# Service difficulty reports: N630VA

A list on [N630VA](https://openairdocs.org/aircraft/N630VA.md).

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

- [SDR 2024FA0000080](https://openairdocs.org/sdr/2024FA0000080.md): Battery · discharged · Jan 31, 2024 · N630VA · Airbus A320214 · Emergency Lighting
  > L2 EMERGENCY DOOR LIGHT (EXIT SIGN) INOPERATIVE. DETERMINED BATTERY IS INOPERATIVE. REPLACEMENT PART IS ON ORDER.
- [SDR ASAA2023071344959](https://openairdocs.org/sdr/ASAA2023071344959.md): Door Sill · corroded · Jul 13, 2023 · N630VA · Airbus A320214 · Fuselage Main, Structure
  > L2 DOOR SILL FWD BLANKING PLATE ATTACH AREA AFT INBD NUTPLATE HOLE CORRODED GROUNDED - YES. ACCOMPLISHED SRM REPAIR TO DISCREPANT AREA IAW A320 SRM 53-41-14-300-001 REPAIR PRINCIPLE 11. REMOVED AND INSTALLED SIDEWALL RETAINER IAW A320 SRM 51-42-11. EVALUATED D
- [SDR ASAA2023070244955](https://openairdocs.org/sdr/ASAA2023070244955.md): Skin · dented · Jul 2, 2023 · N630VA · Airbus A320214 · Wing, Plate/Skin
  > LESSOR ITEM-LH INBOARD FLAP UPPER SURFACE HAS SMALL DENT APPROXIMATELY 4 INCHES FROM TRAILING EDGE AND 20 INCHES FROM INBOARD END GROUNDED - YES. COMPLETED EXTERNAL BONDED METAL DOUBLER REPAIR CATEGORY A PERMANENT REPAIR ON LH INBOARD FLAP UPPER SURFACE LOCAT
- [SDR ASAA2023062044975](https://openairdocs.org/sdr/ASAA2023062044975.md): Floor Support · corroded · Jun 20, 2023 · N630VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > MAIN CABIN FR20 Y-254 FLOORBOARD SUPPORT (LONGERON) ACCOMPLISHED THE REPAIR WITH WRONG SRM REPAIR. REF. G1758761 GROUNDED - YES. REMOVED AND REPLACED DUMMY RAIL P/N D5311141420200 P.O. 1061654.1 IAW A320 SRM 51-42-11 AND AIRBUS DWG# D5311406. REMOVED AND REPLA
- [SDR ASAA2023060644958](https://openairdocs.org/sdr/ASAA2023060644958.md): Skin · gouged · Jun 6, 2023 · N630VA · Airbus A320214 · Fuselage Main, Plate/Skin
  > LESSOR ITEM - BETWEEN FRAME 50 AND 51 STRG 7 AND STRG 8 THERE IS GOUGE MARK ON FUSELAGE THAT IS NOT LISTED ON DENT AND DAMAGE MAP AND LISTING GROUNDED - YES. MEASURED GOUGE FOUND BEYOND LIMITS IAW A320 SRM 53-41-11. LENGTH OF.5' WIDTH OF.5" AND DEPTH OF.02
- [SDR ASAA2023052445185](https://openairdocs.org/sdr/ASAA2023052445185.md): Door Sill · corroded · May 24, 2023 · N630VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > MAIN CABIN AFT R/H AFT FR66 FLOOR AT R2 DOOR FWD OF GIRT BAR FITTING, HAS CORROSION ON TOP OF BEAM. GROUNDED - YES. MAJOR REPAIR ACCOMPLISHED - R2 DOOR SILL MULTIPLE CORROSION AREAS - REPAIR PERFORMED PER AIRBUS DOSSIER 81233224 AND APPROVED PER AIRBUS RDAF 8
- [SDR ASAA2023052445066](https://openairdocs.org/sdr/ASAA2023052445066.md): Shear Plate · gouged · May 24, 2023 · N630VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR AFT L/H AT FR69 TO FR70, SHEAR PLATE HAS GOUGE, MARKED IN RED GROUNDED - YES. REMOVED AND REPLACED LH AFT SHEAR PLATE FROM FR69-FR70 PN D5347112420200 PO: 975781.1 IAW AIRBUS DWG D53474180, A320-SRM 51-72-11
