# Service difficulty reports: N145DQ

A list on [N145DQ](https://openairdocs.org/aircraft/N145DQ.md).

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

- [SDR DALA2025102007622](https://openairdocs.org/sdr/DALA2025102007622.md): Door Sill · no discrepancy · Oct 15, 2025 · N145DQ · Airbus BD5001A10 · Fuselage Main, Structure
  > ERA 622251-14 REV A HAS FOLLOW-ON INSPECTION FOR THE FORWARD CARGO DOOR SILL AREA. ACCOMPLISH SECTION II WITHIN 32,191 FC OR 57,868 FH. THEN EVERY 9,400 FC OR 16,450 FH THEREAFTER. ASSOCIATED ER/A 00-622251 ADDED FOR AC 8145. (LP# 1253822)
- [SDR DALA2024111510976](https://openairdocs.org/sdr/DALA2024111510976.md): Door Frame · corroded · Nov 13, 2024 · N145DQ · Airbus BD5001A10 · Fuselage Main, Structure
  > FWD CARGO DOOR, LOWER DOOR OPENING STRUCTURE - - FASTENER HOLE ( AFT CORNER) IN THE DOOR JAMB HAS CORROSION ON FACE. -M-. REF. SSI 53-21-25-04. NO PRESENCE OF BLUE PAINT OF INK INDICATING PREVIOUS REWORK. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE
- [SDR DALA2024111110819](https://openairdocs.org/sdr/DALA2024111110819.md): Waste Box · corroded · Nov 10, 2024 · N145DQ · Airbus BD5001A10 · Fuselage Main, Structure
  > CORROSION ON AFT I/B SIDE OF LAV WASTE BOX. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0255:2021-2025/001 00110 REPAIRED PER PRI 621946-14 REV 0,REV 1 AND REV 2 AND ER/A 621946-14 REV ORIGINAL SECTION I. PART REPL
- [SDR DALA2024082908529](https://openairdocs.org/sdr/DALA2024082908529.md): Slat Track · corroded · Aug 26, 2024 · N145DQ · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 RACK TEETH (2EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. PERFORMED TIME-LIMITED REPAIR PER ER/A 620078-14AD REV A, SECTION IV AND PRI 6200787-14AD
- [SDR DALA2024082908528](https://openairdocs.org/sdr/DALA2024082908528.md): Slat Track · corroded · Aug 26, 2024 · N145DQ · Airbus BD5001A10 · Leading Edge Devices
  > RH SLAT TRACK NBR 4 PINION TEETH (2EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. PERFORMED TIME-LIMITED REPAIR PER ER/A 620078-14AD REV A, SECTION IV AND PRI 620078-14A
- [SDR DALA2024082908527](https://openairdocs.org/sdr/DALA2024082908527.md): Slat Track · corroded · Aug 26, 2024 · N145DQ · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 4 PINION TEETH (2EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W ER/A 620064-14AD REV A, SECTION IV TIME-LIMITED REPAIR AND PRI 620064-14AD REV 0. (
- [SDR DALA2024082908526](https://openairdocs.org/sdr/DALA2024082908526.md): Slat Track · corroded · Aug 26, 2024 · N145DQ · Airbus BD5001A10 · Leading Edge Devices
  > LH SLAT TRACK NBR 4 RACK TEETH (2EA) HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W ER/A 620064-14AD REV A, SECTION IV TIME-LIMITED REPAIR AND PRI 620064-14AD REV 0. (LP
- [SDR DALA2024082908525](https://openairdocs.org/sdr/DALA2024082908525.md): Slat Track · corroded · Aug 26, 2024 · N145DQ · Airbus BD5001A10 · Leading Edge Devices
  > RT WING SLAT TRACK #2 UPPER SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK REF. 5742-01028-02B. REMOVED LIGHT CORROSION PER BD500-A-J51-21-06-03AAA-258A-A NEED NDT VERIFICATION FOR NO CRACKS O. HERNANDEZ 2217529 NO CRACKS NOTED REF A220 ANDTP 51-01-20.
- [SDR DALA2024052105387](https://openairdocs.org/sdr/DALA2024052105387.md): Light · inoperative · May 15, 2024 · N145DQ · Airbus BD5001A10 · Emergency Lighting
  > AFT RIGHT OVER WING LIGHT INOP. R/R AFT RIGHT OWEED LIGHT IAW A220 AMP 33-55. OPS CHECKS NORMAL. (LP# 5641955)
- [SDR DALA2024020701633](https://openairdocs.org/sdr/DALA2024020701633.md): Slat Track · corroded · Feb 2, 2024 · N145DQ · Bombdr BD1001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 6 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND NO PREVIOUS REWORK REF 5742-01028-02B. REPAIRED R/H SLAT TRACK NBR 6 UPPER AFT SURFACE IAW PRI 610899- 14AD REV 0 AND ERA REV B MATCHED. (LP# 0184544)
