N641VA, cancelled Apr 22, 2024

Service difficulty reports · 47

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 = 'N641VA' AND deregistration_id = 'N641VA-2024-04-22'
  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 ASAA2023090845601Floorboard · delaminatedMAIN CABIN FLOOR BOARD 251CF HAS DELAMINATION ON UPPER SKIN GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR BOARD 251CF AT FR47 TO FR51 LBL30 TO LBL50 IAW A320 AMM 53-00-00-000-801-A AND AMM 53-00-00-400-801-A.Sep 8, 2023 · N641VA · Airbus A320214 · Fuselage Floor PanelSDR ASAA2023090845600Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 251MF HAS DELAMINATION GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR PANEL 251MF AT FR54 TO FR58 LBL10 TO LBL30 IAW A320 AMM 53-00-00-000-801-ASep 8, 2023 · N641VA · Airbus A320214 · Fuselage Floor PanelSDR ASAA2023083146150Floor Panel · damagedMAIN CABIN FLOOR PANEL 231VF HAS DAMAGED UPPER SKIN. GROUNDED - YES. FABRICATED MAIN CABIN FLOOR PANEL 231VF IAW DWG SB2076 REV C.Aug 31, 2023 · N641VA · Airbus A320214 · Fuselage Floor PanelSDR ASAA2023083146149Floor Panel · damagedMAIN CABIN FLOOR PANEL 232KF HAS DAMAGED UPPER SKIN. GROUNDED - YES. FABRICATED MAIN CABIN FLOOR PANEL 2323KF IAW DWG SB2076 REV C.Aug 31, 2023 · N641VA · Airbus A320214 · Fuselage Floor PanelSDR ASAA2023083146148Floor Panel · damagedMAIN CABIN FLOOR PANEL 241EF HAS DAMAGED UPPER SKIN GROUNDED - YES. FABRICATED MAIN CABIN FLOOR PANEL 241EF IAW DWG SB2076 REV CAug 31, 2023 · N641VA · Airbus A320214 · Fuselage Floor PanelSDR ASAA2023083146147Floor Panel · damagedMAIN CABIN FLOOR PANEL 231VF HAS DAMAGED UPPER SKIN. GROUNDED - YES. FABRICATED MAIN CABIN FLOOR PANEL 231VF IAW DWG SB2076 REV C.Aug 31, 2023 · N641VA · Airbus A320214 · Fuselage Floor PanelSDR ASAA2023083146145Floorboard · puncturedMAIN CABIN FLOOR BOARD 231QF HAS PUNCTURES. GROUNDED - YES. FABRICATED NEW FLOOR BOARD PANEL 231QF IAW DWG SB2076 REV A.Aug 31, 2023 · N641VA · Airbus A320214 · Fuselage Floor PanelSDR ASAA2023083145604Floorboard · damagedMAIN CABIN FLOOR BOARD 242HF HAS DAMAGED UPPER SKIN GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR BOARD 242HF AT FR36 TO FR42 RBL51.5 TO RBL69.0 IAW A320 AMM 53-00-000-801-AAug 31, 2023 · N641VA · Airbus A320214 · Fuselage Floor PanelSDR ASAA2023083145602Floorboard · damagedMAIN CABIN FLOOR BOARD 241AF HAS DAMAGE ON UPPER SKIN GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR BOARD 241AF AT FR35 TO FR36 LBL10 TO RBL10 IAW A320 AMM 53-00-00-400-801-A.Aug 31, 2023 · N641VA · Airbus A320214 · Fuselage Floor PanelSDR ASAA2023083145401Floor Panel · dentedMAIN CABIN FLOOR PANEL 251TF HAS A DENT GROUNDED - YES. PERFORMED PERMANENT REPAIR ON CABIN FLOOR PANEL 251TF P/N: D5367150100000 FR58 - FR62 IAW A320 SRM 53-02-00-300-001 AND 51-77-11-911-031.Aug 31, 2023 · N641VA · Airbus A320214 · Fuselage Floor PanelSDR ASAA2023083145309Floor Panel · puncturedMAIN CABIN FLOOR PANEL 251NF HAS PUNCTURES. GROUNDED - YES. PERFORMED PERMANENT REPAIR ON MAIN CABIN FLOOR PANEL 251NF ZONE A IAW A320 SRM 53-02-00-300 AND 51-77-11-911-031 REV 28.Aug 31, 2023 · N641VA · Airbus A320214 · Fuselage Miscellaneous StructureSDR ASAA2023080846088Skin · corrodedL/WING UPPER SKIN FWD OF AILERON HAS MULTIPLE AREAS OF CORROSION AROUND FASTENER HEADS. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR ON L/H WING UPPER SKIN AT RIB 22-RIB 27 IAW ASA EA A320-57EA-01931 REV 00 DATED 10/20/2023.Aug 8, 2023 · N641VA · Airbus A320214 · AileronsSDR ASAA2020022753280Stringer · corrodedCORROSION AT, AFT PIT, R/H FRAME C51, STRINGER 38 GROUNDED - YES. REMOVED CORROSION AND CHECKED LIMITS. ORIGINAL THICKNESS IS .095, REMAINING IS .083, .012 WAS REMOVED. FOUND TO BE OUT OF LIMITS REF A320 SRM 51-73-11 AND AIRBUS DWG E53470525 ISSUE K. REPAIRED Feb 25, 2020 · N641VA · Airbus A320214 · Fuselage Main, Longeron/StringerSDR ASAA2020011732164Seat Track · corrodedMAIN CABIN FLOOR STRUCTURE AT C16, Y254, UPPER SURFACE OF TRACK FLANGE HAS CORROSION GROUNDED - YES. REMOVED CORROSION AND CHECKED LIMITS. ORIGINAL THICKNESS IS .063, REMAINING IS .019, .044 WAS REMOVED. FOUND TO BE OUT OF LIMITS REF A320 SRM 53-11-14-283-00Jan 17, 2020 · N641VA · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA2020030232315Stringer · corrodedCORROSION AT, AFT PIT, R/H FRAME C51, STRINGER 38 LATE FIND GROUNDED - YES. REMOVED CORROSION AND CHECKED THE LIMITS. ORIGINAL THICKNESS IS .095, REMAINING IS .083, .012 WAS REMOVED. FOUND TO BE OUT OF LIMITS REF A320 SRM 51-73-11 AND AIRBUS DWG E53470525 ISJan 16, 2020 · N641VA · Airbus A320214 · Fuselage Main, Longeron/StringerSDR ASAA2020012463942Support · corrodedAFT MAIN CABIN, R/H SIDE, O/B FLOOR WEB SUPPORT ANGLE BETWEEN FR69-70 IS CORRODED GROUNDED - YES. REMOVED AND REPLACED WEB SUPPORT D5347112320300 REF AIRBUS DWG D53474180Jan 16, 2020 · N641VA · Airbus A320214 · Fuselage Miscellaneous StructureSDR ASAA2020022852292Stringer · corrodedAFT CARGO, STR.43 L/H HAS AREA OF CORROSION FROM FR. 56 TO FR.57 GROUNDED - YES. REMOVED CORROSION AND CHECKED THE LIMITS. ORIGINAL THICKNESS IS .110, .078 WAS REMOVED, REMAINING THICKNESS IS .032 FOUND TO BE OUT OF LIMITS REF A320 SRM 51-73-11. REPAIRED STR 4Jan 15, 2020 · N641VA · Airbus A320214 · Fuselage Main, Longeron/StringerSDR ASAA2020022132224Floor Panel · corrodedPARTS RACK- AFT WET AREA FLOOR PANEL 262LG IS CORRODED GROUNDED - YES. RECEIVED NEW FLOOR PANEL PO # 965072.3 FLOOR PANEL INSTALLED ON CARD G1326592 NO ALLOWABLE LIMITSJan 13, 2020 · N641VA · Airbus A320214 · Fuselage Floor PanelSDR ASAA2020022132223Floor Panel · corrodedPARTS RACK- AFT WET AREA FLOOR PANEL 261LG IS CORRODED GROUNDED - YES. RECEIVED NEW FLOOR PANEL PO # 965072.2. FLOOR PANEL INSTALLED ON TASK CARD G1326592 NO ALLOWABLE LIMITSJan 13, 2020 · N641VA · Airbus A320214 · Fuselage Floor PanelSDR ASAA2020022132222Web · corrodedAFT MAIN CABIN, R/H SIDE, O/B FLOOR WEB BETWEEN FR 69-70 IS CORRODED MARKED. GROUNDED - YES. REMOVED AND REPLACED AFT MAIM CABIN R/H SIDE O/B FLOOR WEB BETWEEN 69-70 IAW AIRBUS A320 SRM 51-42-11 AND DWG 18D53474180 NO ALLOWABLE LIMITSJan 13, 2020 · N641VA · Airbus A320214 · Fuselage Miscellaneous StructureSDR ASAA2020022132221Web · corrodedAFT MAIN CABIN, L/H SIDE O/B FLOOR WEB BETWEEN FR69-70 IS CORRODED. MARKED. GROUNDED - YES. REMOVED AND REPLACED FLOOR WEB REF AIRBUS DWG D53474180 AND A320 SRM 51-42-11. NO ALLOWABLE LIMITSJan 13, 2020 · N641VA · Airbus A320214 · Fuselage Miscellaneous StructureSDR ASAA202002132163Floor Support · corrodedAFT MAIN CABIN, R/H SIDE FLOOR BEAM FWD OF R2 DOOR CUTOUT, MOST O/B FLOOR BEAM HAS CORROSION MARKED. GROUNDED - YES. REMOVED CORROSION AND CHECKED LIMITS. ORIGINAL THICKNESS IS .150, REMAINING IS .106, .044 REMOVED. FOUND TO BE OUT OF LIMITS REF A320 SRM 5Jan 13, 2020 · N641VA · Airbus A320214 · Fuselage Miscellaneous StructureSDR ASAA2020021233105Seat Track · corrodedMAIN CABIN FLOOR WEB HAS NUMEROUS SPOTS OF SURFACE CORROSION BETWEEN STA C16 AND STA C20 LBL1651MM. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN SEAT TRACK REF A320 SRM 51-72-11 AND AIRBUS DWG D53112812 ISSUE "E" PO# 965684.1Jan 13, 2020 · N641VA · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA2020021033104Seat Track · corrodedMAIN CABIN FLOOR BEAM HAS SURFACE CORROSION AT STA C20 RBL290MM. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN TRACK REF A320 SRM 51-72-11 AND AIRBUS DWG D53111460 ISSUE "C" PO# 964449.3Jan 13, 2020 · N641VA · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA2020021032103Floorbeam · corrodedMAIN CABIN FLOOR BEAM HAS SURFACE CORROSION AT STA C20 RBL240MM. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR SUPPORT RAIL REF A320 SRM 51-72-11 AND AIRBUS DWG D53111406 ISSUE "B" PO# 964396.1Jan 13, 2020 · N641VA · Airbus A320214 · Fuselage Main, Floor BeamSDR ASAA2020020512079Seat Track · corrodedMAIN CABIN FLOOR BEAM HAS SURFACE CORROSION AT STA C16 RBL813MM GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN SEAT TRACK D5311278220201 REF A320 SRM 51-72-11 AND AIRBUS DWG D53112812 ISSUE "E"Jan 13, 2020 · N641VA · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA2020020512078Seat Track · corrodedMAIN CABIN FLOOR BEAM HAS SURFACE CORROSION AT STA C16 RBL1346MM. GROUNDED - YES. REMOVED AND REPLACED SEAT TRACK REF A320 SRM 51-72-11 AND AIRBUS DWG D53112812Jan 13, 2020 · N641VA · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA2020011332064Web · corrodedAFT MAIN CABIN, L/H SIDE O/B WEB SUPPORT BETWEEN FR69-70 IS CORRODED. MARKED. (LOOK FROM BELOW) GROUNDED - YES. REMOVED AND REPLACED FRAME SUPPORT WEB REF REF AIRBUS DWG D53474180 AND A320 SRM 51-42-11.Jan 13, 2020 · N641VA · Airbus A320214 · Fuselage Miscellaneous StructureSDR ASAA2020012933994Web · crackedAFT MAIN CABIN, L/H SIDE APPROX. 12" AFT OF FR 68 O/B FLOOR WEB/SUPPORT IS CRACKED AND CORRODED. GROUNDED - YES. REMOVED DAMAGED FLOOR WEB AND INSTALLED NEW WEB IAW AIRBUS A320 SRM 51-42-11 AND AIRBUS DRAWING 18D53480505Jan 13, 2020 · N641VA · Airbus A320214 · Fuselage Miscellaneous StructureSDR ASAA2020012433943Floor Support · corrodedAFT MAIN CABIN, FLOOR BEAM APPROX. LBL 6.5" IS CORRODED IN SEVERAL SPOTS FROM FR68-70. MARKED. GROUNDED - YES. REMOVED CORRODED BEAM IAW A320 SRM 51-42-11. DRILLED TO FIT AND INSTALLED BEAM IAW A320 