# N632VA: 2007 Airbus A320-214, registration cancelled 2024-03-26

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 26, 2024
- Exported to: Canada
- Status when cancelled: Valid registration
- Airframe: [Airbus A320-214](https://openairdocs.org/model/airbus-a320-214) (registry code 3940006)
- Engine: [CFM International CFM56-5B4/P series](https://openairdocs.org/engine/cfm-international-cfm56-5b4-p-series) (registry code 13011)
- Data sheets: [TCDS A28NM](https://openairdocs.org/tcds/A28NM) (OpenAirDocs)
- Serial number: 3155
- Year built: 2007
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 13, 2007
- Certificate issued: August 17, 2007
- Last registry action: January 18, 2024
- Mode S code: A84706
- Owner when cancelled: [Wells Fargo Trust Co Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20TRUST%20CO%20NA%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N632VA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=632VA
- Page: https://openairdocs.org/deregistered/N632VA-2024-03-26

From the FAA registry file of November 7, 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 (46)

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

- [SDR ASAA2024030248273](https://openairdocs.org/sdr/ASAA2024030248273), Mar 2, 2024: SLIDE. UNWANTED DEPLOY. RH OVERWING SLIDE DEPLOYED. GROUNDED - YES. REMOVED AND REPLACED RH OVERWING SLIDE S/N A156832 IAW A320 AMM 25-62-42-000-001-A AND AMM 25-62-42-400-001-A.
- [SDR ASAA2024011747371](https://openairdocs.org/sdr/ASAA2024011747371), Jan 12, 2024: UNKNOWN. UNKNOWN. SMOKE IN COCKPIT DURING MANEUVERS AT APPROX 15,000 FT. HAD SLIGHT ELECTRICAL SMELL. RAN SMOKE EVACUATION CHECKLIST WHICH SEEMED TO RESOLVE THE ISSUE. MOST NOTIC
- [SDR ASAA2023083146146](https://openairdocs.org/sdr/ASAA2023083146146), Aug 31, 2023: FLOOR PANEL. PUNCTURED. AFT CABIN 251CF HAS REPAIR NOT LISTED IN REPAIR LISTINGS GROUNDED - YES. REPAIRED AFT MAIN CABIN FLOOR PANEL 251CF IAW A320 SRM 53-02-00-283-001 AND 53-02-00-30
- [SDR ASAA2023083146144](https://openairdocs.org/sdr/ASAA2023083146144), Aug 31, 2023: FLOOR PANEL. PUNCTURED. AFT CABIN FLOOR PANEL 241JF HAS A REPAIR NOT LISTED IN REPAIR LISTINGS. GROUNDED - YES. ACCOMPLISHED REPAIR ON AFT CABIN FLOOR PANEL 241FJ IAW A320 SRM53-02-00-
- [SDR ASAA2023061743629](https://openairdocs.org/sdr/ASAA2023061743629), Jun 17, 2023: ANGLE. CORRODED. ACCESS DOOR 312AR FWD AT FUSELAGE FR71 AND DOOR JAMB HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED DOOR JAMB ANGLE AT ACCESS DOOR 312AR AT FR71 IAW A320 S
- [SDR ASAA2023060644386](https://openairdocs.org/sdr/ASAA2023060644386), Jun 6, 2023: FLOORBOARD. DELAMINATED. MAIN CABIN FLOOR BOARD 231FF HAS INSERT DAMAGE AT L/H. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR BOARD 231FF IAW A320 AMM 53-12-12-420-001-A.
