N318DU

Service difficulty reports · 16

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

Query with SQL
duckdb -csv -c "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 = 'N318DU' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR DALA2026082004765Skin · dentedDURING LAYOVER IN DFW, THE AIRCRAFT WAS FOUND WITH A DENT ON THE FUSELAGE SKIN FWD FUSELAGE LOWER SKIN BETWEEN FR24-26 AND BETWEEN STR22L-23L. TRIMMED OUT DAMAGED PORTION OF THE SKIN PER ASRP BD 500-J51-00-90-01AAA-018A-A. FABRICATED REPAIR DOUBLERS, FILLERS,Aug 20, 2026 · N318DU · Airbus BD5001A11 · Fuselage Main, Plate/SkinSDR DALA2026021901206Seat Track · corrodedFRONT SEAT TRACK NEAR FR 22 RBL 43.5 SHOWS SIGNS OF CORROSION. COMPLIED WITH ER/A 623174-14TR REV A SECTION I. (LP# 1448857)Feb 13, 2026 · N318DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026021901205Seat Track · corrodedFRONT SEAT TRACK NEAR FR 22 RBL 23 SHOWS SIGNS OF CORROSION. COMPLIED WITH ER/A 629030-14TR REV ORIGINAL SECTION I. (LP# 1448856)Feb 13, 2026 · N318DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026021100995Seat Track · corrodedAFT SEAT TRACK NEAR FR 74 LBL 43.5 SHOWS SIGNS OF CORROSION. REPAIRED PER ER/A 623167-14TR, REV ORIGINAL. (LP# 1442279)Feb 8, 2026 · N318DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026021100994Seat Track · corrodedAFT SEAT TRACK NEAR FR 74 RBL 23 SHOWS SIGNS OF CORROSION. " COMPLIED WITH A220 AMM 51-21-11 AND ERA 623169-14TR REV ORIGINAL. (LP# 1442029)Feb 8, 2026 · N318DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026021100993Seat Track · corrodedAFT SEAT TRACK NEAR FR 74 LBL 23 SHOWS SIGNS OF CORROSION. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0004:2500-2647/114 00148 COMPLIED WITH ER/A 623167-14TR REV ORIGINAL. (LP# 1442020)Feb 8, 2026 · N318DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026021100992Seat Track · corrodedAFT SEAT TRACK NEAR FR 74 RBL 43.5 SHOWS SIGNS OF CORROSION. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0004:2500-2647/112 00146 COMPLIED WITH ER/A 623170-14TR REV ORIGINAL. (LP# 1442019)Feb 8, 2026 · N318DU · Airbus BD5001A11 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025122609410Unknown · odorDIVERTED TO LAX DUE TO DIRTY SOCK ODOR/SMELL WITH A DECLARED EMERGENCY. COMPLIED WITH ENGINE WATER WASH AND BOROSCOPED. DEFERRED PER MEL 36-12-00A. REPLACED NBR 2 ENGINE AND RE-ACTIVATED NBR 2 ENGINE BLEED. (LP 7698526, 7654273, 1386817)Dec 24, 2025 · N318DU · Airbus BD5001A11 · Air Distribution SystemSDR DALA2025021001039Slat Track · corrodedLH SLAT TRACK NBR 4 RACK TEETH (2EA) HA EVIDENCE OF CORROSION REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W PRI 624072-14AD TO STEP 6. T. FREE 1643853. PERFORMED EDDY CURRENT INSPECTION PER ER/A 624072-14AD PRI REVFeb 4, 2025 · N318DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2025021001038Slat Track · corrodedLH SLAT TRACK NBR 9 PINION TEETH (1EA) HAS EVIDENCE OF CORROSION REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W PRI 624072-14AD TO STEP 6. T. FREE 1643853. PERFORMED EDDY CURRENT INSPECTION PER ERA624072-14AD PRI REFeb 4, 2025 · N318DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2025021001037Slat Track · corrodedRH SLAT TRACK NBR 4 RACK TEETH (2EA) HAS EVIDENCE OF CORROSION REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W PRI 624075-14AD TO STEP 6. T. FREE 1643853 PERFORMED EDDY CURRENT INSPECTION PER ERA 624075-14AD PRI REV Feb 4, 2025 · N318DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2025021001036Slat Track · corrodedRH SLAT TRACK NBR 4 PINION TEETH (2EA) HAS EVIDENCE OF CORROSION REF 5742-01028-02B. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W PRI 624075-14AD TO STEP 6. T. FREE 1643853. PERFORMED EDDY CURRENT INSPECTION PER ERA 624075-14AD PRI RFeb 4, 2025 · N318DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2025021001035Slat Track · corrodedLH SLAT TRACK NBR 9 RACK TEETH (2EA) HAS EVIDENCE OF CORROSION REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W PRI 624072-14AD TO STEP 6. T. FREE 1643853. PERFORMED EDDY CURRENT INSPECTION PER ERA 624072-14AD PRI REVFeb 4, 2025 · N318DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2025021001034Slat Track · corrodedLH SLAT TRACK NBR 4 PINION TEETH (2EA) HAS EVIDENCE OF CORROSION REF 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED BEFORE FURTHER FLIGHT. C/W PRI 624072-14AD TO STEP 6. T FREE 1643853. PERFORMED EDDY CURRENT INSPECTION PER ERA 624072-14AD PRI REFeb 4, 2025 · N318DU · Airbus BD5001A11 · Leading Edge DevicesSDR DALA2024090908865Engine · odorMUSTY SOCK ODOR DURING APPLICATION OF T/O POWER AND DURING FINAL DESCENT. C/W A220 JIC 0550-2001. IDENTIFIED RIGHT ENGINE AS CAUSE. C/W JIC 6001. PLACED ENGINE BLEED SYSTEM ON MEL REF LOG 6161239. ENGINE PLACED ON MONITOR. C/W JIC 0550-2003 ECS DECONTAMINATIONSep 6, 2024 · N318DU · Airbus BD5001A11 · Engine (Turbine/Turboprop)SDR DALA2023091407571Unknown · unknownELECTRICAL BURNING SMELL ON TAXI IN WHEN BLEEDS SWITCHED TO APU. AFT FA ALSO STRONGLY SMELLED IT. C/W ODI PREVENTION TASKS. C/W WORK CARD 0550-2001, 0550-6001 AND 0550-2002. NO SMOKE, ABNORMAL SMELLS OR FUMES NOTED. A/C OK FOR SERVICE. (LP# 8786312)Sep 14, 2023 · N318DU · Bombdr BD1001A10 · Air Conditioning System
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