N332NB

Service difficulty reports · 194

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 = 'N332NB' 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 DALA12011423132Floor Panel · puncturedAFT CARGO FLOOR PANEL 151ZG MULTIPLE PUNCTURES 1.0" X 1.0". NR 150/21 AFT CARGO FLOOR PANEL 151ZG FABRICATED NEW IAW DWG 3D25-40532. DAMAGE DIM L=1.0" W=1.0".Oct 25, 2012 · N332NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12011413132Floor Panel · damagedAFT CARGO FLOOR PANEL 161DF DAMAGED 1.0" X 1.0" NR 150/24. AFT CARGO FLOOR PANEL 161DF FABRICATED NEW IAW A319 DWG 3D25-40532. DAMAGE DIM L=1.0" W=1.0".Oct 25, 2012 · N332NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12011403132Skin · dentedFWD LEFT SIDE OF FUSELAGE AT FR9 APPROX STR 21L DENTED. NR 200/10. DENT IS OUT OF "NEARNESS/FORM" CRITERION IAW SRM 53-11-11, FIG 104 DIM A= 1.1", B=.400", D=.031", T= .047". CUT OUT DAMAGED AREA IAW SRM 53-11-11, FIG 212, DIM. L=2.740" W=1.210". HFEC CUT OOct 25, 2012 · N332NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA12011393132Floor Panel · delaminatedAFT CARGO FLOOR PANEL 161PF DELAMINATED. 4.0" X 3.5". N/R 150/23. FLOOR PANEL FABRICATED NEW IAW DWG 3D25-40532. DAMAGE DIM L=4.0" W=3.5".Oct 25, 2012 · N332NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12011383132Panel · puncturedAFT CARGO SLOPE PANEL 152UG TOP SKIN PUNCTURED. 3.0" X 1.5". N/R 150/29. AFT CARGO SLOPE PANEL 152UG FABRICATED NEW ON IAW DWG 3025-40532. DAMAGE DIM. L=3.0" W=1.5". RETAIN FOR RECORDS.Oct 25, 2012 · N332NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12011373132Panel · damagedFORWARD CARGO SLOPE PANEL 131 EG MULTIPLE PUNCTURES 1.0" X 1.0". N/R 130/26. FORWARD CARGO SLOPE PANEL 131EG FABRICATED NEW IAW DWG 3D25-40532. DAMAGE DIM. L=1.0" W=1.0". RETAIN FOR RECORDS.Oct 25, 2012 · N332NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12011363132Floor Panel · damagedMAIN CABIN FLOOR PANEL 231YG DAMAGED ON EDGE "3.0 X 3.0". FLOOR PANEL 231YG FABRICATED NEW IAW DWG 3D25-40640.Oct 24, 2012 · N332NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12011353132Floor Panel · delaminatedAFT UTILITY FLOOR PANEL 261PF DELAMINATED AT LOWER SURFACE "4.0 X4 4.0". FABRICATED FLOOR PANEL IAW DWG 3D25-40640.Oct 24, 2012 · N332NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12011343132Floor Panel · puncturedFORWARD UTILITY FLOOR PANEL 222CF PUNCTURED AT SEVERAL LOCATIONS "3 X 3". FLOOR PANEL FABRICATED NEW IAW DWG 3D25-40640.Oct 24, 2012 · N332NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12011333132Shear Plate · crackedAFT UTILITY AREA RT SIDE BTW FR 68-69 STR 23R SHEAR PLATE CRACKED. R & R SHEAR PLATE IAW SRM 51-42-11.Oct 24, 2012 · N332NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12011323132Plate · corrodedL2 DOOR FORWARD AND AFT BLANKING PLATES CORRODED (PANEL RACK). RECEIVED NEW BLANKING PLATES AT L2 DOOR FWD AND AFT TO BE INSTALLED ON W/C 2500-6602.Oct 24, 2012 · N332NB · Airbus A319114 · Passenger/Crew DoorsSDR DALA12010963132Floor Panel · corrodedFORWARD UTILITY FLOOR PANEL 222FF CORRODED ON LWR SURFACE 4.0" X 3.5". INSTALLED NEW FLOOR PANEL IAW SRM 51-72-00.Oct 23, 2012 · N332NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12010953132Floor Panel · corrodedFORWARD UTILITY FLOOR PANEL 221FF CORRODED ON LOWER SURFACE 2.0" X 3.0". INSTALLED NEW FLOOR PANEL IAW SRM 51-72-00.Oct 23, 2012 · N332NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12010943132Web · corrodedFORWARD CABIN LT SIDE AT DOOR FRAME 16 UPPER WEB HAS CORROSION. REMOVED UPPER WEB LT FROM FR 12 TO FR 16 IAW SRM 51-42-11. RECEIVED NEW WEB. INSTALLED NEW UPPER WEB LT FROM FR 12 TO FR 16 IAW SRM 51-42-11. DAMAGE DIM. L=.95" W=.42" D=.041". ORIG MAT .071".Oct 22, 2012 · N332NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12010933132Seat Track · corrodedFORWARD CABIN FLOOR SUPPORT BETWEEN FR16 TO FR20 Y-1292 UPPER FLANGE HAS SCRIBE LINE AND FORWARD SEAT TRACK FLANGE CORRODED. BLENDED AREA IAW ARM 51-74-00. BLENDED AREA MEASURES L=2.00" W=.500" D=054 ORIG MAT .079. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-15 FIOct 22, 2012 · N332NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA12010923132Web · corrodedFORWARD CABIN LT SIDE AT DOOR FRAME 20 UPPER WEB AND ANGLE HAS CORROSION. REMOVED CORROSION FROM PREVIOUS BLENDOUT IAW SRM 51-74-00. AFTER REWORK, BLENDOUT AT WEB L=1.3" W=1.2" REMAINING MATERAL .050" ORIG MATERIAL .071" BLENDED AT ANGLE L=2" W=1" REMAINING MAOct 22, 2012 · N332NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12010913132Floor Support · corrodedFORWARD CABIN FLOOR SUPPORT BTW FR16 TO FR20 Y-254 UPPER FLANGE HAS CORROSION. SSI 531189. BLENDED CORROSION ON Y-254 FLOOR SUPPORT IAW SRM 51-74-00 L=2.0" W=1.625" D=.079". FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14, FIG 105. R & R FLOOR SUPPORT Y-254 IAW SOct 22, 2012 · N332NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12010903132Floor Support · corrodedAFT UTILITY AREA RT SIDE FLOOR SUPPORT Y-1732 BETWEEN FR65-66 UPPER FLANGE HOLES HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14, FIG 102. R & R FLOOR SUPPORT IAW SRM 51-42-11. DIMENSIONS L=1.0" W=0.80 D=0.025.OROct 22, 2012 · N332NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12010893132Floor Support · corrodedAFT CABIN FLOOR SUPPORT BETWEEN FR 64 TO FR 66 Y1292 HARD POINTS HOLES AND UPPER FLANGE CORRODED. REMOVED CORROSION IAW SRM 51-74-00. ORIG MATERIAL .087" L=2.0" W=1.0" D=.070". FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15 FIG 1. REMOVED Y1292 FLOOR SUPPORT IAWOct 21, 2012 · N332NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12010883132Floor Support · corrodedAFT CABIN FLOOR SUPPORT BETWEEN FR 68 TO FR 69 Y1292 UPPER FLANGE HOLES CORRODED. REMOVED CORROSION IAW SRM 51-74-00. ORIG MATERIAL .157" L=2.0" W=1.0" D=.070". FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15, FIG 1. REMOVED Y1292 FLOOR SUPPORT IAW SRM 51-42-11. Oct 21, 2012 · N332NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12010873132Floor Support · corrodedAFT CABIN FLOOR SUPPORT BETWEEN FR 66 TO FR 68 Y1292 UPPER FLANGE HOLES CORRODED. REMOVED CORROSION IAW SRM 51-74-00. ORIG MATERIAL .087" L=2.0" W=1.0" D=.070". FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15, FIG 1. REMOVED Y1292 FLOOR SUPPORT IAW SRM 51-42-11.Oct 21, 2012 · N332NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12010853132Floor Support · corrodedFORWARD UTILITY AREA FLOOR SUPPORT BETWEEN FR14 -FR16 Y503.2 UPPER FLANGE HOLES CORRODED. BLENDED AREA IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS. R & R Y503.2 FLOOR SUPPORT AT FR12-FR16 IAW SRM 51-42-11. DAMAGE DIMENSIONS L=1.42"W=1.34"D=0.054" ORIG.MAT Oct 21, 2012 · N332NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12010843132Web · damagedFORWARD CABIN RT SIDE LOWER DOOR FR 20 UPPER WEB SURFACE HAS CORROSION. REMOVED WEB IAW SRM 51-42-11. INSTALLED