# Service difficulty reports: N835VA, cancelled Mar 15, 2023

A list on [N835VA, cancelled Mar 15, 2023](https://openairdocs.org/deregistered/N835VA-2023-03-15.md).

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

- [SDR ASAA2022121741199](https://openairdocs.org/sdr/ASAA2022121741199.md): Light · failed · Dec 17, 2022 · N835VA · Airbus A320214 · Emergency Lighting
  > SEVERAL EMERGENCY EXIT LIGHTS INOP. GROUNDED - YES. REMOVED AND REPLACED EXIT SIGN LIGHTS AT L1 DOOR, L2 DOOR, R2 DOOR AND EMERGENCY POWER SUPPLY UNIT (EPSU) ON POSITION 10WL IAW A320 AMM 33-51-13-000-001-A, 33-51-38-000-001-A AND 33-51-38-400-001-A. PERFORMED
- [SDR ASAA2022120141046](https://openairdocs.org/sdr/ASAA2022120141046.md): Fitting · corroded · Dec 1, 2022 · N835VA · Airbus A320214 · Emergency Equipment
  > R2 DOOR FWD GIRT BAT FITTING FLOOR PANEL UPPER SKIN IS CORRODED. GROUNDED - YES. REMOVED AND REPLACED R2 DOOR FWD GIRT BAR FITTING FLOOR PANEL IAW SRM 51-42-11 REV. 143.
- [SDR ASAA2022111041183](https://openairdocs.org/sdr/ASAA2022111041183.md): Floor Panel · delaminated · Nov 10, 2022 · N835VA · Airbus A320214 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 241JF HAS AREA OF DELAMINATION. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR PANEL 241JF PER A320 AMM 53-00-00-801-A02.
- [SDR ASAA2022111041180](https://openairdocs.org/sdr/ASAA2022111041180.md): Floor Panel · delaminated · Nov 10, 2022 · N835VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR PANEL 221EF HAS SEVERAL AREAS OF DELAM. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR PANEL 221EF IAW A320 SRM 53-00-283-00 PG 6.
- [SDR ASAA2022111041179](https://openairdocs.org/sdr/ASAA2022111041179.md): Floor Panel · delaminated · Nov 10, 2022 · N835VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR PANEL 231VF HAS AREA OF DELAMINATION. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR PANEL 231VF IAW A320 AMM 53-00-00-400-801-A.
- [SDR ASAA2022111041143](https://openairdocs.org/sdr/ASAA2022111041143.md): Floor Panel · delaminated · Nov 10, 2022 · N835VA · Airbus A320214 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 241JF HAS AREA OF DELAMINATION. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR PANEL 241JF PER A320 AMM 53-00-00-801-A02. ORIG SUB DATE: 12/16/2022
- [SDR ASAA2022111041124](https://openairdocs.org/sdr/ASAA2022111041124.md): Floorboard · delaminated · Nov 10, 2022 · N835VA · Airbus A320214 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD 231AF HAS AREA OF DELAMINATION. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOORBOARD 231AF IAW A320 AMM 53-00-00-000-801-A02 AND AMM 53-00-00-400-801-A02.
- [SDR ASAA2022111041123](https://openairdocs.org/sdr/ASAA2022111041123.md): Floorboard · delaminated · Nov 10, 2022 · N835VA · Airbus A320214 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD 231KF HAS AREA OF DELAMINATION. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOORBOARD 231KF IAW A320 AMM 53-00-00-000-801-A03 AND AMM 53-00-00-400-801-A02.
- [SDR ASAA2022111041122](https://openairdocs.org/sdr/ASAA2022111041122.md): Floor Panel · delaminated · Nov 10, 2022 · N835VA · Airbus A320214 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 231BF HAS AREA OF DELAMINATION. GROUNDED - YES. REMOVED AND REPLACED CABIN FLOOR PANEL 231BF IAW A320 53-00-00-00-801-A02 AND AMM 53-00-00-400-801-A03.
- [SDR ASAA2022111041121](https://openairdocs.org/sdr/ASAA2022111041121.md): Floor Panel · delaminated · Nov 10, 2022 · N835VA · Airbus A320214 · Fuselage Floor Panel
  > FLOOR PANEL 231QF HAS AREA OF DELAMINATION. GROUNDED - YES. REMOVED AND REPLACED CABIN FLOOR PANEL 231QF IAW A320 AMM 53-00-00-000-801-A02 AND AMM 53-00-00-400-801-A02.