- [SDR ASAA2023052444999](https://openairdocs.org/sdr/ASAA2023052444999.md): Shear Plate · corroded · May 24, 2023 · N630VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > RH MAIN CABIN AFT AT FR69 TO FR70, SHEAR PLATE HAS CORROSION AT FASTENER HOLES AT 3EA SPOTS, MARKED IN RED GROUNDED - YES. REMOVED AND REPLACED SHEAR PLATE R/H MAIN CABIN AT FR69 TO FR70 IAW A320 SRM 51-42-11 AND A320 DWG 18 D53474180 REV. U P/N:D534711242030
- [SDR ASAA2023052444998](https://openairdocs.org/sdr/ASAA2023052444998.md): Floorbeam · corroded · May 24, 2023 · N630VA · Airbus A320214 · Fuselage Main, Floor Beam
  > MAIN CABIN AFT R/H AT FR 66, FLOOR BEAM 2ND FROM CENTER, HAS CORROSION ON TOP OF BEAM. MARKED IN RED GROUNDED - YES. REMOVED AND REPLACED FLOOR BEAM IAW ASA A320 SRM 51-42-11/001 AND DWG D53472284 ISSUE A AT RH SIDE FR 66 -Y464.8, IAW A320 SRM 51-72-11
- [SDR ASAA2023052444957](https://openairdocs.org/sdr/ASAA2023052444957.md): Floorbeam · corroded · May 24, 2023 · N630VA · Airbus A320214 · Fuselage Main, Floor Beam
  > MAIN CABIN LH AT FR 67 FLOOR ON BEAM 3RD FROM CENTER, HAS 2 EA SPOT OF CORROSION ON TOP OF BEAM, MARKED IN RED GROUNDED - YES. REMOVED CORROSION ON LH FLOOR BEAM AT FR 67 21 INCHES AFT OF FWD SPLICE ORIGINAL THICKNESS.170 REMOVED.016 REMAINING OF.154.
- [SDR ASAA2023052444757](https://openairdocs.org/sdr/ASAA2023052444757.md): Floorbeam · corroded · May 24, 2023 · N630VA · Airbus A320214 · Fuselage Main, Floor Beam
  > MAIN CABIN AFT R/H AT FR68, FLOOR BEAM 2ND FROM CENTER, HAS CORROSION ON TOP OF BEAM. MARKED IN RED GROUNDED - YES. REMOVED AND REPLACED RH FLOOR BEAM AT FR68 2ND FROM CENTER- Y464.8 IAW ASA A320 SRM 51-42-11 AND AIRBUS DWG D53472095 ISSUE E
- [SDR ASAA2023052444756](https://openairdocs.org/sdr/ASAA2023052444756.md): Door Sill · corroded · May 24, 2023 · N630VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > MAIN CABIN L/H AT FR68 FLOOR AT L2 DOOR, HAS CORROSION AT 4EA FASTENER HOLES, MARKED IN RED GROUNDED - YES. REMOVED CORROSION AND REPAIRED DAMAGE AREA AT FR68 L/H SIDE ON L2 DOOR SILL IAW ASA A320 SRM 53-41-14-300--001 ORIGINAL MATERIAL THICKNESS IS.063 AT N
- [SDR ASAA2023052444755](https://openairdocs.org/sdr/ASAA2023052444755.md): Floor Support · corroded · May 24, 2023 · N630VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > MAIN CABIN AFT R/H FROM FR 67 TO FR 68, FLOOR BEAM 3RD FROM CENTER, HAS CORROSION ON TOP OF BEAM. MARKED IN RED. GROUNDED - YES. REMOVED AND REPLACED FLOOR BEAM RH SIDE AT FR 67 3RD FROM CENTER -Y969.0 IAW ASA SRM 51-42-11 AND AIRBUS DWG D53472193 ISSUE A
- [SDR ASAA2023052444748](https://openairdocs.org/sdr/ASAA2023052444748.md): Floorbeam · corroded · May 24, 2023 · N630VA · Airbus A320214 · Fuselage Main, Floor Beam
  > MAIN CABIN AFT R/H AFT FR 66, FLOOR BEAM 3RD FROM CENTER, HAS CORROSION ON TOP OF BEAM, MARKED IN RED. GROUNDED - YES. REMOVED AND REPLACED FLOOR BEAM R/H SIDE FR 64-66 -Y765 IAW ASA A320 SRM 51-72-11-911-001 AND DWG D53472209 ISSUE F
