N323NB

Service difficulty reports · 259

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 = 'N323NB' 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 DALA2016092706915Connector · miswiredAFT LAV EMERGENCY EXIT SIGN INOPERATIVE. WIRES AT CONNECTOR 9164VC SWAPPED, REPOSITIONED WIRES TO CORRECT LOCATIONSSep 24, 2016 · N323NB · Airbus A319114 · Light System WiringSDR DALA2016041102796Door Frame · crackedLT EMERGENCY EXIT DOOR, FWD EDGE, FRAME SEGMENT CRACK AT RIVET. HFEC FRAME IAW NTM 51-10-08, FOUND CRACK AS MARKED, REMOVED CRACK FRAME.Apr 2, 2016 · N323NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2018040102168Stringer · corrodedDURING INSPECTION OF AFT CARGO ABOVE ATG ANTENNA, FOUND CORROSION ON STRINGER 44L BETWEEN FRAMES 59 AND 60. REMOVED THE CORROSION IAW SRM 53-00-13, FIG 202, SHEET 4. INSTALLED A STRINGER REPAIR IAW SRM 53-00-13, FIG 202, SHEET 3.Jul 20, 2014 · N323NB · Airbus A319114 · Fuselage Main, Longeron/StringerSDR DALA2018040102167Stringer · corrodedINSPECTION OF AFT CARGO ABOVE ATG ANTENNA, FOUND CORROSION ON STRINGER 43L BETWEEN FRAMES 59 AND 60. REMOVED THE CORROSION IAW SRM 53-00-13, FIG 202, SHEET 4. INSTALLED A STRINGER REPAIR IAW SRM 53-00-13, FIG 202, SHEET 3.Jul 20, 2014 · N323NB · Airbus A319114 · Fuselage Main, Longeron/StringerSDR DALA2014070603875Wire · disconnectedEMERGENCY ESCAPE LIGHT INOPERATIVE AT ROW 11. CONNECTED PIN AT LIGHT ASSY. OPS CHECKED GOOD, OK FOR SERVICE.Jun 28, 2014 · N323NB · Airbus A319114 · Light System WiringSDR DALA14031683123Bulb · inoperativeEMERGENCY LIGHT INOPERATIVE. INSTALLED NEW BULB AND MODULE IAW AMM 33-50. OPS CHECKED NORMAL.May 20, 2014 · N323NB · Airbus A319114 · Emergency LightingSDR DALA13009343123Pin · detachedR1 DOOR PIN DETACHED FROM LANYARD. ATTACHED LANYARD TO PIN. OPS CHECKED IS NORMAL.Feb 22, 2013 · N323NB · Airbus A319114 · Passenger/Crew DoorsSDR DALA12004863123Light · inoperativeDURING SERVICE CHECK, FOUND ROW 16 EMERGENCY LIGHTING INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY FOR ROW 16 IAW AMM 33-50. OPS CHECKED GOOD. OK FOR SERVICE.Aug 4, 2012 · N323NB · Airbus A319114 · Emergency LightingSDR DALA12001613123Fitting · corrodedMAIN CABIN AFT UTILITY AREA, R2 DOOR SILL AFT AND FWD GIRT BAR FITTING AREA CORRODED AROUND HOLES. REPAIRED IAW TRM 53-41-14.Jun 13, 2012 · N323NB · Airbus A319114 · Fuselage Main, Attach FittingsSDR DALA12001483123Sill · corrodedFORWARD UTILITY RIGHT PASSENGER DOOR SILL HAS PITTING UNDER FWD GIRT BAR FITTING AREA. ACCOMPLISHED REPAIR IAW ER/A 502571-14, FUSELAGE/RT FWD DOOR SILL/GIRT BAR ATTACH POINTS/CORRODED. SECTION I-PERMANENT REPAIR. SECTION II-INSPECTION METHOD/INTERVALS AT EJun 8, 2012 · N323NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12001473123Sill · corrodedFORWARD LEFT PASSENGER DOOR SILL HAS CORROSION AROUND OUTBOARD AFT FASTENER HOLE FOR FORWARD GIRT BAR FITTING. ACCOMPLISHED REPAIR IAW ER/A 502572-14, FUSELAGE/LT FWD DOOR SILL/GIRT BAR ATTACH POINTS/CORRODED. SECTION I-PERMANENT REPAIR. SECTION II-INSPECTIJun 8, 2012 · N323NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12001463123Sill · corrodedFORWARD UTILITY LEFT PASSENGER DOOR SILL HAS CORROSION AROUND INBD FORWARD FASTENER HOLE FOR