- [SDR ASAA2023060544059](https://openairdocs.org/sdr/ASAA2023060544059), Jun 5, 2023: SEAT TRACK. WORN. MAIN CABIN SEAT INBD TRACK CROWN LATERAL AREA IS WORN AT FR42. GROUNDED - YES. REMOVED AND REPLACED SEAT TRACK P/N: D5337111000800 IAW A320 SRM 51-42-11/001 AND
- [SDR ASAA2023060544058](https://openairdocs.org/sdr/ASAA2023060544058), Jun 5, 2023: SEAT TRACK. WORN. MAIN CABIN OUTBD SEAT TRACK CROWN LATERAL AREA IS WORN BETWEEN FR43 AND FR44. GROUNDED - YES. REMOVED AND REPLCAED MAIN CABIN SEAT TRACK BETWEEN FR41 AND FR47 Y
- [SDR ASAA2023051846503](https://openairdocs.org/sdr/ASAA2023051846503), May 18, 2023: SKIN PANEL. CORRODED. FOUND MULTIPLE AREAS OF CORROSION ON L/H WING TOP SKIN PANEL 2 T/E OVERHANG BETWEEN RIB 14-18 GROUNDED - YES. ACCOMPLISHED EA A320-57EA-01874 REV. 00 MINOR REPA
- [SDR ASAA2023051743345](https://openairdocs.org/sdr/ASAA2023051743345), May 17, 2023: DOOR SILL. CORRODED. AFT CABIN R/H LWR SILL AT FR68 HAS CORROSION. GROUNDED - YES. ACCOMPLISHED CATEGORY "A" PERMANENT REPAIR ON AFT CABIN R/H LWR SILL AT FR68, Y=1732 IAW A320 SRM 
- [SDR ASAA2023051645209](https://openairdocs.org/sdr/ASAA2023051645209), May 16, 2023: FLOOR PANEL. DELAMINATED. MAIN CABIN FLOOR PANEL 251RF HAS MISSING MATERIAL GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR PANEL 251RF IAW A320 AMM 53-00-00-400-801-A AND 53-00-00
- [SDR ASAA2023051345989](https://openairdocs.org/sdr/ASAA2023051345989), May 13, 2023: SKIN PANEL. CORRODED. R/H WING TOP SKIN PANEL 2 T/E OVERHANG HAS EXTENSIVE CORROSION. GROUNDED - YES. ACCOMPLISHED CATEGORY B PERMANENT REPAIR OF R/H WING TOP SKIN PANEL 2 TEOH RIBS 
- [SDR ASAA2023051345909](https://openairdocs.org/sdr/ASAA2023051345909), May 13, 2023: SKIN PANEL. CORRODED. L/H WING/TOP SKIN PANEL 2 TRAILING EDGE OVERHANG HAS EXTENSIVE CORROSION THROUGHOUT GROUNDED - YES. REPAIRED L/H WING TOP SKIN OVERHANG AT RIBS 9-27, STRINGER 1
- [SDR ASAA2023051345908](https://openairdocs.org/sdr/ASAA2023051345908), May 13, 2023: SKIN PANEL. CORRODED. L/H WING/TOP SKIN PANEL 2 OVERHANG BETWEEN RIB 6 AND 27 CORROSION. GROUNDED - YES. REPAIRED L/H WING TOP SKIN TRAILING EDGE OVERHANG IAW ASA EA A320-57EA-01874 
- [SDR ASAA2023051345907](https://openairdocs.org/sdr/ASAA2023051345907), May 13, 2023: SKIN PANEL. CORRODED. L/H WING/TOP SKIN PANEL 2/TRAILING EDGE OVERHANG BETWEEN RIB 6 AND 27 CORROSION. GROUNDED - YES. REPAIRED L/H WING/TOP SKIN PANEL 2 REAR SPAR AT RIB 15-18 IAW A
- [SDR ASAA2023042046700](https://openairdocs.org/sdr/ASAA2023042046700), Apr 20, 2023: FLOOR PANEL. CORRODED. R1 DOOR THRESHOLD PLATE HAS RUST ON 3EA ATTACHING SCREW HOLES. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR PANEL 222FF AT FR16 TO FR20 P/N E5367147800
