N302NB

Service difficulty reports · 149

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 = 'N302NB' 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 DALA2018072504737Floorbeam · corrodedCORROSION FLOORBEAM Y1132 LOCATED BETWEEN FR68 TO FR69 AT AFT GALLEY AREA. REPLACED FLOOR BEAM IAW STR 51-72-11 AND DWG D53472780.Jul 24, 2018 · N302NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA2018022001005Battery Pack · dischargedWHILE PERFORMING EMERGENCY LIGHT CHECK RECEIVED 'EPSU BATTERY LEFT' INOP, REPLACED LEFT EPSU BATTERY PACK.Feb 19, 2018 · N302NB · Airbus A319114 · Emergency LightingSDR DALA2017091006813Battery Pack · inoperativeEMERGENCY BATTERY FAULT ON LIGHT TEST, REPLACED BATTERY PACK.Sep 8, 2017 · N302NB · Airbus A319114 · Emergency LightingSDR DALA2017041403017Lens · unsecureSEAT 1C MOUNTED EMERGENCY LIGHT LENS LOOSE. SECURED THE LENS.Apr 13, 2017 · N302NB · Airbus A319114 · Emergency LightingSDR DALA2016062805030Stringer · corrodedAFT CARGO COMPARTMENT UNDERFLOOR AREA, BETWEEN FRAME 54 - FRAME 55, STR 42L, CORROSION AROUND FASTENERS. INSTALLED REPAIR ANGLE AND FILLER IAW SRM 51-42-11 AND SRM 53-00-13, FIG 202.Jun 27, 2016 · N302NB · Airbus A319114 · Fuselage Main, Longeron/StringerSDR DALA2016111808960Floor Support · corrodedFWD CABIN FLOOR SUPPORT AT Y-1379 BETWEEN FRAMES 15A AND 16, TOP SURFACE HAS CORROSION. REMOVED AND REPLACED THE FLOOR SUPPORT.Jun 23, 2016 · N302NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2016111808961Fitting · corrodedRT FWD DOOR SILL PLATE UPPER SURFACE UNDER AFT GIRT BAR FITTING, AREA AROUND MOUNTING BOLTS HAS OUT OF LIMITS CORROSION. REMOVED AND REPLACED R1 DOOR SILL FITTING.Jun 22, 2016 · N302NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2016062204844Floor Support · corrodedFORWARD CABIN FLOOR SUPPORT LONGERON Y765 BETWEEN FRAME 16 AND FRAME 20 TOP SURFACE HAS 3 AREAS CORRODED. R & R FLOORBEAM, Y765 FROM FRAME 12 TO FRAME 24, IAW SRM 51-42-11.Jun 21, 2016 · N302NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2016062204843Seat Track · corrodedSEAT TRACK, -Y1292 AT FRAME 20 HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-15, FIG 102. R & R SEAT TRACK.Jun 21, 2016 · N302NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016062104842Web · corrodedFORWARD CABIN FLOOR STRUCTURE AT FRAME 20, Y-1732, FORWARD END TOP SURFACE CORRODED. LOCATED AND DRILLED IAW SRM 51-42-12. INSTALLED NEW FWD CABIN FLOOR STRUCTURE WEB AT FRAME 20, Y-1732 IAW SRM 51-42-11.Jun 20, 2016 · N302NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2016062104841Door Sill · corrodedR2 DOOR SILL FORWARD LEG HAS CORROSION. REMOVED DAMAGE IAW SRM 51-73-00. FOUND TO OUT OF LIMITS IAW SRM 53-41-14. PERFORMED REPAIR IAW SRM 53-41-14, FIG 201, SHEET 4.Jun 20, 2016 · N302NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2016062104840Floorboard · corrodedFORWARD FLOORBOARD 221FF, BOTTOM SKIN HAS CORROSION. REPLACED FORWARD CABIN FLOORBOARD 221FF.Jun 20, 2016 · N302NB · Airbus A319114 · Fuselage Floor PanelSDR DALA2016062104839Support · corrodedLEFT AFT CABIN FLOOR AREA BN FRAME 69-70 SHEAR PLATE SUPPORT PLATE HAS CORROSION. R & R LT AFT CABIN SHEAR PLATE SUPPORT, FRAME 69-70 IAW SRM 51-42-11,51-44-11.Jun 20, 2016 · N302NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2016062104838Floor