N330NB

Service difficulty reports · 183

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 = 'N330NB' 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 DALA12003503130Floor Panel · damagedDURING INSPECTION, FOUND FWD CARGO BAY FLOOR PANEL 132DF HAS 4 ELONGATED HOLES. FLOOR PANEL INSTALLED ON W/C 2500-5918. HOLES DIA. 0.250 INCH.Jul 5, 2012 · N330NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12003493130Floor Panel · corrodedDURING INSPECTION, FOUND FORWARD UTILITY AREA FLOOR SUPPORT BETWEEN FR 16 TO FR 20 RT -Y254 UPPER AND LOWER FLANGE SURFACE HAS CORROSION. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.Jul 5, 2012 · N330NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12003483130Floor Panel · corrodedDURING INSPECTION, FOUND FWD CABIN FLOOR PANEL 222FF IS CORRODED, 3 INCH BY 2 INCH AREA. FLOOR PANEL INSTALLED ON W/C 2500-6617.Jul 5, 2012 · N330NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12003473130Floor Support · corrodedDURING INSPECTION, FOUND FORWARD UTILITY AREA CABIN FLOOR SUPPORT BETWEEN FR 16 TO FR 21 LT Y254 UPPER FLANGE HAS CORROSION AND ONE HOLE HAS CRACKED. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.Jul 5, 2012 · N330NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12003463130Floor Support · corrodedDURING INSPECTION, FOUND AFT UTILITY AREA FLOOR SUPPORT AT FR65 RT -Y765 UPPER SURFACE HARD POINT HOLE HAS CORROSION. BLENDED AREA IAW SRM 51-74-00, CHECK LIMITS ORIG. REPLACED WITH NEW FLOOR SUPPORT IAW SRM 51-42-11.Jul 3, 2012 · N330NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12003453130Floor Support · corrodedDURING INSPECTION, FOUND AFT CABIN FLOOR SUPPORT BETWEEN FR 66 TO FR 68 RT -Y765 UPPER FLANGE HAS CORROSION. BLENDED AREA IAW SRM 51-74-00, CHECK LIMITS ORIG. REPLACED WITH NEW FLOOR SUPPORT IAW SRM 51-42-11.Jul 3, 2012 · N330NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12003143130Support · corrodedAFT CABIN LT SIDE BETWEEN FR 69 TO FR 70 STRINGER 23L LOWER SURFACE FRAME SUPPORT HAS CORROSION. REMOVED 1 BRACKET FOR ACCESS IAW SRM 51-42-11. REMOVED FRAME SUPPORT AT FR 69 TO FR 70 IAW SRM 51-42-11. LOCATED AND DRILLED NEW SUPPORT IAW SRM 51-44-11. INSTJul 3, 2012 · N330NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12003133130Support · corrodedAFT UTILITY AREA RT BETWEEN FR 69 TO FR 70 STRINGER 23R UPPER SURFACE SUPPORT FRAME CORRODED. REMOVED AND REPLACED FRAME SUPPORT FR 69-70 STR 23R IAW SRM 51-42-11. REMOVED AND RE-INSTALLED 1 BRACKET FOR ACCESS IAW SRM 51-42-11. SANDED, CLEANED AND PAINTED EJul 3, 2012 · N330NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12003053130Floor Support · corrodedAFT CABIN FLOOR SUPPORT BETWEEN FR 68 TO FR 69 RT -Y1292 UPPER FLANGE CORRODED. BLENDED AREA IAW SRM 51-74-00. CHECK LIMITS ORIG MAT THICK .157 INCH. AFTER BLENDED MAT LOSS D=.075 INCH, L=2.100 INCH W=.200 INCH MAT REMAINING .082 INCH, FOUND TO BE OUT OF LIJul 2, 2012 · N330NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12003043130Floor Support · corrodedAFT CABIN FLOOR SUPPORT BETWEEN FR 66 TO FR 68 RT -Y1292 UPPER FLANGE CORRODED. BLENDED AREA IAW SRM 51-74-00. CHECK LIMITS ORIG MAT THICK .087 INCH. AFTER BLENDED MAT LOSS D=.085 INCH, L=6.200 INCH W=1.800 INCH MAT REMAINING .002 INCH. FOUND TO BE OUT OF LJul 2, 2012 · N330NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12003033130Floor Support · corrodedAFT CABIN FLOOR SUPPORT BTW FR65 RT -Y1292 UPPER FLANGE CORRODED. BLENDED