# Service difficulty reports: N628VA

A list on [N628VA](https://openairdocs.org/aircraft/N628VA.md).

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

- [SDR 2023F00283](https://openairdocs.org/sdr/2023F00283.md): Unknown · unknown · Sep 20, 2023 · N628VA · Airbus A320* · Emergency Lighting
  > L2 DOOR EMERGENCY EXIT LIGHT INOPERABLE. REMOVED AND REPLACED EPSU 13WL IAW AMM 33-51-38,OPS CHECK OK
- [SDR GCXA2023012300001](https://openairdocs.org/sdr/GCXA2023012300001.md): Hydraulic Line · leaking · Jan 20, 2023 · N628VA · Airbus A320214 · Hydraulic System, Main
  > LOSS OF YELLOW HYDRAULIC SYSTEM AT CRUISE. REPLACED HYDRAULIC LINE, UNION, AND PACKINGS.
- [SDR ASAA2021100238392](https://openairdocs.org/sdr/ASAA2021100238392.md): Box Beam · cracked · Oct 2, 2021 · N628VA · Airbus A300* · Fuselage Main, Structure
  > TORSION BOX LOWER SIDE SHELL STR15 R FASTENER HOLE IS CRACKED IN PRESSURE PLATE 2ND HOLE FROM AFT PER SB A320-53-1251 FIG. A-GDAAA VIEW D GROUNDED - YES. REPAIRED IAW ASA EA A320-53EA-01109 REV. 00, DATED 12/10/2021, AIRBUS SB A320-53-1251 REV 4, DATED 05/17/
- [SDR ASAA2021100238391](https://openairdocs.org/sdr/ASAA2021100238391.md): Box Beam · cracked · Oct 2, 2021 · N628VA · Airbus A300* · Fuselage Main, Structure
  > TORSION BOX LOWER SIDE SHELL STR15 L FASTENER HOLE IS CRACKED IN PRESSURE PLATE, 5TH HOLE FROM AFT, PER SB A320-53-1251, FIG A-GDAAA VIEW D. GROUNDED - YES. REPAIRED IAW ASA EA A320-53EA-01109 REV. 00, DATED 12/10/2021, AIRBUS SB A320-53-1251 REV 4, DATED 05/1
- [SDR ASAA2021082336293](https://openairdocs.org/sdr/ASAA2021082336293.md): Reinforcement · corroded · Aug 23, 2021 · N628VA · Airbus A320214 · Fuselage Main, Structure
  > EVIDENCE OF CORROSION FOUND ON THE INTERNAL SURFACE COMMON TO THE AFT LAVATORY VENT FLANGE AND FUSELAGE SKIN GROUNDED - YES. REMOVED AND REPLACED INTERNAL DOUBLER PER A320 SRM 53-41-11-300-004, CORROSION TO SKIN WAS REPAIRED ON CUST CARD P063684
- [SDR ASAA2021082336292](https://openairdocs.org/sdr/ASAA2021082336292.md): Skin Panel · corroded · Aug 23, 2021 · N628VA · Airbus A320214 · Fuselage Main, Plate/Skin
  > EVIDENCE OF CORROSION FOUND ON THE AFT LAVATORY VENT OUTLET SKIN CUTOUT GROUNDED - YES. REPAIRED SKIN PER A320 SRM 53-41-11-300-004
- [SDR ASAA2021082336291](https://openairdocs.org/sdr/ASAA2021082336291.md): Skin Panel · corroded · Aug 23, 2021 · N628VA · Airbus A320214 · Fuselage Main, Plate/Skin
  > EVIDENCE OF CORROSION FOUND ON THE AFT LAVATORY VENT OUTLET SKIN CUTOUT GROUNDED - YES. REPAIRED SKIN PER A320 SRM 53-41-11-300-004
- [SDR ASAA2020021492176](https://openairdocs.org/sdr/ASAA2020021492176.md): Battery · no test · Feb 9, 2020 · N628VA · Airbus A320214 · Emergency Lighting
  > EMERGENCY LIGHT EPSU 11WL FAILS CAPACITY CHECK GROUNDED - YES. REMOVED & REPLACED 11WL BATTERY S/N 792862. OPS CHECK GOOD. A320 AMM 33-51-00, 33-51-38.
- [SDR ASAA2018100427721](https://openairdocs.org/sdr/ASAA2018100427721.md): Floor Support · corroded · Oct 4, 2018 · N628VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > RT FLOORBEAM FR66 - FR68 HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-42-11 AND DWG D53472172.