SRM 51-72-11-911-001 AND AIRBUS DWG 18D5372780Jan 13, 2020 · N641VA · Airbus A320214 · Fuselage Miscellaneous StructureSDR ASAA2020012433941Floor Support · corrodedAFT MAIN CABIN, R/H SIDE, FLOOR BEAM AT APPROX. RBL30.5" AT FR68 IS CORRODED. GROUNDED - YES. REMOVED CORRODED BEAM IAW A320 SRM 51-42-11. DRILLED TO FIT AND INSTALLED BEAM IAW A320 SRM 51-72-11-911-001 AND AIRBUS DWG 18D53472780Jan 13, 2020 · N641VA · Airbus A320214 · Fuselage Miscellaneous StructureSDR ASAA202001243940Floor Support · corrodedAFT MAIN CABIN, L/H FLOOR BEAM APPRX. LBL 30.5 Ï¿½IS CORRODED IN A FEW AREAS FROM FR67-68. MARKED. GROUNDED - YES. REMOVED CORRODED BEAM IAW A320 SRM 51-42-11. DRILLED TO FIT AND INSTALLED BEAM IAW A320 SRM 51-772-11-911-001 AND AIRBUS DWG 18D53471780Jan 13, 2020 · N641VA · Airbus A320214 · Fuselage Miscellaneous StructureSDR ASAA2020022832297Stringer · corrodedAFT CARGO, STR.33 L/H HAS CORROSION IN MULTIPLE AREAS FROM FR.57 TO FR.64 GROUNDED - YES. REMOVED CORROSION ON STR 33LH FROMFR.57 TO FR.64 ORIG. THICKNESS .071, REMAINING .043, REMOVED .028 AND FOUND TO BE OUT OF LIMITS PER A320 SRM 51-73-11, REPAIRED STR 33 Jan 12, 2020 · N641VA · Airbus A320214 · Fuselage Main, Longeron/StringerSDR ASAA2020022832296Stringer · corrodedAFT CARGO, STR. 35 L/H HAS CORROSION IN MULTIPLE AREAS FROM FR.54 TO FR.64 GROUNDED - YES. REMOVED DAMAGE ORIG. THICKNESS .110, REMAINING THICKNESS .080, REMOVED .030 AND IN TRANSITION AREA ORIG. THICKNESS .071, REMAINING THICKNESS .041, REMOVED .030 AND FOUNJan 12, 2020 · N641VA · Airbus A320214 · Fuselage Main, Longeron/StringerSDR ASAA2020022832295Stringer · corrodedAFT CARGO, STR 36 L/H HAS CORROSION IN MULTIPLE AREAS FROM FR.53 TO FR.62 GROUNDED - YES. REMOVED CORROSION ON STR 36LH FROM FR.53 TO FR.62 ORIG. THICKNESS .110 REMAINING .082, REMOVED .028 AND ORIG. THICKNESS .071 IN TRANSITION AREA, REMAINING .044, REMOVEJan 12, 2020 · N641VA · Airbus A320214 · Fuselage Main, Longeron/StringerSDR ASAA2020022832294Stringer · corrodedAFT CARGO, STR 37 L/H HAS CORROSION IN MULTIPLE AREAS FROM FR.55 TO FR.64 GROUNDED - YES. REMOVED CORROSION ON STR 37 L/H FROM FR.55 TO FR.64 ORIG. THICKNESS .110 REMAINING .050, REMOVED .060 AND FOUND TO BE OUT OF LIMITS.PER A320 SRM 51-73-11, REPAIRED STR 3Jan 12, 2020 · N641VA · Airbus A320214 · Fuselage Main, Longeron/StringerSDR ASAA2020022832293Stringer · corrodedAFT CARGO, STR. 38 L/H HAS CORROSION IN MULTIPLE AREAS FROM FR.56 TO FR61. GROUNDED - YES. REMOVED CORROSION ON STR 38 L/H FROM FR.56 TO FR.61 ORIG THICKNESS .110 REMAINING .034, REMOVED .076 AND FOUND TO BE OUT OF LIMITS PER A320 SRM 51-73-11, REPAIRED STR 38Jan 12, 2020 · N641VA · Airbus A320214 · Fuselage Main, Longeron/StringerSDR ASAA2020022832291Stringer · corrodedAFT CARCO, STR.34 L/H HAS CORROSION IN MULTIPLE AREAS FROM FR. 53 TO FR.64 GROUNDED - YES. REMOVED CORROSION ON STR 34LH FROM FR.53 TO FR. 64 ORIG. THICKNESS .110, REMAINING THICKNESS .088, REMOVED .022 AND TRANSITION AREA ORIG. THICKNESS .071, REMAINING .048 Jan 12, 2020 · N641VA · Airbus A320214 · Fuselage Main, Longeron/StringerSDR