# N641VA: 2008 Airbus A320-214, registration cancelled 2024-04-22

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 22, 2024
- Exported to: Egypt
- Status when cancelled: Sale reported
- Airframe: [Airbus A320-214](https://openairdocs.org/model/airbus-a320-214) (registry code 3940006)
- Engine: [CFM International CFM56-5B4 series](https://openairdocs.org/engine/cfm-international-cfm56-5b4-series) (registry code 13010)
- Data sheets: [TCDS A28NM](https://openairdocs.org/tcds/A28NM) (OpenAirDocs)
- Serial number: 3656
- Year built: 2008
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 4, 2010
- Last registry action: April 22, 2024
- Mode S code: A86ACE
- Location: [None, OK](https://openairdocs.org/faa-place/OK/None)
- Owner type: Individual
- The mark today: https://openairdocs.org/aircraft/N641VA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=641VA
- Page: https://openairdocs.org/deregistered/N641VA-2024-04-22

From the FAA registry file of November 5, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Airbus A320-214: https://openairdocs.org/model/airbus-a320-214.md

## Service difficulty reports (47)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR ASAA2023090845601](https://openairdocs.org/sdr/ASAA2023090845601), Sep 8, 2023: FLOORBOARD. DELAMINATED. 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
- [SDR ASAA2023090845600](https://openairdocs.org/sdr/ASAA2023090845600), Sep 8, 2023: FLOOR PANEL. DELAMINATED. 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 53-0
- [SDR ASAA2023083146150](https://openairdocs.org/sdr/ASAA2023083146150), Aug 31, 2023: FLOOR PANEL. DAMAGED. 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), Aug 31, 2023: FLOOR PANEL. DAMAGED. 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), Aug 31, 2023: FLOOR PANEL. DAMAGED. 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), Aug 31, 2023: FLOOR PANEL. DAMAGED. 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), Aug 31, 2023: FLOORBOARD. PUNCTURED. 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), Aug 31, 2023: FLOORBOARD. DAMAGED. 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 A32
- [SDR ASAA2023083145602](https://openairdocs.org/sdr/ASAA2023083145602), Aug 31, 2023: FLOORBOARD. DAMAGED. 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 
- [SDR ASAA2023083145401](https://openairdocs.org/sdr/ASAA2023083145401), Aug 31, 2023: FLOOR PANEL. DENTED. 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
- [SDR ASAA2023083145309](https://openairdocs.org/sdr/ASAA2023083145309), Aug 31, 2023: FLOOR PANEL. PUNCTURED. 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 51-7
- [SDR ASAA2023080846088](https://openairdocs.org/sdr/ASAA2023080846088), Aug 8, 2023: SKIN. CORRODED. 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 S
- [SDR ASAA2020022753280](https://openairdocs.org/sdr/ASAA2020022753280), Feb 25, 2020: STRINGER. CORRODED. 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 
- [SDR ASAA2020011732164](https://openairdocs.org/sdr/ASAA2020011732164), Jan 17, 2020: SEAT TRACK. CORRODED. MAIN CABIN FLOOR STRUCTURE AT C16, Y254, UPPER SURFACE OF TRACK FLANGE HAS CORROSION GROUNDED - YES. REMOVED CORROSION AND CHECKED LIMITS. ORIGINAL THICKNESS IS
- [SDR ASAA2020030232315](https://openairdocs.org/sdr/ASAA2020030232315), Jan 16, 2020: STRINGER. CORRODED. 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 .
- [SDR ASAA2020012463942](https://openairdocs.org/sdr/ASAA2020012463942), Jan 16, 2020: SUPPORT. CORRODED. 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
- [SDR ASAA2020022852292](https://openairdocs.org/sdr/ASAA2020022852292), Jan 15, 2020: STRINGER. CORRODED. 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 
- [SDR ASAA2020022132224](https://openairdocs.org/sdr/ASAA2020022132224), Jan 13, 2020: FLOOR PANEL. CORRODED. 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 ALLOWABL
- [SDR ASAA2020022132223](https://openairdocs.org/sdr/ASAA2020022132223), Jan 13, 2020: FLOOR PANEL. CORRODED. 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 AL
- [SDR ASAA2020022132222](https://openairdocs.org/sdr/ASAA2020022132222), Jan 13, 2020: WEB. CORRODED. 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 
- [SDR ASAA2020022132221](https://openairdocs.org/sdr/ASAA2020022132221), Jan 13, 2020: WEB. CORRODED. 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