- [SDR ASAA2023042043410](https://openairdocs.org/sdr/ASAA2023042043410), Apr 20, 2023: DOOR SILL. CORRODED. AFT CARGO COMPARTMENT DOOR SILL UPPER SURFACE HAS CORROSION FROM FR55 TO FR56. GROUNDED - YES. REMOVED AND REPLACED AFT CARGO COMPARTMENT DOOR SILL/THRESHOLD SH
- [SDR ASAA2023042043333](https://openairdocs.org/sdr/ASAA2023042043333), Apr 20, 2023: WEB. CORRODED. AFT CARGO DOOR CUTOUT TORQUE BOX UPPER WEB IS CORRODED IN NUMEROUS AREA. GROUNDED - YES. REMOVED AND REPLACED AFT CARGO DOOR CUTOUT TORQUE BOX WEB P/N: D5347556
- [SDR ASAA2023042043178](https://openairdocs.org/sdr/ASAA2023042043178), Apr 20, 2023: FLOOR SUPPORT. CORRODED. AFT PIT FLOOR STRUCTURE HAS CORROSION FROM C56 TO C58 ON LEFT SIDE AFT LOOKING FWD. GROUNDED - YES. REMOVED AND REPLACED AFT PIT FLOOR SUPPORT AT FR56 TO FR58 S
- [SDR ASAA2023041543306](https://openairdocs.org/sdr/ASAA2023041543306), Apr 15, 2023: SKIN. CORRODED. R/H FUSELAGE ACCESS DOOR 312AR INNER SKIN IS CORRODED. GROUNDED - YES. REMOVED AND REPLACED INNER SKIN ON ACCESS DOOR 312AR IAW A320 SRM 51-42-11-001
- [SDR ASAA2019041429230](https://openairdocs.org/sdr/ASAA2019041429230), Apr 14, 2019: SHEAR TIE. CORRODED. MAIN CABIN FLOOR LEVEL BETWEEN FR69-FR70 STR23R LATERAL SHEAR TIE WEB CORRODED GROUNDED - YES. REMOVED CORRODED LATERAL SHEAR TIE WEB IN MAIN CABIN FLOOR LEVEL 
- [SDR ASAA2019041429229](https://openairdocs.org/sdr/ASAA2019041429229), Apr 14, 2019: SHEAR TIE. CORRODED. MAIN CABIN FLOOR LEVEL BETWEEN FR69-FR70 STR23R LATERAL SHEAR TIE WEB CORRODED GROUNDED - YES. REMOVED CORRODED LATERAL SHEAR TIE WEB IN MAIN CABIN FLOOR LEVEL 
- [SDR ASAA2019042382913](https://openairdocs.org/sdr/ASAA2019042382913), Mar 28, 2019: BEAM. CORRODED. MAIN CABIN LWR DOOR SILL SUPPORT AT R-2 DOOR, FWD OF FR68 HAS A CORRODED EXISTING REPAIR GROUNDED - YES. REMOVED DAMAGED REPAIR IAW A320 SRM 51-42-11. FABRICATE
- [SDR ASAA2019032979147](https://openairdocs.org/sdr/ASAA2019032979147), Mar 27, 2019: WEB. CORRODED. MAIN CABIN FLOOR @ FR69-FR68 R/H OUTBOARD CUSP WEB CORRODED GROUNDED - YES. BLENDED CORROSION AND FOUND OUT OF LIMITS IAW A320 SRM 53-41-14. ORIG .063 REMOVED .
- [SDR ASAA2019042372998](https://openairdocs.org/sdr/ASAA2019042372998), Mar 27, 2019: DOOR SILL. CORRODED. AFT PASSENGER/CREW RT/SIDE DOOR LOWER FWD GIRT BAR FITTING CORRODED. GROUNDED - YES. REMOVED CORROSION IAW A320 SRM 53-41-14-283-002. ORIG MAT .098, REMAINING M
- [SDR ASAA2019042372991](https://openairdocs.org/sdr/ASAA2019042372991), Mar 27, 2019: DOOR FRAME. CORRODED. L1 DOOR LOWER FRAME AT GIRT BAR LOCATION FWD HAS CORROSION (MARKED IN RED) GROUNDED - YES. REMOVED CORROSION ON L1 LOWER DOOR FRAME AT FWD GIRT BAR PER A320 SRM