AREA IAW SRM 51-74-00. CHECK LIMITS ORIG MAT THICK .087 INCH. AFTER BLENDED MAT LOSS D=.070 INCH, L=2.300 INCH W=.750 INCH. MATERIAL REMAINING .017 INCH FOUND TO BE OUT OF LIMITS IAWJul 2, 2012 · N330NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12003013130Blanking Plate · corrodedR1 DOOR AFT BLANKING PLATE CORRODED. REPLACED R1 DOOR AFT BLANKING PLATE IAW A319 SRM 51-72-00, NO ALLOWABLE LIMITS ESTABLISHED ON BLANKING PLATES L=1.5 W=1.5 D=0.080 IAW A319 SRM 53-12-00. INSTALLED ON W/C 2500-6601.Jul 2, 2012 · N330NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002733130Floor Support · corrodedFORWARD UTILITY AREA FLOOR SUPPORT BTW FWD FR 14 TO FR 16-Y81 UPPER SURFACE FLANGE AND UNDERNEATH RAIL HAS CORROSION. BLENDED DAMAGE AREA IAW SRM 51-74-00 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14 FIG 105. REMOVED AND REPLACED FLOOR SUPPORT JOINT COVER Jul 2, 2012 · N330NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12002903130Floor Support · corrodedFORWARD UTILITY AREA FLOOR SUPPORT BETWEEN FR 12 TO FR 16 LT Y503.2 UPPER FLANGE SURFACE HAS CORROSION. BLENDED AREA IAW SRM 51-74-00. CHECK LIMITS ORIG MAT .163 INCH L=3.05 INCH W=1.07 INCH D=.115 INCH MAT REMAINING .048 INCH TO BE OUT OF LIMITS IAW SRM 51Jul 1, 2012 · N330NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002893130Floor Support · corrodedAFT CABIN FLOOR SUPPORT BETWEEN FR 65 TO FR 66 RT -Y1732 UPPER FLANGE CORRODED. BLENDED AREA IAW SRM 53-00-14. CHECK LIMITS ORIG. MAT. .063 INCH AFTER BLENDED MAT. LOSS L=1.050 INCH W=1.010 INCH D=.025 INCH. MATERIAL REMAINING .038 INCH TO BE OUT OF LIMITSJul 1, 2012 · N330NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002833130Blanking Plate · corrodedDURING INSPECTIONS, FOUND L2 DOOR FWD BLANKING PLATE CORRODED. REPLACED L2 DOOR FWD BLANKING PLATE IAW SRM 51-72-00.Jul 1, 2012 · N330NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002823130Blanking Plate · corrodedDURING INSPECTION, FOUND L1 DOOR FWD BLANKING PLATE CORRODED. REPLACED L1 DOOR FWD BLANKING PLATE IAW SRM 51-72-00.Jul 1, 2012 · N330NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002813130Blanking Plate · corrodedDURING INSPECTIONS, FOUND R2 DOOR FWD BLANKING PLATE CORRODED. REPLACED R2 DOOR FWD BLANKING PLATE IAW SRM 51-72-00. NO ALLOWABLE LIMITS ESTABLISHED ON BLANKING PLATE, L=2.0 W=1.5 D=.080 IAW SRM 53-12-00.Jul 1, 2012 · N330NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002803130Blanking Plate · corrodedDURING INSPECTIONS, FOUND L2 DOOR AFT BLANKING PLATE CORRODED. REPLACED L2 DOOR AFT BLANKING PLATE IAW SRM 51-72-00. NO ALLOWABLE LIMITS ESTABLISHED ON BLANKING PLATE, L=1.9 W=1.4 D=.080 IAW SRM 53-12-00.Jul 1, 2012 · N330NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002993130Floor Support · corrodedFORWARD CABIN BETWEEN FR 19 TO FR 22 RT -Y1292 FLOORBEAM AND SEAT TRACK CORRODED. BLENDED DAMAGED AREA IAW SRM 51-74-00, CHECKED LIMITS ORIG MAT .079 INCH D 100 PERCENT LOSS, L 2 INCH W 1.0 INCH FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14 FIG 102. REMOVED FLJun 30, 2012 · N330NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002983130Floor Support · corrodedFORWARD CABIN FLOOR SUPPORT BETWEEN FR 20 TO FR 21 RT -Y189 UPPER FLANGE SURFACE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14 FIG 102. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11.Jun 30, 2012 · N330NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002883130Floor Panel · corrodedAFT UTILITY AREA FLOOR PANEL 261FF IS CORRODED. FLOOR PANEL INSTALLED ON WORK CARD 2500-6602.Jun 30, 2012 · N330NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12002873130Floor Panel · corrodedAFT UTILITY AREA FLOOR PANEL 262FF IS CORRODED. FLOOR PANEL INSTALLED ON WORK CARD 2500-660.Jun 30, 2012 · N330NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12002703130Floor Support · corrodedAFT CABIN FLOOR SUPPORT BETWEEN FR 68 TO FR 66 LT Y1292 UPPER FLANGE HAS CORROSION. BLENDED DAMAGED AREA IAW SRM 51-74-00. ORIG MAT THICKNESS. 087 INCH L 1.0 INCH W .378 INCH D .053 INCH REMAINING MAT .034 INCH. FOUND TO BE OUT OF LIMITS IAW TRM 51-41-15.Jun 30, 2012 · N330NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002693130Floor Support · corrodedAFT CABIN FLOOR SUPPORT BETWEEN FR 68 TO FR 69 LT Y1292 UPPER FLANGE AND HARD PT HOLES HAS CORROSION. BLENDED DAMAGED AREA IAW SRM 51-74-00. ORIG MAT THICKNESS 0.157 INCH L .005 W .173 D .060. REMAINING MAT. .097 INCH. FOUND TO BE OUT OF LIMITS IAW TRM 53-Jun 30, 2012 · N330NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002683130Floor Support · corrodedAFT CABIN FLOOR SUPPORT AT FR68 LT Y765 UPPER FLANGE HAS CORROSION. BLENDED AREA IAW SRM 51-74-00 L=2 W=1 D=0.060 INCH ORIGINAL MAT .137 INCH. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15 FIG 2. RECEIVED NEW FLOORBEAM. REMOVED AND REPLACED FLOOR SUPPORT IAW Jun 28, 2012 · N330NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1209723130Battery Pack · inoperativeFOUND EPSU LEFT BATTERY BAD. REPLACED BATTERY. TESTS OK. AIRCRAFT OK FOR SERVICE.Feb 17, 2012 · N330NB · Airbus A319114 · Emergency LightingSDR DALA1153823130Power Supply · inoperativeDURING NON ROUTINE CHECK, FOUND THE EMERGENCY LIGHTS AT SEAT ROWS 3, 7, 8, 11, 12, 15, 16, 19 AND 20 INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHT POWER SUPPLY AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.Sep 14, 2011 · N330NB · Airbus A319114 · Emergency LightingSDR DALA1142713130Wire Harness · defectiveDURING NON ROUTINE CHECK, FOUND THE EMERGENCY ESCAPE PATH LIGHT AT ROW 6C INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHT HARNESS AND OPERATIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.Jul 4, 2011 · N330NB · Airbus A319114 · Light System WiringSDR DALA1033083130Battery · failedDURING A NON ROUTINE CHECK, THE EMERGENCY LIGHT SYSTEM AT FORWARD LEFT FAILED EPSU INTERNAL LOAD TEST. MAINTENANCE REMOVED AND RECONNECTED BATTERY AND TEST WAS NORMAL. A/C RETURNED TO SERVICE. (2010-00867)Nov 19, 2010 · N330NB · Airbus A319114 · Emergency LightingSDR DALA1019013130Battery Pack · unsecureDURING A NON-ROUTINE CHECK, FOUND EMERGENCY AISLE SEAT PATH LIGHT 3, 4, 7, 8, 11, 15, 16, 19, AND 20 BURNED OUT. RESECURED LOOSE EPSU 11 WL BATTERY. FUNCTIONAL CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.Aug 9, 2010 · N330NB · Airbus A319114 · Emergency LightingSDR DALA104783130Sign · inoperativeDURING A NON ROUTINE CHECK, FOUND THE EMERGENCY LIGHT AT SEAT 2B INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH MARKING SIGN, REINSTALLED AND REPOSITION WIRE. PERFORMED FUNCTIONAL CHECK AND CHECK WAS NORMAL. A/C RETURNED TO SERVICE.Feb 27, 2010 · N330NB · Airbus A319114 · Emergency LightingSDR NWAA084633130Battery Pack · faultedRT EMERGENCY EGRESS BATTERY SHOWS BATTERY FAULT DURING TEST. REPLACED RT BATTERY. CHECKS OK.Oct 15, 2008 · N330NB · Airbus A319114 · Emergency Lighting
Back to N330NB