- [SDR ASAA2018092927720](https://openairdocs.org/sdr/ASAA2018092927720.md): Seat Track · corroded · Sep 29, 2018 · N628VA · Airbus A320214 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FWD WET AREA, SEAT TRACK CORRODED FR20 BS Y8077 RBL30, RBL-Y14 GROUNDED - YES. REMOVED DAMAGE ON SEAT TRACK, MATL REMOVED 0.015, MAX ALLOWABLE 0.012 FOUND TO BE OUT OF LIMITS PER SRM 53-00-15-283-001 FIG 001. REMOVED SEAT TRACK, SPLICE PLATE AND LIGHT
- [SDR ASAA2018092927716](https://openairdocs.org/sdr/ASAA2018092927716.md): Beam · corroded · Sep 29, 2018 · N628VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > CABIN FWD WET AREA FLOOR LONGITUDIANL BEAM CORRODED AT SCREW HOLE FR16 BS X7087, LBL22, BL+4560 GROUNDED - YES. REMOVED CORROSION AND FOUND CORROSION ON FWD CABIN WET AREA LONG BEAM DAMAGE EXCEEDED SERVICEABLE LIMITS IAW SRM 53-11-14. REMOVED FLOOR PANEL 211KF
- [SDR ASAA2018092727715](https://openairdocs.org/sdr/ASAA2018092727715.md): Floor Support · corroded · Sep 27, 2018 · N628VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > AFT CABIN FR68 AT RBL 30 THE FLOOR SUPPORT HAS CORROSION AROUND 2 CLIP NUTS. GROUNDED - YES. REMOVED DAMAGE, MAT LOSS 0.021 (0.016 MAX ALLOWABLE) AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-14. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-42-11 AND DWG 53472
- [SDR VQI2017F00019](https://openairdocs.org/sdr/VQI2017F00019.md): Unknown · odor · Jun 12, 2017 · N628VA · Airbus A320214 · Air Distribution System
  > DURING CLIMB, AN UNUSUAL ODOR WAS PRESENT IN THE FWD GALLEY, LAVATORY AREA. ALL SYSTEMS NORMAL, DISCONNECTED IFE AND ODOR DISSIPATED AFTER APPROX 20-30 MINUTES TOTAL. BOTH LAVATORY AND GALLEY AREA FULLY INSPECTED FOR SOURCE, NONE NOTED IFE REMAINED OFF FOR
- [SDR VQIA2017080900035](https://openairdocs.org/sdr/VQIA2017080900035.md): Fan · failed · Jan 20, 2017 · N628VA · Airbus A320214 · Air Distribution Fan
  > ON ARRIVAL, A BURNING ODOR FROM FWD GALLEY OVEN. MX INSPECTED AND DISCOVERED LT CABIN FAN FAULT ON ECAM AND SPLY CB X18 TRIPPED. PERFORMED INSPECTION IAW TSM 055000810831 AND FOUND LT CABIN FAN INOP WHICH CAUSED A BURNING SMELL AT FWD GALLEY OVEN. FWD GALLE
- [SDR VQI2015F00037](https://openairdocs.org/sdr/VQI2015F00037.md): Fitting · leaking · Nov 19, 2015 · N628VA · Airbus A320214 · Crew Oxygen System
  > AIRCRAFT EXPERIENCED A LOW CREW OXYGEN WARNING DURING CRUISE, THE ACFT DIVERTED FOR REPAIR. DURING TROUBLESHOOTING THE TECHS FOUND AN OXYGEN LEAK FROM THE LOW PRESSURE LINE FITTING AT THE OXYGEN BOTTLE PRESSURE REGULATOR. THE LINE WAS SECURED AND THE OXYGEN
- [SDR VQI201408040018](https://openairdocs.org/sdr/VQI201408040018.md): Controller · failed · Jul 17, 2014 · N628VA · Airbus A320214 · Cabin Pressure Controller
  > SHORTLY AFTER REACHING CRUISE ALTITUDE, THE CREW RECEIVED A CABIN PRESSURE NR 1 SYSTEM STATUS MESSAGE (CAB PR 1) DISPLAYED ON ECAM WITH AN ASSOCIATED CABIN PRESSURE "BUMP". IAW FCOM PRO-ABN-21 15/24 THE CREW CONTINUED TO DESTINATION. AFTER APPROXIMATELY 1 HR
- [SDR VQI2014F00014](https://openairdocs.org/sdr/VQI2014F00014.md): Pump · failed · May 13, 2014 · N628VA · Airbus A320214 · Hydraulic Pump (Electric/Engine), Main
  > CREW REPORTED AT INITIAL ACCELERATION, CLIMBING THRU 10000 FT, BLUE HYD OVERHEAT AND FAULT W/ASSOCIATED BLUE FLT CONTROL LOSS. CREW RETURNED TO DEPARTURE AND DECLARED AN EMERGENCY. ACFT LANDED WITHOUT INCIDENT AND TAXIIED TO THE GATE UNDER POWER. PROBLEM W