- [SDR ASAA2019042372990](https://openairdocs.org/sdr/ASAA2019042372990), Mar 27, 2019: DOOR FRAME. CORRODED. R1 DOOR LOWER FRAME AT GIRT BAR304 LOCATION FWD AND AFT HAS CORROSION (MARKED IN RED) GROUNDED - YES. REMOVED CORROSION ON R1 DOOR LOWER FRAME AT FWD AND AFT GR
- [SDR ASAA2019042372989](https://openairdocs.org/sdr/ASAA2019042372989), Mar 27, 2019: FLOOR SUPPORT. CORRODED. MAIN CABIN FLOOR @FR68 RBL30 BEAM UPPER SURFACE CORRODED GROUNDED - YES. REMOVED CORROSION OUT OF SRM 53-00-14 LIMITS - DAMAGE WAS 2" LONG - ORIG THK .150", REM
- [SDR ASAA2019032729087](https://openairdocs.org/sdr/ASAA2019032729087), Mar 27, 2019: FITTING. CORRODED. AFT PASSENGER/CREW LT/SIDE DOOR LOWER FWD GIRT BAR FITTING CORRODED. GROUNDED - YES. REMOVED CORROSION AND FOUND WITHIN LIMITS IAW A320 SRM 53-41-174. ORIG .098
- [SDR ASAA20190429148](https://openairdocs.org/sdr/ASAA20190429148), Mar 25, 2019: SHEAR TIE. CORRODED. MAIN CABIN, AFT, LEFT SIDE, LATERAL SHEAR TIE STR 23L BETWEEN FRAME 69 AND 68 CORROSION GROUNDED - YES. BLENDED CORROSION AND FOUND OUT OF LIMITS IAW A320 SRM 5
- [SDR ASAA2019042352912](https://openairdocs.org/sdr/ASAA2019042352912), Mar 25, 2019: BEAM. CORRODED. AFT MAIN CABIN, R-2 DOOR THRESHOLD. DOOR SILL SUPPORT BEAM CORROSION AFT END. GROUNDED - YES. BLENDED CORROSION IAW A320 SRM 53-41-14-283-002. ORIG MAT .071 REM
- [SDR ASAA2019042352988](https://openairdocs.org/sdr/ASAA2019042352988), Mar 25, 2019: BEAM. CORRODED. AFT MAIN CABIN, FLOOR BEAM, BUTT LINE 8 L. JUST FORWARD OF FRAME 70, CORROSION ON TOP GROUNDED - YES. CORROSION LOCATED AT A HARD POINT AREA WHICH IS A EXCLUDED
- [SDR ASAA201902529061](https://openairdocs.org/sdr/ASAA201902529061), Mar 25, 2019: BRACKET. CORRODED. MAIN CABIN, AFT, LEFT SIDE, LATERAL SHEAR TIE STR 23L BETWEEN FRAME 69 AND 70 CORROSION GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN AFT LEFT SIDE LATERAL SH
- [SDR ASAA2019042252957](https://openairdocs.org/sdr/ASAA2019042252957), Mar 25, 2019: SUPPORT BEAM. CORRODED. AFT MAIN CABIN, L-2 DOOR THRESHOLD. DOOR SILL SUPPORT BEAM CORROSION AFT END. GROUNDED - YES. BLENDED CORRODED AREA. ORIGINAL MAT. THICKNESS .071, REMOVED .016,
- [SDR ASAA2018112617046](https://openairdocs.org/sdr/ASAA2018112617046), Nov 21, 2018: OIL SYSTEM. DEPLETED. ON CLIMBOUT RECEIVED ENG 2 STALL ECAM MSG. IT WENT AWAY. 30 SECONDS LATER IT SHOWED UP AGAIN. THEN OIL QUANTITY WAS DEPLETING. ENG 2 FAILED FAIL ECAM THEN SHUT 
- [SDR 2013FA0000312](https://openairdocs.org/sdr/2013FA0000312), Apr 14, 2013: SEAT TRACK. CORRODED. FORWARD CABIN SEAT TRACK FROM FR12-24 AT Y765 HAD AN AREA OF CORROSION AT FR16 BEYOND LIMITS. EXTENT OF THE DAMAGE WAS 1" IN LENGTH X 2" IN WIDTH X .032 DEPTH. 
