N328NB

Service difficulty reports · 175

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 = 'N328NB' 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 DALA13005703128Epsu · failedDURING SERVICE CHECK FOUND EPSU BATTERY EMERGENCY AFT LT FAILED. REMOVED BATTERY, SN 105375 AND REPLACED WITH NEW BATTERY, PERFORMED OPS CHECK IAW AMM 33-51-38. OPS CHECK GOOD. OK FOR SERVICE.Jan 30, 2013 · N328NB · Airbus A319114 · Emergency LightingSDR DALA12017383128Battery Pack · inoperativeDURING EMERGENCY ELECTRICAL CONFIGURATION, EMERGENCY ESCAPE LIGHT AT CENTER CABIN RT OVERWING EMERGENCY EXIT LIGHT, AND BOTH AFT EXIT LIGHTS WERE INOPERATIVE. MX REPLACED RT MID EMERGENCY POWER SUPPLY BATTERY AND CHECK WAS NORMAL.Dec 29, 2012 · N328NB · Airbus A319114 · Emergency LightingSDR DALA12003183128Floor Panel · damagedAFT CABIN UTILITY FLOOR PANEL 261BG DAMAGED. FABRICATED NEW FLOOR PANEL PER DWG 3D25-40640. DAMAGE DIM L=26 INCH W=29 INCH.Jul 6, 2012 · N328NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12003123128Sill · corrodedL1 DOOR SILL FWD GIRT BAR MATING SURFACE, AFT INBOARD MOUNTING BOLT HOLE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00, L=3.1 INCH W=1.8 INCH D=.032 INCH. NO ESTABLISHED DAMAGE LIMITS ON SRM. REMOVED AND REPLACED L1 DOOR SILL IAW SRM 51-42-11.Jul 3, 2012 · N328NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12003113128Floor Panel · damagedAFT CABIN UTILITY FLOOR PANEL 262BG DAMAGED. FABRICATED FLOOR PANEL IAW DWG 3D25-40640. DAMAGE L=24 INCH W=8 INCH.Jul 3, 2012 · N328NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12003103128Floor Panel · damagedCENTER CABIN FLOOR PANEL 241JF DAMAGED. FABRICATED FLOOR PANEL IAW DWG 3D25-40640. DAMAGE L=100 INCH W=1 INCH.Jul 3, 2012 · N328NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12003093128Floor Panel · damagedFORWARD CABIN FLOOR PANEL 232DF DAMAGED. FABRICATED FLOOR PANEL 232DF PER DWG 3D25-40640. DAMAGE W=1.50 INCH, L=1.50 INCH.Jul 3, 2012 · N328NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12003083128Floor Panel · damagedFORWARD CABIN FLOOR PANEL 231EF DAMAGED. FABRICATED FLOOR PANEL IAW DWG 3D25-40640 DAMAGE L=10.0 INCH, W=2.0 INCH.Jul 3, 2012 · N328NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12003073128Floorboard · damagedCABIN FLOORBOARD 251WF DAMAGED. FABRICATED NEW FLOORBOARD PER DWG 3D25-40640. DAMAGE DIM L=59 INCH, W=17 INCH.Jul 3, 2012 · N328NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12003063128Floor Panel · damagedCABIN FLOOR PANEL 252FG DAMAGED. FABRICATED NEW FLOOR PANEL PER DWG 3D25-40640.Jul 3, 2012 · N328NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12003023128Floor Support · corrodedFORWARD MAIN CABIN FLOOR SUPPORT STRUCTURE FOR DOOR BETWEEN -Y254 AND +Y254 AT FR 21 HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00, L=6 INCH, W=.5 INCH, D=.040 INCH ORIG MAT.= .055. NO ALLOWABLE DAMAGE ESTABLISHED ON SRM. REMOVED FLOOR SUPPORT PLATE IAWJul 2, 2012 · N328NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002843128Sill · corrodedDURING INSPECTIONS FOUND R1 DOOR SILL AFT GIRT BAR MATING SURFACE, AFT OTBD MOUNTING BOLT HOLE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00, L=1.10 INCH W=.9 INCH D=.011 INCH AND REPLACED R1 DOOR SILL IAW SRM 51-42-11.Jul 1, 2012 · N328NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002673128Floor Support · corrodedFORWARD MAIN CABIN FLOOR SUPPORT BET FR18 AND FR20 -Y254 HAS CORROSION. BLENDED AREA IAW SRM 51-74-00. MATERIAL LOSS .079 INCH L=4 INCH W=2 INCH. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14 FIG 105. REMOVED AND REPLACED DAMAGE FLOOR SUPPORT IAW SRM 51-42-11Jun 28, 2012 · N328NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002663128Support Angle · corrodedAFT UTILITY Y1732 SHEAR WEB SUPPORT ANGLE, FWD OF FR 70 HAS CORROSION ON UNDERSIDE AT AFT 2 FASTENER HOLES. BLENDED DAMAGED AREA IAW A319 SRM 51-74-00, L=1 INCH W=0.5 D=.030. NO ALLOWABLE LIMITS FOUND. REMOVED AND REPLACED SHEAR WEB SUPPORT ANGLE IAW A319 SJun 28, 2012 · N328NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002633128Floor Panel · corrodedAFT CABIN UTILITY FLOOR PANEL 261FF HAS CORROSION. REPLACED FLOOR PANEL 261FF WITH NEW FLOOR PANEL 261FF IAW SRM 51-72-11. FLOOR PANEL INSTALLED ON WORKCARD 2500-6602.Jun 28, 2012 · N328NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12002783128Floor Support · corrodedDURING INSPECTIONS FOUND AFT UTILITY FLOOR SUPPORT -Y1292 HAS 3 AREAS WITH CORROSION BETWEEN FR 65 AND FR 66. REMOVED CORROSION IAW SRM 51-74-00 L=1.5 INCH W=.5 INCH D=.030 INCH. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.Jun 27, 2012 · N328NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002773128A/C Pack · corrodedDURING INSPECTIONS FOUND AFT UTILITY FLOOR SUPPORT -Y1292 HAS 7 AREAS WITH CORROSION BETWEEN FR 66 AND FR 68. REMOVED CORROSION IAW SRM 51-74-00 L=2 INCH W=1.25 INCH D=.055 INCH. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.Jun 27, 2012 · N328NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002763128A/C Pack · corrodedDURING INSPECTIONS FOUND AFT UTILITY FLOOR SUPPORT -Y1292 HAS 5 AREA WITH EXFOLIATION BETWEEN FR 68 AND FR 69. REMOVED CORROSION IAW SRM 51-74-00 L=1.5 INCH W=1.0 INCH D=.060 INCH. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.Jun 27, 2012 · N328NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002753128A/C Pack · corrodedDURING INSPECTIONS FOUND AFT UTILITY FLOOR SUPPORT Y254 BETWEEN FR 68 AND FR 70, BOTH HARD POINT MOUNT HOLES ARE CORRODED. BLENDED CORROSION IAW SRM 51-74-00. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.Jun 27, 2012 · N328NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002743128Floor Support · corrodedDURING INSPECTIONS FOUND AFT UTILITY FLOOR SUPPORT Y512 HAS CORROSION ABOVE FR 66. BLENDED CORROSION IAW SRM 51-74-00, L=1.5 INCH W=1.0 INCH D=.025 INCH. REPLACED FLOOR SUPPORT PROFILE IAW SRM 51-42-11.Jun 27, 2012 · N328NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002653128Flap Track · corrodedLEFT WING OUTBOARD FLAP TRACK NR 3 AND NR 4 PIVOT BOLTS HAVE CORROSION AND ARE MISSING PLATING. ACCOMPLISHED INSTALLATION OF NEW LEFT WING OUTBOARD FLAP TRACK NR 3 AND NR 4 PIVOT BOLTS ON WORKCARD NO 2750-6020RT. BOLTS REPLACED DUE TO OUT OF LIMITS IAW AMM 2Jun 27, 2012 · N328NB · Airbus A319114 · Trailing Edge FlapsSDR DALA12002643128Flap Track · corrodedRIGHT WING INBOARD FLAP TRACK NR 2 PIVOT BOLT HAS CORROSION AND MISSING PLATING. RT WING INBOARD FLAP NR 2 TRACK PIVOT BOLT REPLACED. FOUND TO BE OUT OF LIMITS IAW A319 AMM 27-54-61-220-001. INSTALLATION ACCOMPLISHED ON WORKCARD NR 2750-6010 RT. DAMAGE DIMJun 27, 2012 · N328NB · Airbus A319114 · Trailing Edge FlapsSDR DALA12002623128Floor Support · corrodedAFT UTILITY Y765 FLOOR SUPPORT HAS EXFOLIATION AROUND HARD POINT MOUNT FWD OF FR 66. REMOVED CORROSION IAW SRM 51-74-00. CHECKED LIMITS L=2.5 INCH W=2.0 INCH D=0.032 INCH. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14 FIG 102. MAXIMUM ALLOWABLE DEPTH OF 0.016Jun 27, 2012 · N328NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002613128Floor Support · corrodedAFT UTILITY FLOOR SUPPORT Y1292 HAS CORROSION ABOVE FR 66. REMOVED CORROSION IAW SRM 51-74-00. ORIG MAT. 0.087 DAMAGE DIM. L=1.5 INCH W=1.0 INCH D=0.072 INCH. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-15. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-11.Jun 27, 2012 · N328NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002603128Floor Support · corrodedAFT UTILITY FLOOR SUPPORT Y1292 HAS CORROSION AROUND FASTENER HOLES BETWEEN FR 68 AND FR 69. REMOVED CORROSION IAW SRM 51-74-00. ORIG MAT. 0.157 DAMAGE DIM. L=1.3 INCH W=1.0 INCH D=0.064 INCH. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-15. REMOVED AND REPLACEDJun 27, 2012 · N328NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002593128Floor Support · corrodedAFT UTILITY FLOOR SUPPORT Y1292 HAS CORROSION 4 AREAS BETWEEN FR 67 AND FR 68. REMOVED CORROSION IAW SRM 51-74-00. ORIG MAT. 0.100 DAMAGE DIM. L=1.0 INCH W=0.7 INCH D=0.030 INCH. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14. REMOVED AND REPLACED FLOOR SUPPORTJun 27, 2012 · N328NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002533128Seat Track · corrodedSEAT TRACK AT Y1292 BETWEEN FR 41 TO FR 47 CORRODED OUT OF LIMITS IN 2 LOCATIONS. REMOVED AND REPLACED SEAT TRACK AT Y1292 FR41-FR47 IAW SRM 51-42-11 IAW A319 SRM 51-23-12. DAMAGE DIM: ORIG. MAT=.140 INCH L=.800 INCH W=.100 D=.015.Jun 27, 2012 · N328NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA12002523128Sill · corrodedAFT UTILITY L2 DOOR SILL Y1732 ABOVE FR 68 HAS 3 AREAS WITH CORROSION. REMOVED CORROSION IAW SRM 51-74-00. AFTER REWORKED AREA, DIMENSIONS AREA: L=1.2 INCH W=0.800 INCH D=0.030 INCH. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14 FIG 101. REMOVED AND REPLACED Jun 27, 2012 · N328NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002513128Floor Support · corrodedAFT UTILITY FLOOR SUPPORT Y765 HAS 6 AREAS WITH CORROSION BETWEEN FR 66 AND FR70. REMOVED CORROSION IAW SRM 51-74-00. CHECKED LIMITS L=1.0 INCH W=0.80 INCH D=0.030 INCH. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14 FIG 102. MAXIMUM ALLOWABLE DEPTH OF 0.016 INJun 27, 2012 · N328NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002583128Floor Support · corrodedAFT UTILITY FLOOR SUPPORT -Y765 HAS 3 AREAS WITH CORROSION BETWEEN FR 64 AND FR 66. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-44-11, 51-42-11. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. DAMAGE DIMENSIONS: L=1.8 W=1.2 D=.030 ORIG MAT THICKNESS = .087.Jun 26, 2012 · N328NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002503128Floor Panel · damagedAFT CARGO FLOOR PANEL 151ZG MISSING INSERTS. FABRICATED FLOOR PANEL IAW DWG 3D25-40532. DAMAGE DIM L=1.0 INCH W=1.0 INCH.Jun 26, 2012 · N328NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12002493128Floor Panel · damagedAFT CARGO FLOOR PANEL 151PE DELAMINATED. FABRICATED FLOOR PANEL IAW DWG 3D25-40532. DAMAGE DIM L=6.0 INCH W=3.0 INCH.Jun 26, 2012 · N328NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12002483128Floor Panel · damagedAFT CARGO FLOOR PANEL 151VG DELAMINATED. FABRICATED FLOOR PANEL IAW DWG 3D25-40532. DAMAGE DIM. L=4.0 INCH W=2.0 INCH.Jun 26, 2012 · N328NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12002473128Floor Panel · damagedFORWARD CARGO FLOOR PANEL 131AF DAMAGED. FABRICATED FLOOR PANEL IAW DWG 3D25-40532. DAMAGE DIM L=2.0 INCH W=1.0 INCH.Jun 26, 2012 · N328NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12002463128Floor Panel · damagedFORWARD CARGO SLOPE FLOOR PANEL 131CG DAMAGED. FABRICATED SLOPE PANEL IAW DWG 3D25-40532. DAMAGE DIM L=2.0 INCH W=1.0 INCH.Jun 26, 2012 · N328NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12002453128Floor Support · corrodedAFT UTILITY FLOOR SUPPORT Y512 HAS 1 AREA WITH CORROSION ABOVE FR 68. REMOVED DAMAGED FLOORBEAM AT Y512 FR68 - FR70 IAW SRM 51-42-11. INSTALLED NEW FLOOR SUPPORT AT Y512 FR68-FR70 IAW SRM 51-42-11.Jun 26, 2012 · N328NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002443128Floor Support · corrodedAFT UTILITY FLOOR SUPPORT -Y765 HAS 6 