AFT GIRT BAR FITTING. ACCOMPLISHED REPAIR IAW ER/A 502572-14, FUSELAGE/LT FWD DOOR SILL/GIRT BAR ATTACH POINTS/CORRODED, SECTION I-PERMANENT REPAIR. SECTION II-INSPEJun 8, 2012 · N323NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12001173123Floor Panel · damagedFORWARD UTILITY FLOOR PANEL 232DF DAMAGED AROUND FASTENER HOLES. FABRICATED FLOOR PANEL IAW DWG 3D25-40640. DAMAGE DIM: L=12 INCH W=1INCH D=.040 INCH.May 31, 2012 · N323NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12001163123Floor Panel · damagedMID CABIN FLOOR PANEL 231MF OUTER FLY TORN. FABRICATED FLOOR PANEL IAW DWG 3D25-40640. DAMAGE DIM: L=.62" W=19" D=.100".May 30, 2012 · N323NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12001153123Floor Panel · crackedAFT CABIN UTILITY FLOOR PANEL 261EF HAS CRACK. FABRICATED FLOOR PANEL 261EF IAW A319 DWG 3D25-40640. DAMAGE DIM: L=.100 W=.50 D=.100.May 30, 2012 · N323NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12001123123Floor Panel · damagedFORWARD CARGO COMPARTMENT SLOPING FLOOR PANEL 131DG TORN. FABRICATED SLOPING FLOOR PANEL.May 30, 2012 · N323NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12001113123Floor Panel · puncturedFORWARD CARGO COMPARTMENT SLOPING FLOOR PANEL 131BF PUNCTURED NEAR FASTENER HOLE. FABRICATED SLOPING FLOOR PANEL 131BF.May 30, 2012 · N323NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12001103123Floor Panel · damagedAFT PIT FLOOR PANEL 151BE DAMAGE. FABRICATED FLOOR PANEL.May 30, 2012 · N323NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12001093123Floor Panel · damagedAFT PIT FLOOR PANEL 152TG DAMAGED. FABRICATED FLOOR PANEL.May 30, 2012 · N323NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12001083123Floor Panel · damagedAFT PIT FLOOR PANEL 151UG DAMAGED. FABRICATED FLOOR PANEL.May 30, 2012 · N323NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12001073123Floor Panel · damagedAFT PIT FLOOR PANEL 151CE DAMAGED. FABRICATED FLOOR PANEL.May 30, 2012 · N323NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12001063123Floor Panel · damagedAFT PIT FLOOR PANEL 151AE DAMAGED. FABRICATED FLOOR PANEL 151AE.May 30, 2012 · N323NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12001053123Floor Panel · damagedAFT PIT FLOOR PANEL 161BF DAMAGED. FABRICATED FLOOR PANEL.May 30, 2012 · N323NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12001003123Floor Panel · delaminatedAFT CABIN UTILITY FLOOR PANEL 261AG IS DELAMINATED. FABRICATED FLOOR PANEL.May 30, 2012 · N323NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12000993123Floor Panel · damagedFORWARD CARGO COMPARTMENT FLOOR PANEL 132DG TORN. FABRICATED FLOOR PANEL.May 30, 2012 · N323NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12000983123Floor Panel · damagedAFT PIT FLOOR PANEL 151GE DAMAGE. FABRICATED FLOOR PANEL.May 30, 2012 · N323NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12000973123Floor Panel · damagedAFT PIT FLOOR PANEL 151ZG DAMAGE. FABRICATED FLOOR PANEL.May 30, 2012 · N323NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12000903123Floor Panel · damagedAFT PIT FLOOR PANEL 151VG DAMAGE INSERTS. FABRICATED NEW FLOOR PANEL.May 26, 2012 · N323NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12000833123Seat Track · corrodedFORWARD UTILITY DUMMY RAIL -Y765 HAS CORROSION ON SEAT TRACK CROWN ABOVE FR20. BLENDED AREA. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK.May 25, 2012 · N323NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA12000823123Web · crackedMAIN CABIN AFT UTILITY AREA BETWEEN FR68-FR69, BETWEEN ST -Y1292 AND ST -Y1732 TRAY WEB HAS CRACKED. REMOVED AND REPLACED AFT CABIN UTILITY TRAY WEB IAW SRM 51-42-11. CRACK DIMENSION 6.5 INCH.May 25, 2012 · N323NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12000793123Floor Panel · corrodedMAIN CABIN FLOOR PANEL 222FF IS CORRODED. REPLACED FLOOR PANEL WITH NEW IAW SRM 51-72-11.May 25, 2012 · N323NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12000783123Floor Panel · corrodedMAIN CABIN FLOOR PANEL 262FF HAS CORROSION. REPLACED FLOOR PANEL WITH NEW IAW SRM 51-72-11.May 25, 2012 · N323NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12000723123Sill · corrodedMAIN CABIN AFT UTILITY AREA L2 DOOR SILL FWD AND AFT GIRT BAR FITTING AREA CORRODED AROUND HOLES AS MARK. REMOVED CORROSION FOUND OUT OF LIMITS IAW SRM 53-41-14. REMOVED AND REPLACED DOOR SILL IAW SRM 51-42-11, DAMAGE DIMENSION L=1.2 INCH W=0.8 D=0.017 INCH.May 24, 2012 · N323NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12000713123Sill · corrodedMAIN CABIN L2 DOOR AFT SHAPE SILL HAS CORROSION. REMOVED CORROSION L=1.7 INCH W=0.7 INCH D=0.031 INCH. NO LIMITS FOUND ON SRM. REMOVED AND REPLACED AFT SHAPE SILL IAW SRM 51-42-11.May 24, 2012 · N323NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12000703123Sill · corrodedLEFT AFT DOOR CENTER SHAPE SILL CORRODED. REMOVED CORROSION L=3.3 INCHES W=0.55 INCH D=0.016 INCHES. NO LIMITS FOUND ON SRM. REMOVED AND REPLACED CENTER SHAPE SILL IAW SRM 51-42-11.May 24, 2012 · N323NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12000323123Sill · corrodedMAIN CABIN R2 DOOR AFT SHAPE SILL HAS CORROSION. REMOVED CORROSION IAW A319 SRM 51-74-00, DIMENSIONS OF BLENDED AREAS L=1.14 INCH W=1.10 INCH D=.019 INCH, NO ALLOWABLE DAMAGE FOUND. REMOVED AND REPLACED FITTING CORNER IAW A319 SRM 51-42-11.May 23, 2012 · N323NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12000283123Floor Support · corrodedMAIN CABIN AFT UTILITY AREA BTW FR 67-FR 68Y765 FLOOR SUPPORT CORRODED. BLENDED FLOOR SUPPORT Y765 FR 67-68 IAW SRM 51-74-00, MAX DEPTH OF REWORK OF NOMINAL THICKNESS .016 MATERIAL LOSE .021, OUT OF LIMITS IAW SRM 53-00-14 FIG 102. LOCATED AND DRILLED NEW FLMay 23, 2012 · N323NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12000273123Floor Support · corrodedMAIN CABIN AFT UTILITY AREA BTW FR 67-FR 68Y765 FLOOR SUPPORT CORRODED. BLENDED FLOOR SUPPORT Y765 FR 67-68 IAW SRM 51-74-00, MAX DEPTH OF REWORK OF NOMINAL THICKNESS .016 MATERIAL LOSE .021. OUT OF LIMITS IAW SRM 53-00-14 FIG 102. LOCATED AND DRILLED NEW FMay 23, 2012 · N323NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12000253123Dummy Rail · corrodedFORWARD UTILITY DUMMY RAIL -Y1292 HAS CORROSION ON SEAT TRACK CROWN AFT OF FR 20. BLENDED AREA IAW SRM 51-74-00. ORIG MAT. 0.150 DAMAGE DIM. L=.500 W.300 D=.075. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-15 FIG 101. REMOVED AND REPLACED SEAT TRACK IAW SRM 51May 23, 2012 · N323NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA12000243123Floor Support · corrodedMAIN CABIN AFT UTILITY AREA BTW FR65 - FR66 ST Y765 FLOOR SUPPORT CORRODED. BLENDED FLOOR SUPPORT Y765 FR 65-66 IAW SRM 51-74-00. ORIG MAT. 0.125 DAMAGE DIM. L=1.5 INCH W=1.0 INCH D=0.040 INCH. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14. LOCATED AND DRILLEMay 23, 2012 · N323NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12000233123Dummy Rail · corrodedFORWARD UTILITY DUMMY RAIL -Y189 CORRODED ABOVE SSI 531189. REMOVED AND REPLACED DUMMY RAIL AT -Y189 IAW SRM 51-42-11. FOUND TO BE OUT OF LIMITS AFTER BLENDING IAW SRM 51-74-00,L=1.5 W=1.75 D=.066.May 22, 2012 · N323NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA12000183123Seat Track · corrodedFORWARD UTILITY DUMMY RAIL Y503.2, EXFOLIATED ABOVE FR 16. REMOVED AND REPLACED DUMMY RAIL IAW SRM 51-42-11.May 21, 2012 · N323NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA12001033123Floor Panel · puncturedAFT CARGO COMPARTMENT FLOOR PANEL 152XG PUNCTURED. FABRICATED FLOOR PANEL.May 20, 2012 · N323NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12001323123Structure · corrodedFORWARD UTILITY AREA RIGHT PASS DOOR CENTER SEAL SHAPER HAS CORROSION AROUND FASTENER HOLE NUT PLATES. BLENDED CORROSION L:0.085 INCH W:0.123 INCH D:0.032 INCH. NO LIMITS FOUND IN SRM. REMOVED AND REPLACED R1 CENTER SEAL SHAPER IAW A319 SRM 51-42-11.May 17, 2012 · N323NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12001023123Floor Panel · corrodedAFT CABIN FLOOR PANEL 262EF CORRODED. FABRICATED FLOOR PANEL.May 17, 2012 · N323NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12000893123Floor Support · corrodedMAIN CABIN AFT UTILITY AREA FLOOR SUPPORT BETWEEN FR66-FR68 ST-Y1292 SEVERAL PLACES CORRODED. BLENDED CORROSION. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT.May 17, 2012 · N323NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12000883123Floor Support · corrodedMAIN CABIN AFT UTILITY AREA FLOOR SUPPORT BETWEEN FR65-FR66 ST-Y1292 SEVERAL PLACES CORRODED. REMOVED CORROSION IAW A319 SRM 51-74-00. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT.May 17, 2012 · N323NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12000873123Floor Support · corrodedMAIN CABIN UTILITY AREA FLOOR SUPPORT BETWEEN FR 68-FR 69 ST-Y1292 HAS CORROSION. REMOVED CORROSION IAW A319 SRM 51-74-00. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORTMay 17, 2012 · N323NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12000863123Floor Support · corrodedMAIN CABIN AFT UTILITY AREA BETWEEN FR68-FR69 ST Y1292 FLOOR SUPPORT CORRODED. BLENDED CORROSION IAW A319 SRM 51-74-00. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT.May 17, 2012 · N323NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12000853123Floor Support · corrodedMAIN CABIN AFT UTILITY AREA BETWEEN FR65-FR66 ST Y1292 FLOOR SUPPORT CORRODED. BLENDED CORROSION IAW A319 SRM 51-74-00, FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT IAW A319 SRM 51-42-11.May 17, 2012 · N323NB · Airbus A319114 · Fuselage Miscellaneous Structure
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