- [SDR ASAA2022110640688](https://openairdocs.org/sdr/ASAA2022110640688.md): Floor Support · corroded · Nov 6, 2022 · N835VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > MAIN FLOOR "L" BEAM AT FR68 AND -Y1162.5 HAS CORROSION ON TOP OF BEAM. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR "L" BEAM AT FR68-69 Y=-1162.5 PAER A320 SRM 53-41-14-01-A REV. 142 AND 51-42-11/001 REV. 142.
- [SDR ASAA2022120340888](https://openairdocs.org/sdr/ASAA2022120340888.md): Floor Panel · cracked · Nov 3, 2022 · N835VA · Airbus A320214 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 131GF HAS A PUNCTURE. GROUNDED - YES. ACCOMPLISHED PERMANENT REPAIR OF MAIN CABIN FLOOR PANEL 131GF IAW A320 SRM 53-02-00-300-004 AND SRM A320 53-02-00-283-001 REV 142-01 AUG 2022.
- [SDR ASAA2022110141178](https://openairdocs.org/sdr/ASAA2022110141178.md): Floor Panel · punctured · Nov 1, 2022 · N835VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR 232SF LARGE PUNCTURE THROUGH COMPOSITE CORE AT FR29. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR BOARD 232SF AT FR29 IAW A320 AMM 53-00-00-400-801-A-01.
- [SDR ASAA2022103040543](https://openairdocs.org/sdr/ASAA2022103040543.md): Profile · corroded · Oct 30, 2022 · N835VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > FORWARD CARGO R/H OUTBOARD FLOOR SUPPORT FRAME UPPER SURFACE HAS CORROSION FR31 TO FR34. GROUNDED - YES. REMOVED AND REPLACED NEW PROFILE PLATE AT FR31 TO FR34 AND Y765 IAW A320 SRM REV 142 53-21-14-03-A ITEM 15 AND SRM 51-72-11-911-001.
- [SDR ASAA2022102940991](https://openairdocs.org/sdr/ASAA2022102940991.md): Floorboard · corroded · Oct 29, 2022 · N835VA · Airbus A320214 · Fuselage Floor Panel
  > L2 DOOR FLOORBOARD UPPER SKIN CORRODED BETWEEN FR66 AND FR68. GROUNDED - YES. REMOVED AND REPLACED FLOORBOARD PANEL 261LG BETWEEN FR66 AND FR68 IAW A320 SRM 53-02-00-233-001.
- [SDR ASAA2022102940990](https://openairdocs.org/sdr/ASAA2022102940990.md): Floorboard · corroded · Oct 29, 2022 · N835VA · Airbus A320214 · Fuselage Floor Panel
  > R2 DOOR FLOORBOARD LOWER SKIN CORRODED AT FR68. GROUNDED - YES. REMOVED AND REPLACED R2 DOOR FLOORBOARD AT FR66 - FR68 IAW A320 SRM 53-02-00-233-001.
- [SDR ASAA2022102940958](https://openairdocs.org/sdr/ASAA2022102940958.md): Fitting · gouged · Oct 29, 2022 · N835VA · Airbus A320214 · Fuselage Main, Attach Fittings
  > MAIN CABIN FLOOR RH OUTBD FLOORBOARD FITTING UPPER SURFACE GOUGED AT FR70 GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR RH OUTBD FLOORBOARD FITTING AT FR70 IAW A320 SRM 51-72-11-911-002
- [SDR ASAA2022102940957](https://openairdocs.org/sdr/ASAA2022102940957.md): Shear Plate · corroded · Oct 29, 2022 · N835VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > MAIN CABIN LH AFT FLOOR SHEAR PLATE UPPER SURFACE CORRODED AT FR70 GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR LH AFT SHEAR PLATE UPPER SURFACE AT FR70 STGR 22L
- [SDR ASAA2022102940914](https://openairdocs.org/sdr/ASAA2022102940914.md): Shear Tie · corroded · Oct 29, 2022 · N835VA · Airbus A320214 · Fuselage Internal Mounting Structure
  > MAIN CABIN OUTBD SHEAR PLATE IS CORRODED AT UPPER SURFACE FR70. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN R/H OUTBD SHEAR PLATE AT FR70 IAW SRM 51-42-11 REV. 142 01 AUG 2022.