- [SDR ASAA202002132163](https://openairdocs.org/sdr/ASAA202002132163), Jan 13, 2020: FLOOR SUPPORT. CORRODED. 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. ORIGI
- [SDR ASAA2020021233105](https://openairdocs.org/sdr/ASAA2020021233105), Jan 13, 2020: SEAT TRACK. CORRODED. 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 R
- [SDR ASAA2020021033104](https://openairdocs.org/sdr/ASAA2020021033104), Jan 13, 2020: SEAT TRACK. CORRODED. 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 D531
- [SDR ASAA2020021032103](https://openairdocs.org/sdr/ASAA2020021032103), Jan 13, 2020: FLOORBEAM. CORRODED. 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 AI
- [SDR ASAA2020020512079](https://openairdocs.org/sdr/ASAA2020020512079), Jan 13, 2020: SEAT TRACK. CORRODED. 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 
- [SDR ASAA2020020512078](https://openairdocs.org/sdr/ASAA2020020512078), Jan 13, 2020: SEAT TRACK. CORRODED. 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), Jan 13, 2020: WEB. CORRODED. 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 A
- [SDR ASAA2020012933994](https://openairdocs.org/sdr/ASAA2020012933994), Jan 13, 2020: WEB. CRACKED. 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
- [SDR ASAA2020012433943](https://openairdocs.org/sdr/ASAA2020012433943), Jan 13, 2020: FLOOR SUPPORT. CORRODED. 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. DRIL
- [SDR ASAA2020012433941](https://openairdocs.org/sdr/ASAA2020012433941), Jan 13, 2020: FLOOR SUPPORT. CORRODED. 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 IN
- [SDR ASAA202001243940](https://openairdocs.org/sdr/ASAA202001243940), Jan 13, 2020: FLOOR SUPPORT. CORRODED. 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. 
- [SDR ASAA2020022832297](https://openairdocs.org/sdr/ASAA2020022832297), Jan 12, 2020: STRINGER. CORRODED. 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,
- [SDR ASAA2020022832296](https://openairdocs.org/sdr/ASAA2020022832296), Jan 12, 2020: STRINGER. CORRODED. 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, REMOVE
- [SDR ASAA2020022832295](https://openairdocs.org/sdr/ASAA2020022832295), Jan 12, 2020: STRINGER. CORRODED. 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
- [SDR ASAA2020022832294](https://openairdocs.org/sdr/ASAA2020022832294), Jan 12, 2020: STRINGER. CORRODED. 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 .1
- [SDR ASAA2020022832293](https://openairdocs.org/sdr/ASAA2020022832293), Jan 12, 2020: STRINGER. CORRODED. 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 .1
- [SDR ASAA2020022832291](https://openairdocs.org/sdr/ASAA2020022832291), Jan 12, 2020: STRINGER. CORRODED. 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 .1
- [SDR ASAA2020030232311](https://openairdocs.org/sdr/ASAA2020030232311), Jan 8, 2020: WEB. CORRODED. 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 DRILL
- [SDR ASAA2020030232312](https://openairdocs.org/sdr/ASAA2020030232312), Jan 7, 2020: SKIN PANEL. GOUGED. 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 R
- [SDR ASAA2018112927195](https://openairdocs.org/sdr/ASAA2018112927195), Nov 29, 2018: ACM. SEIZED. 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 RE
- [SDR VQIA2016020120005](https://openairdocs.org/sdr/VQIA2016020120005), Jan 31, 2016: ACTUATOR. FAILED. ACFT EXPERIENCED A NR 1 ENGINE COMPRESSOR VANE FAULT ON ECAM, THE FLIGHT CREW ELECTED TO RETURN TO DEPARTURE. UPON ARRIVAL TECHS ACCOMPLISHED TSM 75-30-00-810-8
- [SDR VQIA2015072400028](https://openairdocs.org/sdr/VQIA2015072400028), Jul 12, 2015: SENSOR. MALFUNCTIONED. 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 COMPR
- [SDR VQI2015F00022](https://openairdocs.org/sdr/VQI2015F00022), May 29, 2015: GIRT BAR. OBSTRUCTED. 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 N
- [SDR VQI2015F00002](https://openairdocs.org/sdr/VQI2015F00002), Dec 23, 2014: FAN. FAILED. 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
- [SDR VQI2013F00032](https://openairdocs.org/sdr/VQI2013F00032), Oct 29, 2013: BUSHING. MIGRATED. 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
- [SDR VQIA2012F00034](https://openairdocs.org/sdr/VQIA2012F00034), Sep 5, 2012: BUTTON. OUT OF ALIGNMENT. 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 MECHANI

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