Support · corrodedFORWARD CABIN FLOOR SUPPORT LONGERON AT Y-254 BETWEEN FRAME 12 AND FRAME 21 HAS 4 AREAS CORRODED. CORRODED FLOOR SUPPORT R & R IAW SRM 51-42-11.Jun 20, 2016 · N302NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2016062004847Floorbeam · corrodedLEFT FLOORBEAM Y765 HAS 2 SPOTS OF CORROSION. REMOVED CORROSION IAW SRM 51-74-00, FOUND TO BE OUT OF LIMITS. R & R FLOORBEAM.Jun 18, 2016 · N302NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA2016062004846Floor Support · corrodedFWD CABIN FLOOR SUPPORT LONGERON, Y254 BETWEEN FR18 AND FR21 TOP SURFACE HAS 6 AREAS CORRODED. AFTER INVESTIGATION FOUND FLOOR SUPPORT OUT OF LIMITS. R & R FLOOR SUPPORT.Jun 18, 2016 · N302NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2016062004845Seat Track · corrodedSEAT TRACK, Y765 AT FRAME 20 HAS CORROSION. REMOVED CORROSION AND FOUND OUT OF LIMITS. R & R SEAT TRACK.Jun 17, 2016 · N302NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016061704743Floor Support · corrodedFORWARD CABIN FLOOR SUPPORT LONGERON Y-190 BETWEEN FRAME 21 AND FRAME 22 HAS 2 AREAS CORRODED. CHECKED LIMITS IAW SRM 53-11-14, OUT OF LIMITS. R & R TRACKS IAW SRM 51-42-11 AND TRM 53-21-01.Jun 16, 2016 · N302NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2016061704742Floor Support · corrodedFWD CABIN FLOOR SUPPORT LONGERON Y503.2 CORRODED BETWEEN FRAME 12 AND FRAME 16 HAS CORROSION. REPLACED IAW TRM 53-21-01, SRM 51-42-11. THERE IS NO DAMAGE LIMITS FOR THIS AREA IAW SRM 53-00-14.Jun 16, 2016 · N302NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2016061604741Floorbeam · corrodedAT FR69, Y-1292 FLOORBEAM HAS CORROSION, FOUND TO BE OUT OF LIMITS, D=0.030", IAW TRIM 53-41-15, REPLACED WITH NEW STOCK, PN D5347218920400, IAW TRM 53-41-15.Jun 15, 2016 · N302NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA2016061404740Floorbeam · corrodedAT FRAME 70 FLOORBEAM, Y-765, HAS CORROSION AROUND FASTENER HOLE. REMOVED CORROSION AND WAS FOUND TO BE OUT OF LIMITS, REPLACED IAW TRM 53-41-15. D=0.050", PN D5347219320000, Y-765.Jun 13, 2016 · N302NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA2016060804437Support Frame · corrodedAFT CABIN FLOOR RT SHEAR PLATE SUPPORT FRAME CORRODED. LOCATION BET FRAME 69 AND FRAME 70 -Y1170. FOUND TO BE OUT OF LIMITS, MORE THAN 50 PERCENT MATERIAL LOSS. REPLACED SHEAR SUPPORT FRAME BETWEEN FRAME 69 AND FRAME 70, Y117 AS REQUIRED IAW SRM 31-41-14 ANDJun 7, 2016 · N302NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2015112807274Wire Harness · damagedF/A REPORTED SPARKS EMINATING FROM DOOR 2R EXIT SIGN DURING TAXI OUT RETURNED TO GATE. CHAFED WIRES. REPLACED HARNESS 7244VC CONNECTOR TO 44WL SIGN EXIT MARKING OF DOOR 2RT.Nov 27, 2015 · N302NB · Airbus A319114 · Light System WiringSDR DALA2015110106666Wire · damagedEMERGENCY LIGHT ON SEAT 10C INOPERATIVE, REPAIRED WIRING.Oct 31, 2015 · N302NB · Airbus A319114 · Light System WiringSDR DALA2014080704343Engine · malfunctionedFLIGHT 1343, DURING APPROACH, NR 1 ENGINE SHUT ITSELF DOWN. INLET AND EXHAUST ON INITIAL LOOKED OK. FOUND NR 1 FUEL CONTROL FAULT WAS STILL PRESENT. ALSO, FOUND NR 1 FIRE BOTTLE NR 2 WAS DISCHARGED BY FLIGHT CREW. R & R HMU, ECU AND FIRE BOTTLE AND DISCHARGAug 5, 2014 · N302NB · Airbus