- [SDR ASAA2023052444747](https://openairdocs.org/sdr/ASAA2023052444747.md): Floorbeam · corroded · May 24, 2023 · N630VA · Airbus A320214 · Fuselage Main, Floor Beam
  > MAIN CABIN AFT R/H AFT FR 68, FLOOR BEAM 4TH FROM CENTER HAS CORROSION ON TOP OF BEAM. MARKED IN RED. GROUNDED - YES. REMOVED AND REPLACED RH FLOOR BEAM AT FR 68 4TH FROM CENTER -Y 1162.5 IAW ASA A320 SRM 51-72-11
- [SDR ASAA2023052444663](https://openairdocs.org/sdr/ASAA2023052444663.md): Floorbeam · corroded · May 24, 2023 · N630VA · Airbus A320214 · Fuselage Main, Floor Beam
  > MAIN CABIN AFT WET AREA FLOORS STRUCTURE UNDER FLOORBOARD 261JG BETWEEN FRAMES 69 AND 70 APPROX 3 INCHES RIGHT FROM CENTER BUTTLINE HAS CORROSION. DOT ATTACHED. CIRCLED IN RED GREASAE PEN. GROUNDED - YES. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM A320
- [SDR ASAA2023052344956](https://openairdocs.org/sdr/ASAA2023052344956.md): Floor Panel · delaminated · May 23, 2023 · N630VA · Airbus A320214 · Fuselage Floor Panel
  > AFT WET AREA FLOOR PNL 261AC DELAMINATED GROUNDED - YES. FABRICATED NEW FLOOR PANEL 261AG IAW A320 SRM 53-02-00-300-011 AND GILL CORPORATION MANUAL TGC IRM 9701-REV L FH: 47561:57, FC:15607,WTV:010
- [SDR ASAA2021090736238](https://openairdocs.org/sdr/ASAA2021090736238.md): Skin Panel · corroded · Sep 7, 2021 · N630VA · Airbus A320214 · Wing Miscellaneous Structure
  > SUBSURFACE CORROSION INDICATIONS FOUND: L/H WING LOWER SURFACE T/E OVERHANG, MARKED 1.5" X 3" STA5512 / RIB10. DOT:A374 GROUNDED - YES. REMOVED CORROSION AND CHECKED LIMITS. ORIGINAL THICKNESS IS.197, REMAINING IS.146,.051 WAS REMOVED. OUT OF LIMITS REF A32
- [SDR ASAA2019021298143](https://openairdocs.org/sdr/ASAA2019021298143.md): Support · corroded · Jan 9, 2019 · N630VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > AFT WET AREA, AFT OF L2 DOOR, FLOOR STRUCTURE FRAME SUPPORT HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED FRAME SUPPORT IAW A320 SRM 51-42-11 REF AIRBUS DWG #D53474180. NO ALLOWABLE LIMITS GIVEN IN A320 SRM.
- [SDR ASAA2019040188804](https://openairdocs.org/sdr/ASAA2019040188804.md): Floor Support · corroded · Jan 8, 2019 · N630VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > AFT CABIN UNDER FLOOR COMPARTMENT FLOOR BEAM HAS CORROSION ON TOP SURFACE AT FRAME C66 RBL1473 MM ADJACENT TO R2 DOOR. ATTACHED. GROUNDED. REMOVED CORROSION IAW SRM 53-41-14-283-002. ORIG. MAT S.150, REMAINING MAT IS.00. 100% MAT LOSS. REMOVED DAMAGED AREA A
- [SDR ASAA2019040102803](https://openairdocs.org/sdr/ASAA2019040102803.md): Floor Support · corroded · Jan 8, 2019 · N630VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > AFT CABIN UNDERFLOOR COMPARTMENT FLOOR BEAM HAS CORROSION ON TOP SURFACE AT FRAME C66 RBL735MM ADJACENT TO R2 DOOR. STREAMER ATTACHED. GROUNDED - YES. REMOVED AND REPLACED FLOOR BEAM IAW A320 SRM 51-42-11 REF AIRBUS DWG #D53472836.
