N320NB

Service difficulty reports · 221

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 = 'N320NB' 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 DALA1218923120Floor Panel · corrodedFLOOR PANEL 261FF HAS CORRODED ON LOWER SURF. NO ALLOWABLE DAMAGE PER A319 SRM 53-12-00 FOR PANEL 261FF. DAMAGE AREA L=6" X W=3" X D=100%. REPLACED PANEL IAW A319 SRM 51-72-11.Mar 22, 2012 · N320NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1218913120Floor Panel · corrodedFLOOR PANEL 262FF HAS CORRODED ON LOWER SURF. NO ALLOWABLE DAMAGE PER A319 SRM 53-12-00 FOR PANEL 262FF. DAMAGE AREA L=2.5" X W=6" X D=100%. REPLACED PANEL IAW A319 SRM 51-72-11. RETAIN FOR RECORDS.Mar 22, 2012 · N320NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1218903120Floor Support · corrodedFORWARD MAIN CABIN FLOOR SUPPORT BEAM AT FR20 -Y254 HAS CORROSION. SSI 531189. N/R 220/21. REMOVED CORROSION IAW A319 SRM 51-74-00. ORIGINAL MATERIAL THICKNESS 079" AFTER REWORK L=2.0" W=.9" D=.029" FOUND TO BE OUT OF LIMIT IAW A319 SRM 53-00-14 FIG 102. RMar 22, 2012 · N320NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1218893120Floor Panel · damagedFWD CABIN FLOOR PNL 222CF HAS A DAMAGED CORNER N/R 230/36. REPLACED FWD CABIN FLOOR PANEL 222CF WITH NEW FLOOR PANEL IAW A319 SRM 51-72-11. TO BE INSTALLED ON WORKCARD 2500-6617. DAMAGE DIM: L=2.0" W=1.5".Mar 22, 2012 · N320NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1218383120Trunnion · gougedLT WING INBD FLAP TRUNNION LOWER AFT SECTION GOUGED. N/R 560/11. REPLACED LT WING INBD FLAP TORSION SUPPORT ASSY IAW A319 CMM 57-52-21 WAS FOUND TO BE OUT OF PER CMM 57-52-21. DAMAGE DIM: L=1.2" W=0.980" D=0.150". RETAIN FOR RECORDS.Mar 21, 2012 · N320NB · Airbus A319114 · Trailing Edge FlapsSDR DALA1218353120Sill · corrodedAFT CABIN L2 DOOR SILL AT FR 68 CORRODED. REMOVED CORROSION IAW A319 SRM 51-74-00 L=4.00 W=2.0 D=.045 ORIG MAT. 0.063. FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-41-14 FIG 101. REMOVED L2 DOOR SILL IAW A319 SRM 51-42-11. LOCATED AND DRILLED NEW DOOR SILL IAMar 21, 2012 · N320NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1217753120Sill · corrodedAFT CABIN L2 DOOR SILL, AREA COVERED BY FWD GIRT BAR FITTING (AFT OF FR 66) AROUND FASTENER HOLES HAS CORROSION. SSI 534147. N/R 260/44. REMOVED CORROSION IAW A319 SRM 51-74-00 CHECK LIMIT L=2- W=1- D=.060-. FOUND OUT OF LIMIT IAW A319 SRM 53-41-14 FIG 101. Mar 21, 2012 · N320NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1217203120Fitting · corrodedAFT CABIN L2 DOOR SILL, AFT CORNER FITTING CORRODED. REMOVED CORROSION IAW A319 SRM 51-74-00. L=1.3 W=.700 D=.020 ORG MAT 0.080 NO SRM NOTED FOR ALLOWABLE DAMAGE LIMITS. AFT CORNER FITTING WAS REMOVED ON N/R 260/41. INSTALLED NEW CORNER FITTING IAW A319 SRMMar 18, 2012 · N320NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1217193120Floor Support · corrodedFORWARD MAIN CABIN FLOOR SUPPORT BEAM AT FR16 +Y254 HAS CORROSION. REMOVED CORROSION IAW A319 SRM 51-74-00. MEASUREMENTS ARE AS FOLLOWS L=1.5 W=1.2 D=.035 MAX MATERIAL LOSS ALLOWED IS .031. FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-11-14 FIG 105. REMOVED FMar 18, 2012 · N320NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1217183120Sill · corrodedAFT CABIN R2 DOOR SILL, AFT SHAPE SILL CORRODED. BLENDED CORRODED