A319114 · Engine (Turbine/Turboprop)SDR DALA13021423102Battery Pack · inoperativeBATTERY PACKS FOR THE EPSU INOPERATIVE. R & R BATTERY PACKS IAW MM 33-51. CHECKED OK.May 6, 2013 · N302NB · Airbus A319114 · Emergency LightingSDR DALA12013513102Connector · inoperativeEMERGENCY LIGHT AT SEAT 20 ABC INOPERATIVE. REPLACED CONNECTOR. OPS CHECKED GOOD. OK FOR SERVICE.Nov 21, 2012 · N302NB · Airbus A319114 · Light System WiringSDR DALA1149603102Slat · dentedON PRE FLT FOUND LARGE DENT IN LEADING EDGE OF RT WING BETWEEN RT ENG & WING ROOT. PERF INSP PER ENGINEERING. APPLIED SPEED TAPE. PER ERA 495515-14 FOLLOW UP WORK IS REQ ON THE RIGHT WING NR 1 SLAT L/E. SECT II TIME LIMITED REPAIR NTE 7 DAYS FROM 20AUG11. Aug 20, 2011 · N302NB · Airbus A319114 · Leading Edge DevicesSDR DALA1125713102Light · inoperativeDURING NON ROUTINE CHECK, FOUND THE EMERGENCY LIGHT AT ROW 16ABC INOPERATIVE. MX SECURED EMERGENCY LIGHT ASSY AND FUNCTIONAL CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.Apr 11, 2011 · N302NB · Airbus A319114 · Emergency LightingSDR DALA1022703102Skin · dentedDURING M-CHECK FOUND DENT ON FUSELAGE SKIN BETWEEN FRAMES 24-25 STRINGER 42R TO STRINGER 41R. REPAIRED IAW SRM 53-21-11, SRM 51-75-15 & SRM 51-42-11. REPAIR MUST BE INSPECTED AT 60,000 FLIGHT CYCLES IAW SRI 53-21-11.Sep 14, 2010 · N302NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA1022103102Door Frame · corrodedDURING M-CHECK FOUND CORROSION ON DOOR R1 DOOR FRAME 20 AT CABIN FLOOR LINE. REPAIRED IAW NTM 51-10-08, NTM 51-10-02. INDENTIFIED REPAIR AS ENGINEERING APPROVED TIME LIMITED REPAIR IAW ERA 484247-14 SECTION I. INSP TO BE ACCOMPLISHED EVERY 500 FLIGHT CYCLES Sep 11, 2010 · N302NB · Airbus A319114 · Fuselage Main, StructureSDR DALA1022123102Floorbeam · corrodedDURING M-CHECK FOUND CORROSION ON CABIN FLOORBEAM AT +Y1292 FR68. REPAIRED IAW SRM 51-42-11, SRM 51-44-11.Sep 10, 2010 · N302NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA1022113102Floorbeam · corrodedDURING M-CHECK FOUND CORROSION ON CABIN FLOORBEAM AT +Y1292 FR66. REPAIRED IAW SRM 51-42-11, SRM 51-44-11.Sep 10, 2010 · N302NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA1021953102Floor Panel · delaminatedDURING M-CHECK FOUND CARGO FLOOR PANEL 131AF IS DELAMINATED. REPLACED FLOOR PANEL 161PF IAW DWG 3D25-40532.Sep 9, 2010 · N302NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1021943102Floor Panel · delaminatedDURING M-CHECK, FOUND CARGO FLOOR PANEL 161PF IS DELAMINATED. REPLACED FLOOR PANEL 161PF IAW DWG 3D25-40532.Sep 9, 2010 · N302NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1021933102Floor Support · corrodedDURING M-CHECK FOUND CORROSION ON LT FLOOR SUPPORT AT +Y254 FR16-FR20. REPAIRED IAW SRM 51-44-11, SRM 51-42-11.Sep 9, 2010 · N302NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1021733102Attach Fitting · corrodedDURING M-CHECK FOUND CORROSION ON FRAME CLIP IN FWD CARGO COMPARTMENT AT FR30 BETWEEN STRINGER 41R AND STRINGER 42R. REPAIRED IAW SRM 51-44-11, SRM 51-21-11 & SRM 51-42-11.Sep 8, 2010 · N302NB · Airbus A319114 · Fuselage Main, Attach FittingsSDR DALA1021233102Floor Support · corrodedDURING M-CHECK FOUND CORROSION ON RT FLOOR SUPPORT AT Y254 FR20. REPAIRED IAW SRM 51-44-11, SRM 51-42-11.Sep 6, 2010 · N302NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1021213102Support · corrodedDURING M-CHECK FOUND CORROSION ON R2 DOOR LOWER SILL SUPPORT AT Y1732 FR66. REPAIRED IAW SRM 51-42-11, SRM 51-44-11.Sep 4, 2010 · N302NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1021223102Support · corrodedDURING M-CHECK FOUND CORROSION ON L2 DOOR LOWER SILL SUPPORT AT Y1732 FR 66. REPAIRED IAW SRM 51-42-11, SRM 51-44-11.Sep 3, 2010 · N302NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1021203102Support · corrodedDURING M-CHECK, FOUND CORROSION ON FLOORBEAM SUPPORT AT +Y765 FR66. REPAIRED IAW SRM 51-42-11.Sep 3, 2010 · N302NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA1021153102Seat Track · corrodedFWD CABIN RT SEAT TRACK -Y1292 CORRODED FROM FR 19 TO FR21. SSI 531151. REMOVED CORROSION FROM SEAT TRACK -Y1292 FR21 IAW SRM 51-74-00. DIM. L=.500 W=.650 D=.045 FOUND OUT OF LIMITS IAW SRM 53-00-15. REMOVED SEAT TRACK IAW SRM 51-42-11.LOCATED, DRILLED, AND INSep 2, 2010 · N302NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1021143102Seat Track · corrodedFWD CABIN RT SEAT TRACK -Y765 CORRODED FR20-21. REMOVED CORROSION IAW SRM 51-74-00, ORIGINAL THICKNESS .087 MAT LOSS .070, L=1.5" W=1" D=.065" IS OUT OF LIMITS IAW TRM 53-00-15. R & R SEAT TRACK IAW SRM 51-42-11.Sep 2, 2010 · N302NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1020983102Floor Support · corrodedCABIN FLOOR LONGITUDINAL BEAM AT FR66 -Y765 HAS CORROSION. REMOVED SEAT TRACK -Y765 BETWEEN FR 66 TO 64. (NOT FR66 TO 68).Sep 1, 2010 · N302NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1021053102Seat Track · corrodedCABIN FLOOR LONGITUDINAL BEAM AT FR66 -Y765 HAS CORROSION. LOG PAGE NR 0264321. REMOVED SEAT TRACK -Y765 BETWEEN FR 66 TO 64. (NOT FR66 TO 68)Sep 1, 2010 · N302NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1020903102Floor Support · corrodedCABIN FLOOR LONGITUDINAL BEAM AT FR 66, Y512 HAS CORROSION. REMOVED DAMAGED FLOORBEAM AT FR 66, Y512 DAMAGED AREA DIM ARE W=0.50" D=0.24" L=1.5" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14. INSTALLED NEW FLOORBEAM IAW SRM 51-42-11 & PAINTED IAW SRM 51-75-12.Aug 28, 2010 · N302NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1010293102Wire Harness · inoperativeDURING A NON ROUTINE CHECK, MX FOUND SEAT 5C EMERGENCY LIGHT INOPERATIVE. FOUND WIRE PULLED FROM INBD CONNECTOR OF HARNESS. REPLACED HARNESS AND FUNCTIONAL CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.May 17, 2010 · N302NB · Airbus A319114 · Light System WiringSDR 0101913102Flow Valve · defectiveDURING CLIMB FOLLOWING AN AIR CONDITIONING PACK 2 RESET DUE TO AN OVERHEAT, FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN. NR 2 PACK WAS SELECTED OFF. RETURNED TO DEPARTURE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE DEACTIVATED THE NR 2 PACK AND PLACED OMay 19, 2001 · N302NB · Airbus A319113 · Cabin Cooling SystemSDR 0000893102Smoke · detectedDURING CRUISE, RECEIVED SMOKE LAVATORY SMOKE ECAM WARNING. A PORTABLE FIRE EXTINGUISHER WAS USED BY FLIGHT ATTENDANT IN RIGHT AFT LAV UNDER SINK WASTE CONTAINER. INVESTIGATION OF WASTE CONTAINER CONTENTS REVEALED A CIGARETTE TO BE THE CAUSE. MAINTENANCE INSMar 7, 2000 · N302NB · Airbus A319113 · Smoke Detection
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