NEW WEB. RT FR20 TO FR24 IAW SRM 51-42-11. DAMAGE DIMENSIONS L=1.0"W=1.0"D=0.020", ORIG MAT. 0.71".Oct 21, 2012 · N332NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12010833132Floor Support · corrodedFORWARD CABIN FLOOR SUPPORT BETWEEN FR16 TO FR23, Y254 UPPER FLANGE CORRODED. BLENDED AREA IAW RM 51-74-00, CHECKED LIMITS ORIG MAT .079" DAMAGE DIM. L=1.60" W=1.52" D=.053". FOUND TO BE OUT OF LIMIT IAW SRM 53-11-14, FIG 105. R & R FLOOR SUPPORT IAW SROct 19, 2012 · N332NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12010863132Sill · corrodedLEFT AFT PASSENGER DOOR SILL AT FR 66 UPPER FLANGE SURFACE AND GIRT BAR INBD. NUT PLATE HOLES HAS CORROSION. CUTOUT DAMAGED IAW SRM 53-41-14, FIG 201. INSTALLED REPAIR ANGLE AND FILLER IAW SRM 53-41-14, FIG 201. DIMENSION CUTOUT L=1.3" W=.900". FABRICATED Oct 18, 2012 · N332NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12010823132Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT BETWEEN FR 68-69 Y-1292 UPPER AND LOWER FLANGE HOLES HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. CHECK DIMENSIONS ORIG MATERIAL THICKNESS .157", L=5.500", W=1.100"D=.065", REMAINING .092", FOUND TO BE OUT OF LIMITS IAW TOct 18, 2012 · N332NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12010813132Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT BETWEEN FR 66 TO FR 68 Y-1292 UPPER AND LOWER FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00, DIMENSIONS L=1.0" W=.090" D.060", ORIG THICK .087". FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15, FIG 1. REMOVED FLOOR SUPPOROct 18, 2012 · N332NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12010803132Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT BETWEEN FR 64 TO FR 66 Y-1292 INSIDE HARD POINT HOLES AND UPPER FLANGE OF FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00, DIMENSIONS L=1.0"W=1.0"D =.060",ORIG THICK .098". FOUND TO BE OUT OF LIMITS IAW TRM 53-41Oct 18, 2012 · N332NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12010793132Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT BETWEEN FR 65-66 Y1732 UPPER FLANG HOLES HAS CORROSION. R & R FLOOR SUPPORT IAW SRM 51-42-11. BLENDED AREA IAW SRM 51-74-00 L=1.0 W=0.8" D=0.03" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14, FIG 102.Oct 18, 2012 · N332NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12010783132Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT BETWEEN FR 67-68, Y-254 UPPER AND LOWER FLANGE HOLES HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 51-00-14, FIG 102. R & R FLOOR SUPPORT IAW SRM 51-42-11.Oct 18, 2012 · N332NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12010583132Floor Support · corrodedFORWARD UTILITY AREA FLOORBEAM BETWEEN FR16 TO FR20 Y1292 HARD POINT HOLE INSIDE AND UPPER FLANGE BEAM CORROSION. SSI 531189. BLENDED AREA IAW SRM 51-74-00 L=2.0 W=1.10 D=.040 FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14, FIG 102. R & R FLOOR BEAM IAW SRM 51-42Oct 18, 2012 · N332NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12010573132Floorbeam · corrodedFORWARD CABIN FLOORBEAM BETWEEN FR 20 TO FR 24 Y-189 UPPER FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. ORIG MAT .080 DAMAGE DIM. L=6.0 W=2.0 D=.060. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14. R & R FLOORBEAM IAW SRM 51-42-11.Oct 16, 2012 · N332NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA12010143132Floor Support · corrodedAFT UTILITY AREA FLOORBEAM BTW FR66 TO FR69 Y765 UPPER FLANGE CORRODED. REMOVED CORROSION IAW SRM 71-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-71-15, FIG 1. R & R FLOORBEAM Y765 FR66 -69 IAW SRM 51-42-11 AND TRM 53-21-01. RETAIN FOR RECORDS.Oct 15, 2012 · N332NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12010133132Floor Support · corrodedAFT UTILITY FLOORBEAM BETWEEN FR64 TO FR66 Y765 UPPER FLANGE CORRODED. REMOVED CORROSION IAW SRM 71-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-71-15, FIG 1. R & R SPLICE AND FLOORBEAM Y765, FR64-66 IAW SRM 51-42-11 AND TRM 53-21-01. RETAIN FOR RECORDS.Oct 15, 2012 · N332NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12010123132Floor Support · corrodedAFT UTILITY FLOORBEAM BETWEEN FR66-68 Y-765, UPPER AND LOWER FLANGE HOLES HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00 FOUND TO BE OUT OF LIMITS IAW TRM 53-71-15, FIG 1. R & R FLOORBEAM IAW SRM 51-42-11 AND TRM 53-21-01. RETAIN FOR RECORDS.Oct 15, 2012 · N332NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1211193132Wire · brokenAIRCRAFT 3132 SEAT 3AB EMERGENCY ESCAPE PATH LIGHT INOPERATIVE. FOUND WIRES BROKEN AND CONNECTOR MISSING NEAR FLOOR TRACK. REPINNED BROKEN WIRES AND INSTALLED NEW CONNECTORS. RE-SECURED HARNESS.Feb 22, 2012 · N332NB · Airbus A319114 · Light System WiringSDR DALA1019403132Wire · unsecureDURING A NON-ROUTINE CHECK, FOUND EMERGENCY PATH LIGHT AT ROW 4 & 11 INOPERATIVE. RESECURED PIGTAIL AND FUNCTIONAL CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.Aug 15, 2010 · N332NB · Airbus A319114 · Emergency LightingSDR DALA1019413132Connector · unsecureDURING A NON ROUTINE CHECK, FOUND EMERGENCY PATH LIGHT AT ROW 2 INOPERATIVE. RESECURED LOOSE CONNECTION AND FUNCTIONAL CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.Aug 15, 2010 · N332NB · Airbus A319114 · Emergency LightingSDR DALA109673132Door Frame · gougedDURING LINE CHECK FOUND GOUGE IN AFT CARGO DOOR FRAME AT FR59. REPAIRED IAW ERA 482347-14.May 7, 2010 · N332NB · Airbus A319114 · Fuselage Main, StructureSDR NWAA 091693132Controller · faultyCAB PR SYS 1 AND 2 FAULT, ECAM MESSAGE, FOLLOWED COM PROCEDURE AND SWITCHED TO MANUAL SYSTEM. OUTFLOW WAS FULLY CLOSED AND CABIN STILL CLIMBING 4-500 FPM AT FL390. NOTICED VENT EXTRACT VALVE ON ECAM PRESS GAGE INDICATING INTERMITTENT IN INTERMEDIATE POSITIONMay 15, 2009 · N332NB · Airbus A319114 · Cabin Pressure ControllerSDR NWAA09273132Fan · defectiveDIVERTED BECAUSE OF STRONG BURNING SMELL THAT WOULD COME AND GO THROUGHOUT THE ACFT. LANDING WAS UNEVENT. AT GATE, COND LT AND RT CAB FAN FAULT ON ECAM, FOUND RECIRC FAN L SPLY CIRCUIT BREAKER POPPED. REPLACED LT RECIRCULATION FAN, CHECKS GOOD. (K)Feb 1, 2009 · N332NB · Airbus A319114 · Air Distribution FanSDR NWAA072043132Attach Fitting · damagedDURING "H" CHECK MAINTENANCE DAMAGED LAVATORY D ATTACH FITTING. REPAIRED PER EA 31-208441.May 23, 2007 · N332NB · Airbus A319114 · Fuselage Main, Attach FittingsSDR 0600813132Power Supply · failedDURING A-CHECK THE EPSU INT LOAD FWD L MESSAGE ON CIDS. REPLACED EMERGENCY POWER SUPPLY UNIT (EPSU) 31-3350-9-0001 S/N 04111.Apr 22, 2006 · N332NB · Airbus A319114 · Emergency LightingSDR 0600803132Power Supply · inoperativeDURING A-CHECK THE EPSU INT LOAD FWD L MESSAGE ON CIDS. REPLACED EMERGENCY POWER SUPPLY UNIT (EPSU) 31-3350-9-0001 S/N 04080.Apr 22, 2006 · N332NB · Airbus A319114 · Emergency Lighting
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