N343NB

Service difficulty reports · 223

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 = 'N343NB' 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 DALA13063283143Floor Panel · delaminatedCENTER CABIN FLOOR PANEL 252GF DELAMINATED, FOUND OUT OF LIMITS IAW SRM 53-12-00 DIAGRAM 102. FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.Nov 20, 2013 · N343NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13062653143Fitting · corrodedAFT UTILITY AREA LT AFT DOOR CUT-OUT AT FRAME 68 LOWER CORNER CORRODED. REMOVED CORROSION IAW SRM 51-74-00, FOUND TO BE NO LIMITS ESTABLISHED FOR SRM. LOCATED AND DRILLED NEW CORNER FITTING IAW SRM 51-44-00. INSTALLED NEW CORNER FITTING ACCOMPLISHED ON NONNov 19, 2013 · N343NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13062643143Floor Support · corrodedFORWARD UTILITY AREA FLOOR SUPPORT Y765 FRAMES 14-21 UPPER SURFACE FLANGE CORRODED. REMOVED CORROSION IAW SRM 51-74-00, FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14 FIG 102. REMOVED DAMAGED FLOOR SUPPORT IAW SRM 51-42-11. INSTALLED NEW FLOOR SUPPORT IAW TRM Nov 19, 2013 · N343NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13062633143Skin · corrodedAFT UTILITY AREA LT AFT DOOR CUT-OUT AT FRAME 68 LOWER CORNER CORRODED. REMOVED CORROSION IAW SRM 51-74-00, FOUND TO BE NO LIMITS ESTABLISHED FOR SRM. LOCATED AND DRILLED NEW CORNER FITTING IAW SRM 51-44-00. INSTALLED NEW CORNER FITTING ACCOMPLISHED ON NONNov 19, 2013 · N343NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA13062223143Web · corrodedFORWARD CABIN STRINGER 23R FRAMES 20-21 UPPER SURFACE WEB HAS CORRODED. BLENDED AREA IAW SRM 51-74-00. REMOVED & REPLACED WEB IAW SRM 51-42-11 & DWG D53118159.Nov 17, 2013 · N343NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13062213143Shear Plate · corrodedAFT UTILITY AREA RT SHEAR PLATE CORRODED. REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-42-11 & DWG D53474180.Nov 17, 2013 · N343NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13062203143Shear Plate · corrodedAFT UTILITY AREA LT SHEAR PLATE CORRODED. REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-42-11 & DWG D53474180.Nov 17, 2013 · N343NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13062163143Seat Track · corrodedFORWARD UTILITY AREA SEAT TRACK -Y1292 BTW FRAMES 18 - 22 UPPER SURFACE FLANGE HAS SCRIBE LINE & CORROSION ON CROWN. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-15 FIG. 101. REMOVED AND REPLACED SEAT TRACK IAW TRM 53-21-01.Nov 16, 2013 · N343NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA13062153143Floor Support · corrodedFORWARD UTILITY AREA FLOOR SUPPORT Y1292 BETWEEN FRAMES 14 - 22 UPPER SURFACE FLANGE CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-15 FIG.101. REMOVED AND REPLACED FLOOR SUPPORT IAW TRM 53-21-01.Nov 16, 2013 · N343NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13062143143Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT Y765 AROUND THE HOLE AT FRAME 66 CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. REMOVED AND REPLACED FLOOR SUPPORT IAW TRM 53-21-01.Nov 16, 2013 · N343NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13062133143Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT Y765 AT FRAME 68 CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. REMOVED AND REPLACED FLOOR SUPPORT IAW TRM 53-21-01.Nov 16, 2013 · N343NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13062113143Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT Y254 AT FRAME 68 CORRODED. BLENDED AREA IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-14 FIG 102. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-11 AND TRM 53-21-01.Nov 16, 2013 · N343NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13062103143Floor Panel · corrodedAFT UTILITY FLOOR PANEL 261FF CORRODED. REPLACED FLOOR PANEL IAW SRM 51-72-11.Nov 16, 2013 · N343NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13062093143Floor Panel · corrodedAFT UTILITY FLOOR PANEL 262FF CORRODED, NO ALLOWABLE LIMIT ON SRM. REPLACED FLOOR PANEL IAW SRM 51-72-11.Nov 16, 2013 · N343NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13062083143Floor Panel · corrodedFORWARD UTILITY FLOOR PANEL 222FF CORRODED, NO ALLOWABLE LIMITS IN SRM. REPLACED FLOOR PANEL IAW 51-72-11.Nov 16, 2013 · N343NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13062073143Floor Panel · corrodedFORWARD UTILITY FLOOR PANEL 221FF CORRODED, NO ALLOWABLE LIMITS IN SRM. REPLACED FLOOR PANEL IAW SRM 51-72-11.Nov 16, 2013 · N343NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13062043143Floor Support · corrodedFORWARD UTILITY AREA FLOOR SUPPORT Y254 BETWEEN FRAMES 16 - 20 UPPER SURFACE FLANGE CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14, FIG. 107. REMOVED & REPLACED FLOOR SUPPORT IAW TRM 53-21-01.Nov 15, 2013 · N343NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13062033143Floor Support · corrodedFORWARD UTILITY AREA FLOOR SUPPORT Y503.2 BETWEEN FRAMES 12 - 16 UPPER SURFACE FLANGE CORRODED. REMOVED CORROSION IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-11-14 FIG 107. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-11 AND TRM 53-21-01.Nov 15, 2013 · N343NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13060883143Floor Support · corrodedFORWARD CABIN FLOOR SUPPORT -Y189 FRAMES 20 - 24 UPPER FLANGE CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14 FIG.105. REMOVED & REPLACED FLOOR SUPPORT IAW SRM 51-42-11 & TRM 53-21-01.Nov 14, 2013 · N343NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13034813143Floor Panel · damagedRAMP CREW REPORTED .7500 " HOLE IN AFT BAG BIN FLOOR. HOLE IS 3.5 FT INSIDE OF AFT FRAME OF AFT BAG BIN DOOR. INSTALLED TEMP REPAIR IAW SRM 53-02-00.Jul 10, 2013 · N343NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13002243143Battery · inoperativeEPSU BATTERY RT MESSAGE DURING EMERGENCY LIGHT TEST. REPLACED RT EPSU BATTERY IAW AMM 33-51-38. OPS CHECKED GOOD.Jan 14, 2013 · N343NB · Airbus A319114 · Emergency LightingSDR DALA1169173143Epsu · faultyDURING EMERGENCY LIGHT TEST, FORWARD LEFT EPSU FAULTED ON CIDS. REMOVED AND REPLACED FORWARD LEFT EPSU PER AMM. OPERATIONAL CHECK WAS NORMAL. AIRCRAFT OK FOR SERVICE.Dec 10, 2011 · N343NB · Airbus A319114 · Emergency LightingSDR NWAA091373143Skin · damagedDURING GROUND OPERATIONS FORWARD FUSELAGE NOSE SKIN WAS DAMAGED BETWEEN FRAME 1-4 AND BETWEEN LAP SKIN S39L AND S41L-S41R. REPAIRED PER EA 31-215413 REV B OF EA 31-215413 REQUIRES A FATIGUE AND DAMAGE TOLERANCE APPROVAL FOR CONTINUED REVENUE FLIGHT BEYOND 10 Apr 10, 2009 · N343NB · Airbus A319114 · Fuselage Main, Plate/Skin
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