N325NB

Service difficulty reports · 138

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 = 'N325NB' 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 DALA12005913125Floor Panel · damagedAFT CARGO FLOOR PANEL 151UG HAS EDGE DAMAGE 6 INCHES BY 1 INCH. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00 FIG 209 DWG 3D25-40532.Aug 18, 2012 · N325NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12005903125Panel · delaminatedFORWARD CARGO SLOPE WALL PANEL 131BF PUNCTURED AND DELAMINATED. FABRICATED NEW PANEL IAW SRM 53-02-00 FIG 209 DWG 3D25-40532.Aug 18, 2012 · N325NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12005893125Floor Panel · delaminatedAFT CARGO FLOOR PANEL 151ZG DELAMINATED 4 INCHES BY 4 INCHES. FLOOR PANEL FABRICATED PER DWG 3D25-40532 IAW SRM 53-02-00 FIG 209.Aug 18, 2012 · N325NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12005883125Floor Panel · puncturedAFT CARGO FLOOR PANEL 161NF MULTIPLE PUNCTURES 2.0 INCHES BY 2.5 INCHES. FLOOR PANEL FABRICATED PER DWG 3D25-40532 IAW SRM 53-02-00 FIG 209.Aug 18, 2012 · N325NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12005873125Panel · puncturedAFT CARGO SLOPE PANEL 151BE MULTIPLE PUNCTURES. SLOPE PANEL FABRICATED PER DWG 3D25-40532 IAW SRM 53-02-00 FIG 209.Aug 18, 2012 · N325NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12005863125Panel · puncturedAFT CARGO SLOPE PANEL 152XG MULTIPLE PUNCTURES. FABRICATED SLOPE PANEL PER DWG 3D25-40532 IAW SRM 53-02-00 FIG 209.Aug 18, 2012 · N325NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12005853125Panel · puncturedAFT CARGO SLOPE PANEL 152WG MULTIPLE PUNCTURES. SLOPE PANEL FABRICATED PER DWG 3D25-40532 IAW A319 SRM 53-02-00 FIG 209.Aug 18, 2012 · N325NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12005843125Floor Panel · puncturedAFT CARGO FLOOR PANEL 161PF PUNCTURED 1.0 INCH BY 1.0 INCH. FLOOR PANEL FABRICATED PER DWG 3D25-40532 IAW A319 SRM 53-02-00 FIG 209.Aug 18, 2012 · N325NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12005833125Panel · delaminatedAFT CARGO SLOPE PANEL 151DE DELAMINATED 2 FT BY 2 INCHES. SLOPE PANEL FABRICATED PER DWG 3D25-40532 IAW A319 SRM 53-02-00 FIG 209.Aug 18, 2012 · N325NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12005823125Panel · delaminatedAFT CARGO SLOPE PANEL 162BF DELAMINATED 2 INCH BY 2 INCH. SLOPE PANEL FABRICATED PER DWG NR 3D25-40532 IAW A319 SRM 53-02-00 FIG 209.Aug 18, 2012 · N325NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12005583125Floor Panel · delaminatedAFT UTILITY FLOOR PANEL 261PF DAMAGED 4" BY 4". FABRICATED NEW FLOOR PANEL 261PF AT AFT UTILITY AREA IAW A319 SRM 53-02-00 FIG 209.Aug 15, 2012 · N325NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12005573125Floor Panel · delaminatedFWD UTILITY FLOOR PANEL 231CF DELAMINATED. FABRICATED NEW FLOOR PANEL 231CF AT FWD UTILITY AREA IAW A319 SRM 53-02-00 FIG 209. DAMAGE DIM L=1.0" W=1.5".Aug 15, 2012 · N325NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12005563125Floor Panel · corrodedFORWARD UTILITY FLOOR PANEL 232FF HAS CORROSION. FABRICATED NEW FLOOR PANEL 232FF AT FORWARD UTILITY AREA IAW A319 SRM 53-02-00 FIG 209. DAMAGE DIM L=1.5" W=1.5".Aug 15, 2012 · N325NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12005553125Sill · corrodedRIGHT PASSENGER DOOR WAY AT FR16 INSIDE GIRT BAR FITTING DOOR SILL HAS CORROSION. REMOVED CORROSION IAW A319 SRM 51-74-00, L=.180" W=.180" D=.016. NO ESTABLISHED LIMITS AVAILABLE IAW A319 SRM 51-11-14. REMOVED DOOR SILL FR16 TO FR20 IAW A319 SRM 51-42-11. RAug 14, 2012 · N325NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12005543125Floor Support · corrodedAFT CABIN UTILITY