAD COMPLETE. (LP# 232 - [SDR DALA2022061504206](https://openairdocs.org/sdr/DALA2022061504206.md): Skin · none · Jun 10, 2022 · N385DZ · Airbus A321211 · Fuselage Main, Plate/Skin > ER/A 599938-14 HAS BEEN ISSUED FOR A FUSELAGE SKIN REPAIR AT FR6 6/67 AND S-41/43RH. FOLLOW ON ACTION IS REQUIRED. SECTION I IS LIMITED TO 6 MONTHS (182 DAYS) FROM 09JUN22 WHILE A DAMAGE TOLERANCE ANALYSIS ( DTA) CAN TAKE PLACE. ER/A TO BE REVISED PRIOR TO TH - [SDR DALA2022061504202](https://openairdocs.org/sdr/DALA2022061504202.md): Skin · damaged · Jun 10, 2022 · N385DZ · Airbus A321211 · Fuselage Main, Plate/Skin > MON, 30 L/L, 8749824;VIS;FOUND DAMAGE TO FUSELAGE APPX 10" AFT OF FRAME 66 BETWEEN. REPAIRED DAMAGED EXTERIOR FUSELAGE SKIN BETWEEN FR66 AND FR67, AND BETWEEN S-41RH AND S-43RH IAW ER/A 599938-14 REV ORIGINAL ASSOCIATED ER/A 14-599938 ADDED FOR AC 3085. (LP# - [SDR DALA2022060904050](https://openairdocs.org/sdr/DALA2022060904050.md): Tail Cone · dented · Jun 8, 2022 · N385DZ · Airbus A321211 · Fuselage Main, Plate/Skin > DENT IN SKIN ON TAILCONE, 0 BL, APPROX 10" AFT OF RUDDER POSITION INDICATOR. INSTALLED REPAIR AT TAILCONE 0 BL APPROX. 10" AFT OF RUDDER POSITION INDICATOR IAW A321 SRM 53-51-11-300-002. REPAIR IS CAT "A". (LP# 2269258) - [SDR DALA2022040402248](https://openairdocs.org/sdr/DALA2022040402248.md): None · none · Apr 1, 2022 · N385DZ · Airbus A321211 · Brake Anti-Skid Section > SHIP 3085 - ATO - AT 80 KNOTS DUE TO A BRAKES RELEASED ECAM MESSAGE. SYSTEM FAULTED THE #4 WHEEL TACH. CORRECTIVE ACTION: REPLACED #4 WHEEL TACHOMETER. OPS CHECK GOOD. NO FAULTS. (8499288) - [SDR DALA2021071503999](https://openairdocs.org/sdr/DALA2021071503999.md): Wire · pulled · Jul 14, 2021 · N385DZ · Airbus A321211 · Light System Wiring > EMERGENCY LIGHTS FAULT EPSU MID L. FOUND WIRES FOR EMERGENCY LIGHTS AT SEAT 17ABC PULLED OUT, SECURED WIRES AND REPLACED ESPU AT 12AABC CEILING AREA (15WL), CKS GOOD PER AMM 33-51-38. (LP# 7756758) - [SDR DALA2021061403221](https://openairdocs.org/sdr/DALA2021061403221.md): Wire · detached · Jun 10, 2021 · N385DZ · Airbus A321211 · Light System Wiring > DURING SVC CHECK, FOUND EMERGENCY LIGHT AT ROW 17ABC INOP. FWD TO MEL PER A321 MEL 33-50-03B. READ OUT ASSOCIATED WIRES FOUND NO VOLTS AT LIGHT CONNECTOR BUT GROUND IS OKAY REF. A321 AWM 33-51, MISSING 6VDC PWR AT LIGHT CONNECTOR, REQUIRES FURTHER T/S. RETURNE ## 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 = 'N385DZ' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N385DZ/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.