AREA IAW A319 SRM 51-74-00 DIM OF REWORKED AREA L=1.8" W=1.0" D=0.042. NO ALLOWABLE DAMAGE FOUND. REMOVED AND REPLACED CORNER FITTING IAW A319 SRM 51-42-11.Mar 18, 2012 · N320NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1217163120Floor Panel · corrodedFORWARD ENTRY WAY FLOOR PANEL 222FF HAS CORROSION ON UNDER SIDE OF PANEL. REPLACED FLOOR PANEL 222FF IAW A319 SRM 51-72-00.Mar 17, 2012 · N320NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1217093120Floor Panel · delaminatedCABIN FLOOR PANEL 231 KF IS DELAMINATED APR 4"X16". FABRICATED NEW FLOOR PANEL 231 KF IAW DRAWING 3D25-40640.Mar 17, 2012 · N320NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1217083120Floor Panel · corrodedFWD ENTRY WAY FLOOR PANEL 221 FF HAS CORROSION. REPLACED FLOOR PANEL 221FF IAW A319 SRM 51-72-00.Mar 17, 2012 · N320NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1217073120Floor Support · corrodedAFT CABIN FLOOR SUPPORT +Y765 BET FR66 TO FR68 CORRODED. SSI 534147. REMOVED AND REPLACED FLOORBEAM. FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-00-14 L=3.00 W=1.00 D=0.125 ORIG MAT. THICKNESS .125. INSTALLED FLOOR SUPPORT IAW A319 SRM 51-42-11. TOP COATED Mar 15, 2012 · N320NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1215873120Dummy Rail · corrodedFWD MAIN CABIN FLOOR SUPPORT DUMMY BEAM AT FR16+Y503 HAS CORRISION. SSI 531189. REMOVED CORROSION IAW A319 SRM 51-74-00. CHECK LIMIT L=3.3 W=1.8 IN. D=.028 IN. FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-11-14 FIG 106. REMOVED AND REPLACED FWD MAIN CABIN FMar 13, 2012 · N320NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1140243120Epsu · failedDURING A NON ROUTINE CHECK, FOUND THE EMERGENCY LIGHT TEST OF THE ESPU INTERNAL FWD LEFT FAILED. MAINTENANCE REPLACED 10WL FWD ESPU AND FUNCTIONAL TEST WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.Jun 19, 2011 · N320NB · Airbus A319114 · Emergency LightingSDR DALA1118893120Wire · damagedDURING A NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT SEAT 13C AND 17C INOPERATIVE. MAINTENANCE REPAIRED WIRE AT SEAT AND PERFORMED FUNCTIONAL CHECK. CHECK WAS NORMAL. A/C RETURNED TO SERVICE.Mar 15, 2011 · N320NB · Airbus A319114 · Light System WiringSDR DALA1118883120Wire · brokenDURING A NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT SEAT 3B INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT SEAT 3B AND PERFORMED FUNCTIONAL CHECK. CHECK WAS NORMAL. A/C RETURNED TO SERVICE.Mar 15, 2011 · N320NB · Airbus A319114 · Light System WiringSDR DALA1032983120Power Supply · inoperativeDURING A NON ROUTINE CHECK, FOUND EPSU AT 10WL FAULTED ON LOAD TEST. MAINTENANCE REPLACED POWER SUPPLY AND FUNCTIONAL TEST WAS NORMAL. A/C RETURNED TO SERVICE. (2010-00870)Nov 21, 2010 · N320NB · Airbus A319114 · Emergency LightingSDR DALA1026593120Light · inoperativeDURING A NON-ROUTINE CHECK, FOUND 1B EMERGENCY LIGHT INOPERATIVE. MAINT REPLACED 2 EMERGENCY LIGHT ASSY AND FUNCTIONAL CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.Oct 13, 2010 · N320NB · Airbus A319114 · Emergency LightingSDR 0602523120Power Supply · no testFORWARD EMERGENCY LIGHT POWER SUPPLY FAILS TEST. CORRECTED BY REPLACING FORWARD EPSU, CHECKS OK.Nov 27, 2006 · N320NB · Airbus A319114 · Emergency Lighting
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