- [SDR ASAA2019010827987](https://openairdocs.org/sdr/ASAA2019010827987.md): Floorbeam · corroded · Jan 8, 2019 · N630VA · Airbus A320214 · Fuselage Main, Floor Beam
  > AFT CABIN UNDERFLOOR COMPARTMENT FLOORBEAM HAS CORROSION ON TOP SURFACE AT FRAME C66 RBL1300MM ADJACENT TO R2 DOOR. GROUNDED - YES. REMOVED AND REPLACED FLOORBEAM SUPPORT PER SRM 51-42-11 AND DWG D53472840
- [SDR ASAA2019040178805](https://openairdocs.org/sdr/ASAA2019040178805.md): Shear Plate · corroded · Jan 7, 2019 · N630VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > AFT MAIN CABIN RH LATERAL SHEAR PLATE HAS CORROSION UPPER SURFACE STA.69 TO 70 GROUNDED - YES. REMOVED AND REPLACED SHEAR PLATE IAW A320 SRM 51-42-11 REF AIRBUS DWG D53474180. OPS CHECK PERFORMED IAW A320 AMM 38-31-36-710-050-A
- [SDR ASAA2019010728608](https://openairdocs.org/sdr/ASAA2019010728608.md): Door Sill · corroded · Jan 7, 2019 · N630VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > MAIN CABIN R2 DOOR SILL HAS CORROSION 2" AFT STA.69 @ I/B FASTENER HOLE UPPER SURFACE GROUNDED - YES. ACCOMPLISHED DOUBLER REPAIR IAW SRM 53-41-14-300-01. EVALUATED CORROSION - ORIGINAL THICKNESS.063, REMAINING.00, MAT'L LOSS.063 AND FOUND TO BE OUT OF LIMI
- [SDR ASAA2019010727989](https://openairdocs.org/sdr/ASAA2019010727989.md): Floor Support · corroded · Jan 7, 2019 · N630VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT STRUCTURE APPROX 7" FWD OF FRAME 70 AT LBL 7 FLOOR BOARD SUPPORT BEAM UPPER SURFACE IS CORRODED GROUNDED - YES. REMOVED AND REPLACED FLOOR BEAM SUPPORT PER SRM 51-42-11 AND DWG D53472780.
- [SDR ASAA2019010727988](https://openairdocs.org/sdr/ASAA2019010727988.md): Shear Plate · corroded · Jan 7, 2019 · N630VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > AFT MAIN CABIN LT LATERAL SHEAR PLATE HAS CORROSION UPPER SURFACE STA 69 TO 70 GROUNDED - YES. REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-42-11 REF DWG D53474180.
- [SDR ASAA2019010628673](https://openairdocs.org/sdr/ASAA2019010628673.md): Dummy Rail · corroded · Jan 6, 2019 · N630VA · Airbus A320214 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN DUMMY RAIL AT STA. Y-81 HAS CORROSION AT FR16 GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN DUMMY RAIL IAW SRM 51-42-11 AND SRM 51-72-11. REMOVED CORROSION, ORIGINAL THICKNESS.149, REMOVED.038, REMAINING.111 AND FOUND TO BE OUT OF LIMITS IAW SR
- [SDR ASAA2019010628672](https://openairdocs.org/sdr/ASAA2019010628672.md): Seat Track · corroded · Jan 6, 2019 · N630VA · Airbus A320214 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK AT STA. Y-1292 HAS CORROSION AT FR16 AND 10" AFT GROUNDED - YES. REMOVED CORROSION - ORIGINAL.087, REMOVED.040, REMAINING.047 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-11-15. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-42-11 AND SRM 51-7
- [SDR ASAA2019010628607](https://openairdocs.org/sdr/ASAA2019010628607.md): Seat Track · corroded · Jan 6, 2019 · N630VA · Airbus A320214 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK AT STA.Y-765 HAS CORROSION AT FR16 GROUNDED - YES. REMOVED CORROSION FROM EDGE OF FLANGE, ORIGINAL WIDTH.787, REMOVED.075 AND REMAINING.712 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-11-15 (NO ALLOWABLE DAMAGE CRITERIA GIVEN FOR EDGE REM
