N375NC

Service difficulty reports · 139

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 = 'N375NC' 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 DALA2019070103997Floorbeam · corrodedCORROSION FLOORBEAM -Y1162 FR 68 TO FR 69 AT AFT GALLEY AREA (1 EA), REPLACED FLOORBEAM -Y1162 LOC. FR68 TO FR 69 AR AFT GALLEY AREA ASPER SRM 51-72-11 AND DWG D53472780 SHEET 9.Jun 30, 2019 · N375NC · Airbus A320212 · Fuselage Main, Floor BeamSDR DALA2019071904350Structure · dentedDENT ON RT SIDE OF EMPENNAGE BETWEEN STR21 AND STR 20, FRAME 74 AND 75, PERFORMED PERMANENT REPAIR ON DENTED AREA ASPER ER/A 579558-14. REV ORIGINAL AND PRI 579558-14 REV 0 AND REV 1.May 2, 2019 · N375NC · Airbus A320212 · Aerodynamic FairingsSDR DALA2019040902327Light · inoperativeEMERGENCY LIGHT LEFT FORWARD OVERWING INOP, REPLACED LT FORWARD OVERWING EXIT LT ASSYApr 7, 2019 · N375NC · Airbus A320212 · Emergency LightingSDR DALA2018062204162Smoke Warning · false activationLAVATORY SMOKE WARNING ON ECAM. CABIN CREW REPORTED NO SMOKE IN LAVATORY. PASSENGER WAS IN AFT RIGHT LAVATORY AT THE TIME OF WARNING. OPERATION CHECKS OKAY.Jun 20, 2018 · N375NC · Airbus A320212 · Smoke DetectionSDR DALA2017101907630Battery Pack · faultedEMERGENCY LIGHTS FAULT, LT EPSU LOAD FAIL, REPLACED THE BATTERY PACK.Oct 19, 2017 · N375NC · Airbus A320212 · Emergency LightingSDR DALA2016113009408Frame · corrodedCORROSION ON LOWER SILL FRAME 66 LT AT AFT GALLEY AREA, REPAIRED IAW SRM 53-41-14, PARAGRAPH. 5A FIGURE 201.Nov 29, 2016 · N375NC · Airbus A320211 · Fuselage Main, FrameSDR DALA2016110608278Wire · brokenEMERGENCY LIGHT AT 18C INOPERATIVE, REPAIRED BROKEN WIRENov 5, 2016 · N375NC · Airbus A320212 · Light System WiringSDR DALA2016091606698Power Supply · no testEPSU EMERGENCY LIGHT SYS TEST FAULT. REPLACED R2 DOOR SLIDE.Sep 15, 2016 · N375NC · Airbus A320212 · Emergency LightingSDR DALA2015060703606Battery Pack · inoperativeDURING NON-ROUTINE CHECK, ROW 10WL EMERGENCY POWER SUPPLY BATTERY INOPERATIVE. REPLACED BATTERY IN ROW 10WL EMERGENCY POWER SUPPLY UNIT AND OPS CHECK WAS NORMAL.Jun 5, 2015 · N375NC · Airbus A320212 · Emergency LightingSDR DALA2015042002809Power Supply · failedDURING NON ROUTINE CHECK, FOUND EMERGENCY POWER SUPPLY UNIT 11WL FAILS BITE CHECK. REPLACED EPSU AT 11WL.Apr 18, 2015 · N375NC · Airbus A320211 · Emergency LightingSDR DALA2014091705069Power Supply · inoperativeDURING NON-ROUTINE CHECK, FOUND EPSU EMERGENCY SYSTEM FAULT. MAINTENANCE REPLACED EPSU AND FUNCTIONAL CHECK WAS NORMAL.Sep 16, 2014 · N375NC · Airbus A320212 · Emergency LightingSDR DALA13049803275Shear Plate · corrodedDURING INSPECTION, FOUND CORROSION ON SHEAR PLATE IN AFT CABIN FLOOR STRUCTURE LOCATED BETWEEN FR 69 AND FR 70 AT LEVEL STR 23R. MEASURES APPROX L=2" W=1.5" D=0.003". REPLACED SHEAR PLATE LOCATION BETWEEN FR 69 AND FR 70 AT LEVEL STR 23R AFT CABIN FLOOR STOct 3, 2013 · N375NC · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA13049793275Shear Plate · corrodedDURING INSPECTION, FOUND CORROSION ON SHEAR PLATE IN AFT CABIN FLOOR STRUCTURE LOCATED FR 69 AND FR 70 AT LEVEL STR 23L. MEASURES APPROX: L=3"; W=2"; D=0.003". REPLACED SHEAR PLATE LOCATION BETWEEN FR 69 AND FR 70 AT LEVEL STR 23L AFT CABIN FLOOR STRUCTURE SROct 2, 2013 · N375NC · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA13049303275Stringer · corrodedCORROSION ON STRINGER 43L IN AFT CARGO BAY BETWEEN FRAMES 56 AND 57. REPAIRED STRINGER IAW SRM 53-00-13, PARA 4A, FIG 201.Oct 1, 2013 · N375NC · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA13048213275Strut · corrodedDURING INSPECTION, FOUND CORROSION ON INTERCONNECTING STRUT OF INBD RT FLAP. REPLACED STRUT IAW ADMS 2750-6010-RT.Sep 29, 2013 · N375NC · Airbus A320212 · Trailing Edge FlapsSDR DALA13048203275Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER SILL IN AFT CABIN FLOOR STRUCT LOCATION BETWEEN FR 66 AND FR 68 AND AT LEVEL STR 23L. REPLACED IAW 51-72-11.Sep 28, 2013 · N375NC · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA13048193275Strut · corrodedDURING INSPECTION, FOUND CORROSION ON INTERCONNECTING STRUT OF INBOARD FLAP, REPLACED INTERCONNECTING STRUT OF INBD FLAP LT.Sep 28, 2013 · N375NC · Airbus A320212 · Trailing Edge FlapsSDR DALA13049293275Floor Support · corrodedCORROSION ON FLOOR SUPPORT Y1162 BETWEEN FRAMES 67+15" AND 69. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472780.Sep 27, 2013 · N375NC · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA13049283275Floor Support · corrodedCORROSION ON FLOOR SUPPORT Y1225 BETWEEN FRAMES 66+5" AND 67+15" . REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472815.Sep 27, 2013 · N375NC · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA13049273275Skin · nickedNICK ON LOWER EXTERNAL FUSELAGE SKIN BETWEEN FRAMES 28 - 29 AND BETWEEN STRINGERS 43-44R. REPAIREDIAW SRM 53-21-11 PARA 5 K. FIG 214.Sep 27, 2013 · N375NC · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA13047063275Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT IN AFT CABIN BETWEEN FRAMES 67+16" AND 68 AT LEVEL S23R. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53480505.Sep 24, 2013 · N375NC · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA13046823275Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y1162 IN AFT CABIN BETWEEN FRAMES 67+15" AND 69. REPLACED FLOOR SUPPORT IAW SRM AND DWG D53472815.Sep 23, 2013 · N375NC · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA13046813275Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y1225 IN AFT CABIN BETWEEN FRAMES 66+5" AND 67+15". REPLACED FLOOR SUPPORT IAW 51-72-11 AND DWG D53472780.Sep 23, 2013 · N375NC · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA13046263275Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y765 BETWEEN FRAMES 66+5" AND 70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11AND DWG D53472000.Sep 21, 2013 · N375NC · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA13046253275Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON PAX CABIN FLOOR SUPPORT -Y189 BETWEEN FRAMES 20 AND 21. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 .Sep 21, 2013 · N375NC · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA13046243275Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON PAX CABIN SEAT TRACK -Y765 BETWEEN FRAMES 20 AND 21. REPLACED IAW SRM A320-51-72-11 AND DWG D53112812, D53110920.Sep 21, 2013 · N375NC · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA13046233275Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON PAX CABIN SEAT TRACK LOCATED -Y1292 BETWEEN FR 20 AND FR 21. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D53112812.Sep 21, 2013 · N375NC · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA13045933275Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON PAX CABIN FLOOR SUPPORT LOCATED Y254 BETWEEN FR 16 AND FR 21. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWGS D53112816 , D53110920 AND D53110984.Sep 19, 2013 · N375NC · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA13045923275Dummy Rail · corrodedDURING INSPECTION, FOUND CORROSION ON PAX CABIN RAIL DUMMY LOCATED Y503.2 AND FR 16. REPLACED RAIL DUMMY LOCATED Y503.2 AND FR 14 TO FR 16 IAW SRM 51-72-11, TOOL USED DIGIMATIC DEPTH GAGES, PN 547-2185, SN 001658.Sep 19, 2013 · N375NC · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA13045563275Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON PAX CABIN SEAT TRACK LOCATED Y765 BETWEEN FRAMES 20 AND 23. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWS D53112812, D53110920 AND D53110984.Sep 17, 2013 · N375NC · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA13045003275Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON PAX CABIN FLOOR SUPPORT. REPLACED SUPPORT FLOOR LOCATED Y1292 BETWEEN FR 12 TO FR 24 PAX CABIN IAW SRM 51-72-11 AND DWG D53112812.Sep 16, 2013 · N375NC · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA13025103275Wire · brokenEMERGENCY LIGHT AT SEATS 12,13,14,26 INOPERATIVE. WIRE BROKEN AT 26, REPAIRED, OPS OK.May 22, 2013 · N375NC · Airbus A320212 · Light System WiringSDR DALA13008283275Wire · brokenDURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHTS AT ROW 1AB INOPERATIVE. MX REPAIRED BROKEN WIRES AND FUNCTIONAL CHECK WAS NORMAL.Feb 20, 2013 · N375NC · Airbus A320212 · Light System WiringSDR DALA13013263275Power Supply · faultedDURING NON ROUTINE CHECK, FOUND FORWARD LT EMERGENCY BATTERY FAULT. MX REPLACED FORWARD ESPU AND FUNCTIONAL CHECK WAS NORMAL.Jan 26, 2013 · N375NC · Airbus A320212 · Emergency LightingSDR DALA12016023275Power Supply · inoperativeDURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHTS AT FORWARD GALLEY AND F/C INOPERATIVE. MX REPLACED EMERGENCY POWER SUPPLY UNIT AND FUNCTIONAL CHECK WAS NORMAL.Dec 12, 2012 · N375NC · Airbus A320212 · Emergency LightingSDR DALA1208363275Connector · disconnectedDURING NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT ROW 17 AND 18 INOPERATIVE. MAINTENANCE RECONNECTED CONNECTOR AT ROW 8 AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.Feb 13, 2012 · N375NC · Airbus A320212 · Light System WiringSDR NWAA092273275Wire · disconnectedEMERGENCY EGRESS PATH LIGHTS AT ROWS 16-19ABC INOP. RECONNECTED WIRES AT SEAT ROWS 16-19ABC, OPS CHECK GOOD.Jun 21, 2009 · N375NC · Airbus A320212 · Light System WiringSDR NWAA 091283275Epsu · no testEMERGENCY EGRESS LIGHT TEST FAILED. REPLACED LT OVERWING EPSU (11WL), CHECKS GOOD.Apr 19, 2009 · N375NC · Airbus A320212 · Emergency LightingSDR NWAA081693275Skin · damagedDURING GROUND OPERATIONS FUSELAGE SKIN WAS DAMAGED FROM S41L-S43L AT FR 57 TO FR 58. REPAIRED PER EA 32-212764 SECT II SECT III PERMANENT REPAIR TO BE ACCOMPLISHED WITHIN 60 DAYS OF SECT II.Apr 16, 2008 · N375NC · Airbus A320212 · Fuselage Main, Plate/Skin
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