- [SDR DALA2024020701632](https://openairdocs.org/sdr/DALA2024020701632.md): Slat Track · corroded · Feb 2, 2024 · N145DQ · Bombdr BD1001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 5 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND NO PREVIOUS REWORK REF 5742-01028-02B. REPAIRED R/H SLAT TRACK NBR 5 UPPER AFT SURFACE IAW PRI 610899- 14AD REV 0 AND ERA REV B MATCHED. (LP# 0184532)
- [SDR DALA2024020701631](https://openairdocs.org/sdr/DALA2024020701631.md): Slat Track · corroded · Feb 2, 2024 · N145DQ · Bombdr BD1001A10 · Leading Edge Devices
  > R/H SLAT TRACK NBR 2 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND NO PREVIOUS REWORK REF 5742-01028-02B. REPAIRED R/H SLAT TRACK NBR 2 UPPER AFT SURFACE IAW PRI 610899- 14AD REV 0 AND ERA REV B MATCHED. (LP# 0184525)
- [SDR DALA2024020701630](https://openairdocs.org/sdr/DALA2024020701630.md): Slat Track · corroded · Feb 2, 2024 · N145DQ · Bombdr BD1001A10 · Leading Edge Devices
  > L/H SLAT TRACK NBR 4 UPPER AFT INBOARD SIDE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK. REF. 5742-01028-02A. MEASURED L/H SLAT TRACK NBR 4 UPPER AFT INBOARD SIDE IAW PRI 610903-14AD REV 0 AND ERA REV A MATCHED.
- [SDR DALA2024020701629](https://openairdocs.org/sdr/DALA2024020701629.md): Slat Track · corroded · Feb 2, 2024 · N145DQ · Bombdr BD1001A10 · Leading Edge Devices
  > L/H SLAT TRACK NBR 4 LOWER FORWARD OUTBOARD SURFACE HAS EVIDENCE OF WEAR AND PREVIOUS REWORK. REF. 5742-01028-02A. MEASURED L/H SLAT TRACK NBR 4 LOWER FORWARD OUTBOARD SIDE IAW PRI 610903-14AD REV 0 AND ERA REV A MATCHED. ASSOCIATED AA 5742-01028.
- [SDR DALA2024020701628](https://openairdocs.org/sdr/DALA2024020701628.md): Slat Track · corroded · Feb 2, 2024 · N145DQ · Bombdr BD1001A10 · Leading Edge Devices
  > L/H SLAT TRACK NBR 5 UPPER AFT SURFACE HAS EVIDENCE OF CORROSION AND PREVIOUS REWORK. REF. 5742-01028-02A. REPAIRED L/H SLAT TRACK NBR 5 UPPER AFT SURFACE IAW PRI 610903- 14AD REV 0 AND ERA REV A MATCHED.
- [SDR DALA2023122910727](https://openairdocs.org/sdr/DALA2023122910727.md): Unknown · unknown · Dec 28, 2023 · N145DQ · Bombdr BD1001A10 · Turbine Engine Oil System
  > SHIP 8145 -IFSD/ATB- RETURNED TO RDU DUE TO LOSS OF OIL QUANTITY AND PRESSURE DROPPING. PER QRH CREW SHUT DOWN RIGHT ENGINE AT 9 QTS INDICATION AND LOSING OIL PRESSURE. MAINTAINED POSITIVE OIL PRESSURE DURING WINDMILLING. CORRECTIVE ACTION: FOUND EXTERNAL OIL
- [SDR DALA2023103008885](https://openairdocs.org/sdr/DALA2023103008885.md): Unknown · unknown · Oct 16, 2023 · N145DQ · Bombdr BD1001A10 · Air Distribution System
  > ON CLIMBOUT A STRONG DIRTY MUSTY SMELL WAS DETECTED IN FLIGHT DECK FROM LIFTOFF THROUGH FL180 WHERE SMELL SUBSIDED AND THEN DISSIPATED ONCE CRZ. FAS DID NOT NOTICE SMELL IN CABIN. SMELL RETURNED 16-8K IN IMC WITH CAI & WAI ON. PERFORMED HIGH POWER RUN PER A220
- [SDR DALA2023092607922](https://openairdocs.org/sdr/DALA2023092607922.md): Unknown · unknown · Sep 23, 2023 · N145DQ · Bombdr BD1001A10 · Air Distribution System
  > STRONG SOCK/MOLDY CHEESE ODOR DURING LANDING AND TAXI, WENT AWAY ONCE APU WAS PROVIDING BLEED AIR TO THE PACKS. PERFORMED ENGINE WATER WASH WORK CARD 7200-9001-02. RAN R ENG FOR 10 MIN AT 70% POWER, REMOVED BORE PLUGS HP1, 2, 3 + LP1 REF A220 AMP 72-00. BORESC
- [SDR DALA2023073106174](https://openairdocs.org/sdr/DALA2023073106174.md): Unknown · unknown · Jul 26, 2023 · N145DQ · Bombdr BD1001A10 · Fire Protection System
  > SHIP 8145 - DIV - TO BOI DUE TO "EQUIP BAY SMK FAIL" CAUTION MESSAGE. CORRECTIVE ACTION: REPLACED BOTH EQUIPMENT BAY SMOKE DETECTORS AND THE FIRE DETECTION AND EXTINGUISHING (FIDEX) CONTROL UNIT. (LP# 4662602)
- [SDR DALA2023063005244](https://openairdocs.org/sdr/DALA2023063005244.md): Unknown · unknown · Jun 29, 2023 · N145DQ · Bombdr BD1001A10 · Central Display
  > SHIP 8145 - ATB - DUE TO "CAS MISCOMPARE" ADVISORY MESSAGE WITH MULTIPLE ASSOCIATED FAULTS. CORRECTIVE ACTION: REPLACED DATA CONCENTRATOR MODULE (DCM) CARD 1A. (9649706, 9649707)

## 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 = 'N145DQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N145DQ/reports

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