N340NB

Service difficulty reports · 211

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 = 'N340NB' 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 DALA13041973140Support · crackedAFT UTILITY AREA LT SIDE STRINGER 23L BETWEEN FRAMES 68-69 SUPPORT PLATE CRACKED. R & R SUPPORT PLATE IAW DWG D53480019 AND SRM 51-42-11. CRACKED DIMENSION L=5.0".Aug 28, 2013 · N340NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13041943140Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT BETWEEN FRAMES 64-66 UPPER SURFACE FLANGES AND HARD POINT HOLES Y-765 HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. R & R FLOOR SUPPORT IAW TRM 53-21-01.Aug 27, 2013 · N340NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13041933140Structure · corrodedFORWARD UTILITY AREA BETWEEN FRAMES 12-14, Y-81, UPPER SURFACE FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. R & R FLANGE JOINT COVER IAW SRM 51-42-11 & DWG D53112829.Aug 27, 2013 · N340NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13041443140Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT BETWEEN FRAMES 66 & 68 UPPER SURFACE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00, FOUND OUT OF LIMITS IAW TRM 53-41-15. R & R FLOOR SUPPORT IAW SRM 51-42-11 AND TRM 53-21-01.Aug 26, 2013 · N340NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13041433140Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT BETWEEN FRAMES 66-70, Y-765 CORRODED. BLENDED AREA IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. R & R FLOOR SUPPORT IAW TRM 53-21-01.Aug 26, 2013 · N340NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13041393140Web · corrodedFORWARD UTILITY AREA, RT SIDE STRINGER 23R BETWEEN FRAMES 20-21 UPPER SURFACE WEB HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. NO ESTABLISHED LIMITS IN SRM. R & R WEB IAW SRM 51-42-11 AND DWG D53112570.Aug 24, 2013 · N340NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13041323140Floor Support · corrodedFWD UTILITY AREA FLOOR SUPPORT BETWEEN FR16-FR21, Y254 UPPER FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14. R & R FLOOR SUPPORT IAW SRM 51-42-11 AND TRM 53-21-01.Aug 23, 2013 · N340NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13041313140Floor Support · corrodedFWD UTILITY AREA FLOOR SUPPORT BETWEEN FR16-FR18, Y1292 UPPER SURFACE FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-11-15. R & R FLOOR SUPPORT IAW TRM 53-21-01.Aug 23, 2013 · N340NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12013093140Light · damagedEMERGENCY SEAT MOUNTED LIGHTING DAMAGED. WIRING EXPOSED, COVER MISSING INTERIOR. INSTALLED COVER AT SEAT 01 B. OPS CHECK NORMAL. ACFT OK FOR SERVICE.Nov 17, 2012 · N340NB · Airbus A319114 · Emergency LightingSDR DALA1110593140Connector · disconnectedDURING A NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT ROW 11 INOPERATIVE. MX RECONNECTED A CONNECTOR AND FUNCTIONAL CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.Feb 14, 2011 · N340NB · Airbus A319114 · Light System WiringSDR NWAA082993140Pump · failedIN FLIGHT GOT "HYD RSVR LO LEVER" ECAM. CONFIRMED YELLOW HYDRAULIC LEVEL AT ZERO. COMPLIED WITH ECAM & COM PROCEDURES. LANDED AND TAXIED AND UNEVENTFULLY. REPLACED NR 2 ENGINE DRIVEN HYDRAULIC PUMP. CHECKS GOOD. (A)Jul 5, 2008 · N340NB · Airbus A319114 · Hydraulic Pump (Electric/Engine), Main
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