- [SDR 2013FA0000311](https://openairdocs.org/sdr/2013FA0000311), Apr 11, 2013: SILL. CORRODED. RIGHT AFT PASSENGER DOOR SILL BETWEEN FR 66-68, ST 23-24 AT RBL 56 HAD AN AREA OF CORROSION BEYOND LIMITS. EXTENT OF DAMAGE WAS 1" IN LENGTH X 1" IN WIDTH X .05
- [SDR 2013FA0000260](https://openairdocs.org/sdr/2013FA0000260), Apr 10, 2013: SUPPORT. CORRODED. LEFT AFT SHEAR PLATE SUPPORT, FR 69-70, ST 23L-24L HAS CORROSION BEYOND LIMITS. EXTENT OF DAMAGE 2" L X 2" W X .020 DEPTH. SUPPORT BELOW A SHEAR PLATE WAS R & R
- [SDR 2013FA0000259](https://openairdocs.org/sdr/2013FA0000259), Apr 10, 2013: SHEAR PLATE. CORRODED. RIGHT AFT SHEAR PLATE BETWEEN FR 69-70, S23R HAS CORROSION BEYOND LIMITS. EXTENT OF DAMAGE 2" L X 2" W X .040 DEPTH. SHEAR PLATE WAS R & R IAW SRM 51-40-00 AND 
- [SDR VQIA2012F00000](https://openairdocs.org/sdr/VQIA2012F00000), Jan 7, 2012: UNKNOWN. ODOR. (APPROX 3.5 HRS INTO THIS FLIGHT) THE FLIGHT CREW "DETECTED STRONG CHEMICAL ODOR WHILE IN CRUISE, UNABLE TO DETERMINE ORIGIN, DIVERTED". THE FLT CREW DONNED 02 
- [SDR VQI2012F00003](https://openairdocs.org/sdr/VQI2012F00003), Dec 22, 2011: GUIDE. OUT OF POSITION. AFTER THE FLIGHT, DURING THE TURN, IT WAS NOTED THAT THE L1 DOOR WOULD NOT REMAIN LOCKED OPEN. MX WAS AT THE STATION AND FOUND THE GUIDE AND BUSHING OUT OF POSI
- [SDR VQI2012F00002](https://openairdocs.org/sdr/VQI2012F00002), Dec 22, 2011: BUSHING. OUT OF POSITION. AFTER THE FLIGHT, DURING THE TURN, IT WAS NOTED THAT THE L1 DOOR WOULD NOT REMAIN LOCKED OPEN. MX WAS AT THE STATION AND FOUND THE GUIDE AND BUSHING OUT OF POSI
- [SDR VQI2010F00001](https://openairdocs.org/sdr/VQI2010F00001), Sep 10, 2010: ACTUATOR. UNSERVICEABLE. ACFT WAS UNDERGOING A C2 CHECK. DURING THE ACCOMPLISHMENT OF MPD TASK CARD 274451-04-1, 2 DIFFERENT GREASE TYPES WERE FOUND. THE GREASES WERE WIPED CLEAN OFF TH
- [SDR VQI2009F00003](https://openairdocs.org/sdr/VQI2009F00003), Nov 13, 2009: ENGINE. FAILED. FLIGHT PUSHED BACK 6 MINUTES EARLY AT 1624Z AND TOOK OFF AT 1639Z. AT 1903Z, CUSTOMER SUPPORT CONTACTED MX, ADVISING THAT THE NR 1 ENG SHUTDOWN AT APPROX 1853Z.
- [SDR 2009FA0000012](https://openairdocs.org/sdr/2009FA0000012), Dec 30, 2008: ECU. FAULTY. FLIGHT 515 LAX TO JFK. DURING CRUISE 3 ECAM WARNINGS, THRUST LEVER FAULT, CTL VALVE FAULT, AND ENG2 FADEC A FAULT. AN ASSOCIATED LAND ASAP AMBER ECAM ADVISORY M
- [SDR VQI2008F00005](https://openairdocs.org/sdr/VQI2008F00005), Oct 30, 2008: UNKNOWN. ODOR. FLT DIVERTED DUE TO ODOR IN CABIN AROUND SEAT ROWS 4 TO 7. AT ABOUT 10,000 FT & CLIMBING ODOR FIRST NOTICED BY FLT TEAM MEMBER & THEN DISAPPEARED. LATER, AT ABO

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20081030851769I](https://openairdocs.org/incident/20081030851769I), Oct 30, 2008: Airbus A320214 (N632VA), Pittsburgh, PA, No damage. (-23) Flight 510 iad to lax diverted to pit due to smell in the cabin around seat rows 4 to 7. At about 10,000 feet and climbing the smell was first noticed by…

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