ASAA2020030232311Web · corrodedAFT CARGO COMPARTMENT, DOOR BOX UPPER WEB CORRODED @ APPROX -41 FR C55 - FR C56, RBL -Y41 GROUNDED - YES. REMOVED CORRODED UPPER DOOR BOX WEB, LOCATED AND DRILLED NEW WEB P/N D5347556522200 PO# 963724.1 AND INSTALLED NEW WEB PER AIRBUS DWG E53470321 ISSUE AV SJan 8, 2020 · N641VA · Airbus A320214 · Fuselage Miscellaneous StructureSDR ASAA2020030232312Skin Panel · gougedLEFT WING INBOARD LEADING EDGE AT SLAT #1 ON THE INBOARD SIDE OF THE FIXED LEADING EDGE IS GOUGED WITH BARE METAL. "MARKED IN RED" GROUNDED - YES. REMOVED AND REPLACED L/H I/B FIXED L/E SKIN PANEL P/N D5745004820639 REF AIRBUS DWG D57450033 AND A320 SRM 51-42-Jan 7, 2020 · N641VA · Airbus A320214 · Leading Edge DevicesSDR ASAA2018112927195Acm · seizedSTRONG BURNING SMELL IN CABIN WITH SMOKE. GROUNDED - YES. R/R AIR CYCLE MACHINE IAW AMM 21-52-00, OPS CHECK/ LEAK CHECK GOOD. THIS CLEARS MDDR 61722, PLACARD REMOVED, MEL LIST UPDATED, MCC NOTIFIED.Nov 29, 2018 · N641VA · Airbus A320214 · Cabin Cooling SystemSDR VQIA2016020120005Actuator · failedACFT EXPERIENCED A NR 1 ENGINE COMPRESSOR VANE FAULT ON ECAM, THE FLIGHT CREW ELECTED TO RETURN TO DEPARTURE. UPON ARRIVAL TECHS ACCOMPLISHED TSM 75-30-00-810-801-A. THE VBV BALL SCREW ACTURATOR WAS FOUND FAULTY AND REPLACED IAW AMM 75-31-50, THE ASSOCIATED Jan 31, 2016 · N641VA · Airbus A320214 · Engine (Turbine/Turboprop)SDR VQIA2015072400028Sensor · malfunctionedAIRCRAFT REPORTED ENGINE 1 COMPRESSOR VANE FAULT UPON DEPARTURE, ELECTED TO RETURN TO DEPARTURE. ACFT LANDED SAFELY AND WAS TAKEN OUT OF SERVICE. ENGINE 1 COMPRESSOR VANE, MASTER CAUTION SEVERAL TIMES IN CLIMB, STARTING AT 6000 FT IB CLIMB OUT. R & R VBV POSJul 12, 2015 · N641VA · Airbus A320214 · Engine Indicating SystemSDR VQI2015F00022Girt Bar · obstructedACFT WAS GETTING READY FOR FLIGHT WHEN R2 DOOR WOULD NOT ARM. AFT RT CABIN DOOR NOT ARMING. CLEARED OBSTRUCTION FOUND UNDER R2 DOOR COMPLETED OPS CHECK, FOUND NO ISSUES AMM 52-13-12.May 29, 2015 · N641VA · Airbus A320214 · Emergency EquipmentSDR VQI2015F00002Fan · failedEXPERIENCED A VENT EXTRANT FAULT MESSAGE ON ECAM AND A SHORT DURATION ELECTRICAL BURNING ODOR. THE FLIGHT CREW FOLLOWED FCOM PROCEDURES AND CONTINUED, TSM 24-00-11-810-823A & 21-26-00-810-809A WERE ACCOMPLISHED, THE EXTRACT FAN 18HQ WAS FOUND FAILED AND PLACEDec 23, 2014 · N641VA · Airbus A320214 · Air Distribution FanSDR VQI2013F00032Bushing · migratedACFT EXPERIENCED A L1 DOOR GUST LOCK FAILURE. FAULT DETERMINED TO BE THE RESULT OF A MIGRATED BUSHING IN THE GUST LOCK MECHANISM. BUSHING REINSTALLED IAW AMM 52-11-00-05, NO FURTHER ISSUES WERE NOTED.Oct 29, 2013 · N641VA · Airbus A320214 · Fuselage Miscellaneous StructureSDR VQIA2012F00034Button · out of alignmentDURING GROUND SERVICING, CREW NOTED THAT THE L1 DOOR GUST LOCK MECHANISM WAS NOT ENGAGING. ON INSPECTION, NOTED THAT THE GUST LOCK RELEASE BUTTON HAD NO MECHANICAL TENSION. BUSHING THAT ALIGNS THE PLASTIC PLUNGER BUTTON WAS FOUND MIGRATED FROM ITS NORMAL POSep 5, 2012 · N641VA · Airbus A320214 · Passenger/Crew Doors
Back to N641VA, cancelled Apr 22, 2024