AREAS WITH CORROSION BETWEEN FR66 AND FR68. REMOVED CORROSION IAW A319 SRM 51-74-00, CHECK LIMIT L=2.0 INCH W=0.60 INCH D=0.73 INCH FOUND OUT OF LIMIT IAW A319 SRM 53-41-15. REMOVED AND REPLACED FLOOR SUPPORT AT -Y765, FJun 26, 2012 · N328NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002433128Fitting · corrodedAFT UTILITY L2 DOOR SILL AFT SEAL SHAPER HAS CORROSION. BLENDED AREA IAW A319 SRM 51-74-00, DIM OF BLEND OUT AREA L=1.5 INCH W=0.5 INCH D=0.031 INCH, NO ALLOWABLE LIMITS FOUND. REMOVED AND REPLACED CORNER FITTING AT FR68 IAW SRM 51-42-11.Jun 26, 2012 · N328NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002423128Sill · corrodedL2 PAX DOOR CENTER SHAPE SILL AFT FASTENER HOLE HAS CORROSION. BLENDED AREA IAW SRM 51-44-00, DIM OF BLEND OUT AREA L=1.0 INCH W=0.40 INCH D=0.020 INCH. NO ALLOWABLE LIMITS FOUND. REMOVED AND REPLACED CENTER SHAPE SILL IAW SRM 51-42-11.Jun 26, 2012 · N328NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002413128Attach Fitting · corrodedAFT UTILITY R2 DOOR SILL FWD GIRT BAR FITTING ATTACH AREA HAS CORROSION AROUND 9 FASTENER HOLES. REMOVED CORROSION IAW A319 SRM 51-74-00 CHECK LIMITS L=.600 INCH W=1.0 INCH D=0.075 INCH. FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-41-14 FIG 101. REMOVED AND RJun 25, 2012 · N328NB · Airbus A319114 · Fuselage Main, Attach FittingsSDR DALA12002363128Floor Support · corrodedFORWARD MAIN CABIN FLOOR SUPPORT BET FR 20 AND FR 23-Y765 HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00, L=1.0 INCH W=.3 INCH D=.038 INCH. FOUND OUT OF LIMITS IAW SRM 53-00-15 FIG 101. REMOVED AND REPLACED FLOOR SUPPORT FROM FR 12 TO FR24 -Y765 IAW SRM Jun 25, 2012 · N328NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002243128Panel · damagedAFT CARGO SLOPE PANEL 152TG DELAMINATED. FABRICATED NEW SLOPE PANEL 152TG PER DWG 3D25-40532. DAMAGE DIM: 8.0 BY 4.0.Jun 25, 2012 · N328NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002233128Panel · damagedAFT CARGO SLOPE PANEL 151UG DELAMINATED. FABRICATED NEW SLOPE PANEL 151UG PER DWG 3D25-40532. DAMAGE DIM: 8.0 BY 3.0.Jun 25, 2012 · N328NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002223128Panel · damagedAFT CARGO SLOPE PANEL 152WG DELAMINATED. FABRICATED NEW SLOPE PANEL 152WG PER DWG 3D25-40532. DAMAGE DIM: 12.0 BY 4.0.Jun 25, 2012 · N328NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002213128Panel · damagedAFT CARGO SLOPE PANEL 151TG DELAMINATED. FABRICATED NEW SLOPE PANEL 151TG PER DWG 3D25-40532. DAMAGE DIM: 12.0 BY 3.0.Jun 25, 2012 · N328NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002203128Panel · damagedAFT CARGO SLOPE PANEL 151DE DELAMINATED. FABRICATED NEW SLOPE PANEL 151DE PER DWG 3D25-40532. DAMAGE DIM: 3.0 BY 4.0.Jun 25, 2012 · N328NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002193128Panel · damagedAFT CARGO SLOPE PANEL 151BE DELAMINATED. FABRICATED NEW SLOPE PANEL 151BE PER DWG 3D25-40532. DAMAGE DIM: 12.0 BY 5.0.Jun 25, 2012 · N328NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002183128Panel · damagedAFT CARGO SLOPE PANEL 151AE DELAMINATED. FABRICATED NEW SLOPE PNL 151AE PER DWG 3D25-40532. DAMAGE DIM, 4.0 BY 4.0.Jun 25, 2012 · N328NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002173128Panel · damagedFORWARD CARGO SLOPE PANEL 131DG DAMAGED AND DELAMINATED. FABRICATED NEW SLOPE PANEL 131DG PER DWG 3D25-40532. DAMAGE DIM: 3.0 BY 1.0.Jun 25, 2012 · N328NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12002163128Floor Panel · damagedCOCKPIT FLOOR PANEL 221LF DAMAGED. REPLACED FLOOR PANEL WITH NEW IAW SRM 51-72-11. DAMAGE DIM: 4.0 INCH BY 3.0 INCH.Jun 25, 2012 · N328NB · Airbus A319114 · Fuselage Floor Panel
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