N120DU

Service difficulty reports · 62

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 = 'N120DU' 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 DALA2024022302542Engine · vibrationSHIP 8120 -DIV- TO DTW DUE TO #1 ENGINE N2 VIBRATION INDICATION. THROTTLE WAS REDUCED TO STOP VIBRATION INDICATION, VIBE CAUTION MESSAGE REOCCURRED EACH TIME THROTTLE ADVANCED. CORRECTIVE ACTION: #1 ENGINE REPLACED. (LP# 0209612, 4898355, 0209953) PW1521G3Feb 20, 2024 · N120DU · Airbus BD5001A10 · Engine (Turbine/Turboprop)SDR DALA2024012200944None · noneACCOMPLISH ER/A 610713-14 PRI REV 0 AND FINAL ER/A 610713-14 REV C. ACCOMPLISHED ER/A 610713-14 PRI REV 0 AND FINAL ER/A 610713-14 REV C. ASSOCIATED ER/A 14-610713 ADDED FOR AC 8120. (LP# 0156819)Jan 16, 2024 · N120DU · Airbus BD5001A10 · Standard Practices/StructuresSDR DALA2025011600376Skin · damagedERA 610713-14 REV C PERMANENT REPAIR HAS DTE DAMAGE TOLERANCE LI MIT. ERA 610713-14 REV C REQUIRES ENGINEERING REVISION TO OPERATE BEYOND 12 MONTHS FROM SECTION III REPAIR INSTALL. ASSOCIATED ER/A 00-610713 ADDED FOR AC 8120. PER ER/A 610713-14AD REV D, DTE STJan 15, 2024 · N120DU · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2024011800797Skin · dentedC/W RI 610713-14. / NOSE FUSELAGE / LHS SKIN / FR15 / DENT REPAIR. (LP# 2882837)Jul 24, 2023 · N120DU · Airbus BD5001A10 · Fuselage Main, Plate/SkinSDR DALA2023061304825Unknown · unknownRH MLG DOOR AFT STRIKER PLATE WORN THRU AND COMPOSITE IS DAMAGED UNDERNEATH. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 030-0001:5280-4019/001 00035 REPAIRED RH MLG FLYING DOOR PER ER/A 599219-14TR REV. A. (LP# 280778Jun 9, 2023 · N120DU · Airbus BD5001A10 · DoorsSDR DALA2022071904977Bracket · corrodedREF AMDS 5327-01014-01, AD 2021-13-20, LAV SERVICE ACCESS DOOR 146BR, BONDING WIRE BRACKET HAS CORROSION. REPAIR CORROSION PRIOR TO FURTHER FLIGHT. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 026-0001:5327-01014-01 /001 00089 REPLACED BONDING WIRE REF A220 AMP 5Jul 14, 2022 · N120DU · Airbus BD5001A10 · Fuselage Internal Mounting StructureSDR DALA2022070604698None · noneSHIP 8120 - DIV - TO MDT DUE TO DUAL EQUIPMENT BAY SMOKE DETECTOR FAILURE. CORRECTIVE ACTION: REPLACED BOTH SMOKE DETECTORS. (LP# 8822696)Jul 2, 2022 · N120DU · Airbus BD5001A10 · Smoke DetectionSDR DALA2022042803008Ecs · failedSHIP 8120 -ATB- DUE TO RIGHT BLEED FAIL. CORRECTIVE ACTION: REPLACED ECS HARNESS, AND INTEGRATED AIR SYSTEM CONTROLLER #2. (LP#8254172)Apr 18, 2022 · N120DU · Airbus BD5001A10 · Pneumatic Indicating SystemSDR DALA2022020800833None · noneSHIP 8120 - DIV TO DTW DUE TO LOSS OF BOTH E/E EQUIP BAY SMOKE DETECTORS, EQUIP BAY SMOKE FAIL INDICATED. NNP REQUIRES LAND NEAREST SUITABLE. CORRECTIVE ACTION: INSPECTED AIRFLOW TUBING, REPLACED BOTH DETECTORS AND FIDEX. AIRCRAFT RTS. (LP# 6172412)Feb 5, 2022 · N120DU · Airbus BD5001A10 · Smoke DetectionSDR DALA2020122104180Bottle · low pressureL1 DOOR EOAM IN YELLOW. DISARMED, SERVICED, AND REARMED L1 DOOR EOAM TO GREEN, PER A220 BD500-A-J52-11-08-01AAA-214A-A. NO LEAKS NOTED. OK FOR SERVICE. COMPLIED WITH DOOR ASSIST REARM RII INSP.Dec 19, 2020 · N120DU · Airbus BD5001A10 · Emergency EquipmentSDR DALA2020111403716Engine · unknownON 7 DAY ENGINE RUN, NR 2 ENGINE EGTR WENT TO 1006 WITH SMALL FLAMES OUT TAIL PIPE AND SLIGHT RUMBLE ON START UP. R & R NR 2 ENGINE EEC, REF A220 AMP 73-21. CHECKS GOOD 3 GOOD ENGINE STARTS. A/C OK FOR SERVICE. CONTROL, ELECTR OFF 81-7321-9-0019 S/N 05967.Nov 12, 2020 · N120DU · Airbus BD5001A10 · Engine (Turbine/Turboprop)SDR DALA2020101903386Seal · leakingSTRONG SMOKE SMELL AFTER ROTATION. PERFORMED PERTINENT PORTION OF THE SMOKE/FIRE/FUMES QRH. AIR RETURN TO DTW. SMOKE/FUMES QUESTIONNAIRE COMPLETED.REPLACED IPC 1 CEM PER A220 AMP 21-42-03. OPS TEST OK. REPLACED CEM AS PRECAUTIONARY MEASURE. PERFORMED W/C 0550-Oct 17, 2020 · N120DU · Airbus BD5001A10 · AC Generator-Alternator
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