# Service difficulty reports: N641VA, cancelled Apr 22, 2024 A list on [N641VA, cancelled Apr 22, 2024](https://openairdocs.org/deregistered/N641VA-2024-04-22.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR ASAA2023090845601](https://openairdocs.org/sdr/ASAA2023090845601.md): Floorboard · delaminated · Sep 8, 2023 · N641VA · Airbus A320214 · Fuselage Floor Panel > MAIN 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. - [SDR ASAA2023090845600](https://openairdocs.org/sdr/ASAA2023090845600.md): Floor Panel · delaminated · Sep 8, 2023 · N641VA · Airbus A320214 · Fuselage Floor Panel > MAIN 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-A - [SDR ASAA2023083146150](https://openairdocs.org/sdr/ASAA2023083146150.md): Floor Panel · damaged · Aug 31, 2023 · N641VA · Airbus A320214 · Fuselage Floor Panel > MAIN CABIN FLOOR PANEL 231VF HAS DAMAGED UPPER SKIN. GROUNDED - YES. FABRICATED MAIN CABIN FLOOR PANEL 231VF IAW DWG SB2076 REV C. - [SDR ASAA2023083146149](https://openairdocs.org/sdr/ASAA2023083146149.md): Floor Panel · damaged · Aug 31, 2023 · N641VA · Airbus A320214 · Fuselage Floor Panel > MAIN CABIN FLOOR PANEL 232KF HAS DAMAGED UPPER SKIN. GROUNDED - YES. FABRICATED MAIN CABIN FLOOR PANEL 2323KF IAW DWG SB2076 REV C. - [SDR ASAA2023083146148](https://openairdocs.org/sdr/ASAA2023083146148.md): Floor Panel · damaged · Aug 31, 2023 · N641VA · Airbus A320214 · Fuselage Floor Panel > MAIN CABIN FLOOR PANEL 241EF HAS DAMAGED UPPER SKIN GROUNDED - YES. FABRICATED MAIN CABIN FLOOR PANEL 241EF IAW DWG SB2076 REV C - [SDR ASAA2023083146147](https://openairdocs.org/sdr/ASAA2023083146147.md): Floor Panel · damaged · Aug 31, 2023 · N641VA · Airbus A320214 · Fuselage Floor Panel > MAIN CABIN FLOOR PANEL 231VF HAS DAMAGED UPPER SKIN. GROUNDED - YES. FABRICATED MAIN CABIN FLOOR PANEL 231VF IAW DWG SB2076 REV C. - [SDR ASAA2023083146145](https://openairdocs.org/sdr/ASAA2023083146145.md): Floorboard · punctured · Aug 31, 2023 · N641VA · Airbus A320214 · Fuselage Floor Panel > MAIN CABIN FLOOR BOARD 231QF HAS PUNCTURES. GROUNDED - YES. FABRICATED NEW FLOOR BOARD PANEL 231QF IAW DWG SB2076 REV A. - [SDR ASAA2023083145604](https://openairdocs.org/sdr/ASAA2023083145604.md): Floorboard · damaged · Aug 31, 2023 · N641VA · Airbus A320214 · Fuselage Floor Panel > MAIN 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-A - [SDR ASAA2023083145602](https://openairdocs.org/sdr/ASAA2023083145602.md): Floorboard · damaged · Aug 31, 2023 · N641VA · Airbus A320214 · Fuselage Floor Panel > MAIN 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. - [SDR ASAA2023083145401](https://openairdocs.org/sdr/ASAA2023083145401.md): Floor Panel · dented · Aug 31, 2023 · N641VA · Airbus A320214 · Fuselage Floor Panel > MAIN 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. - [SDR ASAA2023083145309](https://openairdocs.org/sdr/ASAA2023083145309.md): Floor Panel · punctured · Aug 31, 2023 · N641VA · Airbus A320214 · Fuselage Miscellaneous Structure > MAIN 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. - [SDR ASAA2023080846088](https://openairdocs.org/sdr/ASAA2023080846088.md): Skin · corroded · Aug 8, 2023 · N641VA · Airbus A320214 · Ailerons > L/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. - [SDR ASAA2020022753280](https://openairdocs.org/sdr/ASAA2020022753280.md): Stringer · corroded · Feb 25, 2020 · N641VA · Airbus A320214 · Fuselage Main, Longeron/Stringer > CORROSION 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 - [SDR ASAA2020011732164](https://openairdocs.org/sdr/ASAA2020011732164.md): Seat Track · corroded · Jan 17, 2020 · N641VA · Airbus A320214 · Fuselage, Seat/Cargo Attach Fittings > MAIN 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 53-11-14-283-00 - [SDR ASAA2020030232315](https://openairdocs.org/sdr/ASAA2020030232315.md): Stringer · corroded · Jan 16, 2020 · N641VA · Airbus A320214 · Fuselage Main, Longeron/Stringer > CORROSION 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 IS - [SDR ASAA2020012463942](https://openairdocs.org/sdr/ASAA2020012463942.md): Support · corroded · Jan 16, 2020 · N641VA · Airbus A320214 · Fuselage Miscellaneous Structure > AFT 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 D53474180 - [SDR ASAA2020022852292](https://openairdocs.org/sdr/ASAA2020022852292.md): Stringer · corroded · Jan 15, 2020 · N641VA · Airbus A320214 · Fuselage Main, Longeron/Stringer > AFT 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 4 - [SDR ASAA2020022132224](https://openairdocs.org/sdr/ASAA2020022132224.md): Floor Panel · corroded · Jan 13, 2020 · N641VA · Airbus A320214 · Fuselage Floor Panel > PARTS 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 LIMITS - [SDR ASAA2020022132223](https://openairdocs.org/sdr/ASAA2020022132223.md): Floor Panel · corroded · Jan 13, 2020 · N641VA · Airbus A320214 · Fuselage Floor Panel > PARTS 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 LIMITS - [SDR ASAA2020022132222](https://openairdocs.org/sdr/ASAA2020022132222.md): Web · corroded · Jan 13, 2020 · N641VA · Airbus A320214 · Fuselage Miscellaneous Structure > AFT 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 LIMITS - [SDR ASAA2020022132221](https://openairdocs.org/sdr/ASAA2020022132221.md): Web · corroded · Jan 13, 2020 · N641VA · Airbus A320214 · Fuselage Miscellaneous Structure > AFT 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 LIMITS - [SDR ASAA202002132163](https://openairdocs.org/sdr/ASAA202002132163.md): Floor Support · corroded · Jan 13, 2020 · N641VA · Airbus A320214 · Fuselage Miscellaneous Structure > AFT 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 5 - [SDR ASAA2020021233105](https://openairdocs.org/sdr/ASAA2020021233105.md): Seat Track · corroded · Jan 13, 2020 · N641VA · Airbus A320214 · Fuselage, Seat/Cargo Attach Fittings > MAIN 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# 965684.1 - [SDR ASAA2020021033104](https://openairdocs.org/sdr/ASAA2020021033104.md): Seat Track · corroded · Jan 13, 2020 · N641VA · Airbus A320214 · Fuselage, Seat/Cargo Attach Fittings > MAIN 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# 964449.3 - [SDR ASAA2020021032103](https://openairdocs.org/sdr/ASAA2020021032103.md): Floorbeam · corroded · Jan 13, 2020 · N641VA · Airbus A320214 · Fuselage Main, Floor Beam > MAIN 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# 964396.1 - [SDR ASAA2020020512079](https://openairdocs.org/sdr/ASAA2020020512079.md): Seat Track · corroded · Jan 13, 2020 · N641VA · Airbus A320214 · Fuselage, Seat/Cargo Attach Fittings > MAIN 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" - [SDR ASAA2020020512078](https://openairdocs.org/sdr/ASAA2020020512078.md): Seat Track · corroded · Jan 13, 2020 · N641VA · Airbus A320214 · Fuselage, Seat/Cargo Attach Fittings > MAIN 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 D53112812 - [SDR ASAA2020011332064](https://openairdocs.org/sdr/ASAA2020011332064.md): Web · corroded · Jan 13, 2020 · N641VA · Airbus A320214 · Fuselage Miscellaneous Structure > AFT 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. - [SDR ASAA2020012933994](https://openairdocs.org/sdr/ASAA2020012933994.md): Web · cracked · Jan 13, 2020 · N641VA · Airbus A320214 · Fuselage Miscellaneous Structure > AFT 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 18D53480505 - [SDR ASAA2020012433943](https://openairdocs.org/sdr/ASAA2020012433943.md): Floor Support · corroded · Jan 13, 2020 · N641VA · Airbus A320214 · Fuselage Miscellaneous Structure > AFT 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 18D5372780 - [SDR ASAA2020012433941](https://openairdocs.org/sdr/ASAA2020012433941.md): Floor Support · corroded · Jan 13, 2020 · N641VA · Airbus A320214 · Fuselage Miscellaneous Structure > AFT 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 18D53472780 - [SDR ASAA202001243940](https://openairdocs.org/sdr/ASAA202001243940.md): Floor Support · corroded · Jan 13, 2020 · N641VA · Airbus A320214 · Fuselage Miscellaneous Structure > AFT 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 18D53471780 - [SDR ASAA2020022832297](https://openairdocs.org/sdr/ASAA2020022832297.md): Stringer · corroded · Jan 12, 2020 · N641VA · Airbus A320214 · Fuselage Main, Longeron/Stringer > AFT 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 - [SDR ASAA2020022832296](https://openairdocs.org/sdr/ASAA2020022832296.md): Stringer · corroded · Jan 12, 2020 · N641VA · Airbus A320214 · Fuselage Main, Longeron/Stringer > AFT 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 FOUN - [SDR ASAA2020022832295](https://openairdocs.org/sdr/ASAA2020022832295.md): Stringer · corroded · Jan 12, 2020 · N641VA · Airbus A320214 · Fuselage Main, Longeron/Stringer > AFT 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, REMOVE - [SDR ASAA2020022832294](https://openairdocs.org/sdr/ASAA2020022832294.md): Stringer · corroded · Jan 12, 2020 · N641VA · Airbus A320214 · Fuselage Main, Longeron/Stringer > AFT 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 3 - [SDR ASAA2020022832293](https://openairdocs.org/sdr/ASAA2020022832293.md): Stringer · corroded · Jan 12, 2020 · N641VA · Airbus A320214 · Fuselage Main, Longeron/Stringer > AFT 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 38 - [SDR ASAA2020022832291](https://openairdocs.org/sdr/ASAA2020022832291.md): Stringer · corroded · Jan 12, 2020 · N641VA · Airbus A320214 · Fuselage Main, Longeron/Stringer > AFT 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 - [SDR ASAA2020030232311](https://openairdocs.org/sdr/ASAA2020030232311.md): Web · corroded · Jan 8, 2020 · N641VA · Airbus A320214 · Fuselage Miscellaneous Structure > AFT 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 S - [SDR ASAA2020030232312](https://openairdocs.org/sdr/ASAA2020030232312.md): Skin Panel · gouged · Jan 7, 2020 · N641VA · Airbus A320214 · Leading Edge Devices > LEFT 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- - [SDR ASAA2018112927195](https://openairdocs.org/sdr/ASAA2018112927195.md): Acm · seized · Nov 29, 2018 · N641VA · Airbus A320214 · Cabin Cooling System > STRONG 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. - [SDR VQIA2016020120005](https://openairdocs.org/sdr/VQIA2016020120005.md): Actuator · failed · Jan 31, 2016 · N641VA · Airbus A320214 · Engine (Turbine/Turboprop) > ACFT 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 - [SDR VQIA2015072400028](https://openairdocs.org/sdr/VQIA2015072400028.md): Sensor · malfunctioned · Jul 12, 2015 · N641VA · Airbus A320214 · Engine Indicating System > AIRCRAFT 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 POS - [SDR VQI2015F00022](https://openairdocs.org/sdr/VQI2015F00022.md): Girt Bar · obstructed · May 29, 2015 · N641VA · Airbus A320214 · Emergency Equipment > ACFT 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. - [SDR VQI2015F00002](https://openairdocs.org/sdr/VQI2015F00002.md): Fan · failed · Dec 23, 2014 · N641VA · Airbus A320214 · Air Distribution Fan > EXPERIENCED 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 PLACE - [SDR VQI2013F00032](https://openairdocs.org/sdr/VQI2013F00032.md): Bushing · migrated · Oct 29, 2013 · N641VA · Airbus A320214 · Fuselage Miscellaneous Structure > ACFT 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. - [SDR VQIA2012F00034](https://openairdocs.org/sdr/VQIA2012F00034.md): Button · out of alignment · Sep 5, 2012 · N641VA · Airbus A320214 · Passenger/Crew Doors > DURING 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 PO ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N641VA-2024-04-22/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.