AREA FLOOR SUPPORT WEB UPPER SURFACE AREA COVERED BY SHEAR PLATE HAS CORROSION, LOC FR69-FR70, STR 23R. REMOVED CORROSION IAW A319 SRM 51-74-00 L=2.5 W=1.5 D=.054 ORIG. .063 NO ESTABLISHED LIMITS PER A319 SRM 53-41-14. REMOVED AND INSTALLEDAug 14, 2012 · N325NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12005473125Floorbeam · corrodedAFT UTILITY AREA FLOORBEAM BTW FR64 TO FR66 Y-765 HARD POINT HOLES UPPER FLANGE SURFACE CORRODED. BLENDED AREA IAW A319 SRM 51-74-00. ORIGINAL THICKNESS .087" D+.060" L=1.5" W=1". REMAINING THICKNESS .027 FOUND OUT OF LIMITS IAW A319 TRM 53-41-15. REMOVED Aug 12, 2012 · N325NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA12005463125Floorbeam · corrodedFORWARD UTILITY AREA FLOORBEAM BTW FR14 TO FR16 Y765 UPPER FLANGE HOLES HAS CORROSION. BLENDED CORRODED AREA IAW A319 SRM 51-74-00 DIM L=1.400 INCH W=1.200 INCH D=.065 INCH. FOUND OUT OF LIMITS IAW A319 SRM 53-11-14 FIG 102. REMOVED AND REPLACED FLOORBEAM Aug 12, 2012 · N325NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA12005453125Skin · dentedAFT FUSELAGE LOWER EXTERNAL SKIN (BELOW L2 DOOR 3 INCH FWD OF FR 68 BTW STR 28L - 29L) DENTED (PREVIOUSLY IDENTIFIED ON LP 3335721). HFEC IAW NTM 51-10-08 PT 6 INTERNAL AND EXTERNAL. NO DEFECTS. DIMENSION OF DENTED AREA L=2.7 W=1.5 D=0.053 A=1.85 B=0.58 ORIAug 12, 2012 · N325NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA12005533125Floorbeam · corrodedAFT UTILITY AREA FLOORBEAM BTW FR68 TO FR69 Y1292 UPPER FLANGE HAS CORROSION. BLENDED AREA IAW A319 SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW A319 TRM 53-41-15. REMOVED AND REPLACED FLOORBEAM IAW A319 SRM 51-42-11. ORIG MAT. .157". DAMAGE DIM L=2.0" W=1Aug 11, 2012 · N325NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA12005523125Floorbeam · corrodedAFT UTILITY AREA FLOORBEAM BTW FR66 TO FR68 Y1292 UPPER FLANGE HAS CORROSION. BLENDED AREA IAW A319 SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW A319 TRM 53-41-15. REMOVED AND REPLACED FLOORBEAM IAW A319 SRM 51-42-11. ORIG MAT. .087". DAMAGE DIM L=2.0" W=1Aug 11, 2012 · N325NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA12005513125Floorbeam · corrodedAFT UTILITY AREA FLOORBEAM BTW FR64 TO FR66 Y1292 HARD POINT HOLES AND UPPER FLANGES HAS CORROSION. BLENDED AREA IAW A319 SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW A319 TRM 53-41-15. REMOVED AND REPLACED FLOORBEAM IAW A319 SRM 51-42-11 ORIG MAT. .087 INCHAug 11, 2012 · N325NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA12005313125Floor Panel · corrodedFORWARD UTILITY FLOOR PANEL 222FF HAS CORROSION. RECEIVED NEW FLOOR PANEL INSTALLED ON JOB CARD 2500-6601.Aug 11, 2012 · N325NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12005443125Floor Support · corrodedAFT CARGO FLOOR PANEL 152BE CORRODED AROUND FASTENER HOLE .200 INCH BY .150 INCH. AFT CARGO FLOOR PANEL REPLACED IAW A319 SRM 51-72-00. INSTALLED ON W/C 2500-5919 PANEL 152BE. NO LIMITS AVAILABLE.Aug 9, 2012 · N325NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12005203125Shear Plate · crackedAFT UTILITY AREA RT SIDE BTW FR 68 TO FR 69 STRINGER 23R SHEAR PLATE CRACKED. REMOVED SHEAR PLATE AND SUPPORT IAW SRM 51-42-11. LOCATED AND DRILLED NEW SHEAR PLATE IAW SRM 51-44-11. INSTALLED NEW SHEAR PLATE IAW SRM 51-42-11.Aug 9, 2012 · N325NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12005193125Floor Panel · corrodedAFT UTILITY FLOOR PANEL 261FF CORRODED 5 INCHES BY 4 INCHES. FLOOR PANEL INSTALLED ON W/C 5310-6017.Aug 8, 2012 · N325NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12005183125Floor Panel · corrodedAFT UTILITY FLOOR PANEL 262FF CORRODED 3 INCH BY 5 INCH. FLOOR PANEL INSTALLED ON W/C 5310-6017.Aug 8, 2012 · N325NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12005173125Floor Support · corrodedFORWARD UTILITY AREA FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-11-14 FIG 107. REMOVED AND REPLACED IAW SRM 51-42-11.Aug 8, 2012 · N325NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12005163125Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-15. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11.Aug 7, 2012 · N325NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12005153125Floor Support · corrodedFORWARD UTILITY AREA FLOOR SUPPORT CORRODED. BLENDED AREA IAW SRM 51-74-00. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-11.Aug 6, 2012 · N325NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12005093125Floor Support · corrodedFORWARD UTILITY AREA FLOOR SUPPORT CORRODED. BLENDED AREA IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14 FIG 106. REMOVED FLOOR SUPPORT IAW SRM 51-42-11. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-42-11.Aug 6, 2012 · N325NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12005283125Floorbeam · corrodedFORWARD UTILITY AREA FLOORBEAM AT FR 14 Y-81 UNDERNEATH OF RAIL HAS CORROSION. REMOVED AND REPLACED FR 14 BEAM Y-81 IAW SRM 51-42-11.Aug 4, 2012 · N325NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA12005503125Floorbeam · corrodedAFT UTILITY AREA FLOORBEAM BTW FR 66 TO FR 68 Y-1292 UPPER FLANGE HAS CORROSION. REMOVED CORROSION IAW A319 SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-41-15. REMOVED AND REPLACED BEAM IAW A319 SRM 51-42-11.Aug 3, 2012 · N325NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA12005493125Floorbeam · corrodedAFT UTILITY AREA FLOORBEAM BTW FR 68 TO 69 Y-1292 UPPER FLANGE HAS CORROSION. REMOVED CORROSION IAW A319 SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-41-15. REMOVED AND REPLACED BEAM IAW A319 SRM 51-42-11.Aug 3, 2012 · N325NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA12005483125Floorbeam · corrodedAFT UTILITY AREA FLOORBEAM BTW FR 64 TO 66 Y-1292 HARD POINT UPPER FLANGE HOLES CORRODED. REMOVED CORROSION IAW A319 SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW A319 TRM 53-41-15. REMOVED AND REPLACED BEAM IAW A319 SRM 51-42-11.Aug 3, 2012 · N325NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA12005303125Floorbeam · corrodedAFT UTILITY AREA FLOORBEAM BTW FR 66 TO FR 68 Y-765 UPPER FLANGE HAS CORROSION. BLENDED AREA IAW SRM 51-74-00 ORIGINAL THICKNESS .157 INCH D=0.040 INCH DIA 3.5 INCH, FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. REMOVED BEAM BETWEEN FRAME 66 AND 68 Y-765 IAW SAug 3, 2012 · N325NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA12005293125Floorbeam · corrodedAFT UTILITY AREA FLOORBEAM AT FR68 Y-465 UPPER FLANGE HAS CORROSION. REMOVED AND REPLACED FLOORBEAM AT FR 68 Y-465 IAW SRM 51-42-11.Aug 3, 2012 · N325NB · Airbus A319114 · Fuselage Main, Floor BeamSDR NWAA080293125Pump · leakingEN ROUTE GREEN SYS HYD QUANTITY DECREASING, GOT GREEN HYD LOW PRESS ON ECAM. WENT THROUGH ECAM COM, SHUT-DOWN GREEN HYD SYSTEM PER COM. QUANTITY AMOUNT GRADUALLY DECREASED BELOW AMBER BOX WHEN GOT THE ECAM MESSAGE GREEN LOW PRESS. PER COM LANDING GEAR ALTERJan 30, 2008 · N325NB · Airbus A319114 · Hydraulic Pump (Electric/Engine), MainSDR 0203863125Service difficultyReceived VENT EXTRACT FAULT shortly after takeoff. Crew experienced grinding noise, mild vibration and strong smoke smell. Returned to IAH and landed uneventfully. Found avionics cooling extract fan 18Q failed. Applied MEL 21-26-02 provisions and returned A/C Nov 15, 2002 · N325NB · Airbus A319114 · Air Distribution Fan
Back to N325NB