- [SDR ASAA2019010628606](https://openairdocs.org/sdr/ASAA2019010628606.md): Dummy Rail · corroded · Jan 6, 2019 · N630VA · Airbus A320214 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN DUMMY RAIL AT STA.Y-254 HAS CORROSION AT FR16 GROUNDED - YES. ACCOMPLISHED DOUBLER REPAIR TO FLOOR SUPPORT IAW SRM 53-00-14-300-007 REMOVED CORROSION - ORIGINAL THICKNESS.079, REMOVED.045, REMAINING.034 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-1
- [SDR VQI20201711010053](https://openairdocs.org/sdr/VQI20201711010053.md): Control Unit · failed · Sep 14, 2017 · N630VA · Airbus A320214 · Electrical Power System
  > THE FLIGHT CREW REPORTED AN ELECTRICAL BURNING ODOR IN THE FLIGHT DECK, ASSOCIATED WITH POWER TRANSFER BETWEEN GROUND AND APU ELECTRICAL POWER. DURING TROUBLESHOOTING THE GAPCU UNIT WAS DISCOVERED FAILED, THE UNIT WAS REPLACED AND THE AIRCRAFT WAS RETURNED T
- [SDR VQI2017F00008](https://openairdocs.org/sdr/VQI2017F00008.md): Unknown · odor · May 16, 2017 · N630VA · Airbus A320214 · Air Distribution System
  > A FUEL ODOR IN THE CABIN DURING TAXI TO TAKEOFF. RETURNED TO THE GATE, ACCOMPLISHED TSM 055000810831A WITH NO FINDINGS. THE ACFT CONTINUED TO ITS DESTINATION WITHOUT FURTHER ISSUE. NO REPORTS OF ODOR ON SUBSEQUENT FLIGHTS.
- [SDR VQIA201508260032](https://openairdocs.org/sdr/VQIA201508260032.md): Reservoir · low pressure · Aug 11, 2015 · N630VA · Airbus A320214 · Escape Slide
  > ACFT WAS BEING TOWED FROM REMOTE SPOT TO THE GATE BY MAINTENANCE, WHEN THE FOLLOWING DEFECT WAS DISCOVERED: RT OVERWING SLIDE PRESSURE LOW. R & R RT OVERWING SLIDE RESERVOIR IAW AMM 25-62-46. OPS CHECKED GOOD.
- [SDR 2013FA0000158](https://openairdocs.org/sdr/2013FA0000158.md): Support · corroded · Feb 12, 2013 · N630VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > RIGHT SHEAR PLATE SUPPORT BETWEEN FR69-70, ST 23-24 RT CORRODED BEYOND LIMITS. EXTENT OF DAMAGE 2"L X 2"W X.040" D.
- [SDR 2013FA0000157](https://openairdocs.org/sdr/2013FA0000157.md): Support · corroded · Feb 12, 2013 · N630VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > LEFT SHEAR PLATE SUPPORT BETWEEN FR69-70, ST 23-24 LT CORRODED BEYOND LIMITS. EXTENT OF DAMAGE 2"L X 2" W, X.020"D.
- [SDR 2013FA0000156](https://openairdocs.org/sdr/2013FA0000156.md): Shear Plate · corroded · Feb 9, 2013 · N630VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > LEFT AFT SHEAR PLATE BETWEEN FR 69-70, ST 23-24 LEFT CORRODED BEYOND LIMITS. EXTENT OF DAMAGE 1"L X 1"W X.025" D.
- [SDR 2013FA0000155](https://openairdocs.org/sdr/2013FA0000155.md): Shear Plate · corroded · Feb 9, 2013 · N630VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > RT AFT SHEAR PLATE BETWEEN FR 69-70, ST23-24, RT CORRODED BEYOND LIMITS. EXTENT OF DAMAGE, 2" L X 2" W X.030" D.
- [SDR VQI2008F00000](https://openairdocs.org/sdr/VQI2008F00000.md): Stringer · damaged · Jan 11, 2008 · N630VA · Airbus A320214 · Fuselage Main, Longeron/Stringer
  > ON APPROACH, AC SUSTAINED LIGHTING STRIKE, DAMAGING THE FUSELAGE SKIN FASTENER. LOCATION OF DAMAGE STRINGER 41, RT 4.40 INCHED AFTER FRAME 25. FASTENER REQUIRED REPLACEMENT AND STRINGER REPAIR. ADDITIONALLY, THE LT FWD NLG DOOR AND LT AFT NLG DOOR, RT WING

## 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 = 'N630VA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N630VA/reports

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