- [SDR VQI2014F00011](https://openairdocs.org/sdr/VQI2014F00011.md): Unknown · unknown · Mar 17, 2014 · N628VA · Airbus A320214 · Emergency Exits
  > LEFT OVERWING EMERGENCY EXIT DOORS ARE NOT INDICATING ARMED. MAINTENANCE RESET THE OVERWING EMERGENCY EXIT DOOR IAW AMM 52-21-11-04, NO FURTHER DISCREPANCIES NOTED AFTER SEVERAL FLIGHTS.
- [SDR VQI2013F00039](https://openairdocs.org/sdr/VQI2013F00039.md): Unknown · odor · Nov 29, 2013 · N628VA · Airbus A320214 · Air Distribution System
  > DURING CLIMB, INFLIGHT TEAM REPORTED ELECTRICAL BURNING ODOR IN CABIN. SHUTDOWN THE IFE SYSTEM. ODOR DISSIPATED AND NO OTHER ISSUES WERE NOTED. RETURNED TO DEPARTURE, LANDED UNEVENTFULLY. MX ACCOMPLISHED TSM 24-00-00-810-823A FOR ELECTRICAL BURNING ODOR
- [SDR VQIA201308090025](https://openairdocs.org/sdr/VQIA201308090025.md): Gust Lock · dirty · Jun 28, 2013 · N628VA · Airbus A320214 · Passenger/Crew Doors
  > ON ARRIVAL, L1 DOOR WAS OPENED AND NOTED THE L1 DOOR GUST LOCK WOULD NOT ENGAGE. MX REMOVED L1 DOOR LINER. CLEANED GUST LOCK MECHANISM, ROD SEAL INTO ITS NORMAL POSITION AND OPS CHECKED GOOD IAW AMM 52-11-21.
- [SDR VQIA2013F00018](https://openairdocs.org/sdr/VQIA2013F00018.md): Gust Lock · failed · Jun 20, 2013 · N628VA · Airbus A320214 · Passenger/Crew Doors
  > DISCOVERED THE L1 DOOR GUST LOCK WOULD NOT ENGAGE. MX RESECURED THE GUST LOCK ROD SEAL AND OPS CHECKED OK IAW AMM 52-11-21.
- [SDR VQI2012F00004](https://openairdocs.org/sdr/VQI2012F00004.md): Unknown · malfunctioned · Feb 7, 2012 · N628VA · Airbus A320214 · Leading Edge Slat Position Indicating System
  > DURING APPROACH AT 1815Z, CREW NOTED A F/CTL SLATS FAULT WITH NO MOVEMENT OF THE SLATS IN THE SELECTED FLAP SETTING. MC NOTED AN ASSOCIATED SLT 1 AND 2 SYS JAM CHECK SLT MECH DRIVE MESSAGE. DECLARED AN EMERGENCY. UNEVENTFUL LANDING. THE F/CTL SLATS FAULT M
- [SDR VQI2011F00017](https://openairdocs.org/sdr/VQI2011F00017.md): Check Valve · unserviceable · Aug 21, 2011 · N628VA · Airbus A320214 · Hydraulic System, Main
  > ACFT WAS OPERATING FLIGHT, AFTER MAKING A NORMAL DEPARTURE AT 00F8Z (3 MIN LATE DUE TO NON-MX ISSUES) AND TOOK OFF AT 0106Z AIRMAN REPORTED A HYD Y RSVR OVHT ALONG WITH A HYD Y ENG 2 PUMP LO PR AND SYS LO PR MESSAGE AT 0111Z. AN ACARS WAS SENT BY THE CREW AT
- [SDR VQI2011F00008](https://openairdocs.org/sdr/VQI2011F00008.md): Floor Support · corroded · May 8, 2011 · N628VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > FUSELAGE DETAIL INSP OF CABIN FLOOR STRUCTURE BELOW AFT GALLEY WAS ACCOMPLISHED. DURING THE INSP, CORROSION WAS FOUND ON 1 LONGERON BEAM (Y=464.8) WHICH EXCEEDED SRM 53-00-14 ALLOWABLE LIMITS. LONGERON BEAM (PN D53472284008) WAS REPLACED.
- [SDR VQI2011F00007](https://openairdocs.org/sdr/VQI2011F00007.md): Wire Harness · damaged · May 1, 2011 · N628VA · Airbus A320214 · Passenger Compartment Equipment
  > ACFT WAS IN FOR OVERNIGHT SCHEDULED MX. DURING THE WEEKLY CHECK, IT WAS NOTED THAT THE LAST 3 ROWS OF COACH SEATS, 24, 25, AND 26 ABC, EXIT PATH LIGHTING WOULD NOT ILLUMINATE. UPON TROUBLESHOOTING, LINE MX FOUND THAT THE CONNECTOR FIN 7260VC10 HAD BROKEN WIR

## 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 = 'N628VA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N628VA/reports

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