- [SDR ASAA2022102940913](https://openairdocs.org/sdr/ASAA2022102940913.md): Floorbeam · corroded · Oct 29, 2022 · N835VA · Airbus A320214 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOORBEAM UPPER SURFACE CORRODED BETWEEN FR67 AND FR68 RBL 24. GROUNDED - YES. REMOVED AND REPLACED 1EA FLOORBEAM IN MAIN CABIN AT RBL24 FR67 - FR70 IAW A320 SRM 54-41-14-01-A AND SRM 51-42-11/001 REV. 26 01 AUG 2022.
- [SDR ASAA2022102940910](https://openairdocs.org/sdr/ASAA2022102940910.md): Floorbeam · corroded · Oct 29, 2022 · N835VA · Airbus A320214 · Fuselage Main, Floor Beam
  > MAIN CABIN OUTBD FLOORBEAM UPPER SURFACE HAS CORROSION IN 2EA PLACES AT FR68 JUST INBD OF GIRT BAR FITTING. GROUNDED - YES. ACCOMPLISHED CATEGORY "A" PERMANENT REPAIR AT MAIN CABIN R/H OUTBD DOOR SILL AT FR68 IAW SRM 53-41-14-80-A AND SRM 53-41-14-300-001 REV.
- [SDR ASAA2022122741253](https://openairdocs.org/sdr/ASAA2022122741253.md): Floorboard · corroded · Oct 27, 2022 · N835VA · Airbus A320214 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD AT R1 DOOR HAS CORROSION PANEL 222FF. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOORBOARD AT R1 DOOR PANEL 222FF IAW A320 AMM 53-00-00-400-801-A.
- [SDR ASAA2022102741177](https://openairdocs.org/sdr/ASAA2022102741177.md): Floorboard · corroded · Oct 27, 2022 · N835VA · Airbus A320214 · Fuselage Floor Panel
  > MAIN CABIN FLOOR BOARD FWD CABIN L1 DOOR ENTRY 221FF HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR BOARD 221FF AT L1 DOOR ENTRY WAY IAW A320 AMM 53-00-00-000-801-A.
- [SDR ASAA2022102741030](https://openairdocs.org/sdr/ASAA2022102741030.md): Fitting · corroded · Oct 27, 2022 · N835VA · Airbus A320214 · Fuselage Main, Attach Fittings
  > R1 DOOR CUTOUT HAS 3EA AREAS OF CORROSION UNDER LWR SCUFF PLATE GROUNDED - YES. REMOVED AND REPLACED CORRODED FITTING IAW A320 SRM 51-42-11 REV 143 01 NOV 2022
- [SDR ASAA2022102740956](https://openairdocs.org/sdr/ASAA2022102740956.md): Floorboard · damaged · Oct 27, 2022 · N835VA · Airbus A320214 · Fuselage Floor Panel
  > L/H SIDE CAPT SEAT FLOOR PANEL FWD CORNER BROKEN OFF GROUNDED - YES. REMOVED AND REPLACED CAPT SEAT FLOOR PANEL 211HF IAW A320 AMM 53-12-11-400-001.
- [SDR ASAA2022102740890](https://openairdocs.org/sdr/ASAA2022102740890.md): Floorboard · delaminated · Oct 27, 2022 · N835VA · Airbus A320214 · Fuselage Floor Panel
  > FLOORBOARD HAS DELAM FWD CABIN PANEL 221EF. GROUNDED - YES. ACCOMPLISHED PERMANENT REPAIR ON MAIN CABIN FLOORBOARD 221EF IAW A320 SRM 53-02-00-283-001 REV 142 01 AUG 2022 AND SRM 53-02-00-300-001 FIG 001.
- [SDR ASAA2022102541018](https://openairdocs.org/sdr/ASAA2022102541018.md): Blanking Plate · corroded · Oct 25, 2022 · N835VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > LH AFT PASSENGER DOOR FLOOR HAS CORROSION AT FWD GIRT BAR GROUNDED - YES. REMOVED AND REPLACED FWD GIRT BAR BLANKING PLATE AT LH AFT PASSSENGER DOOR IAW A320 AMM 53-13-31-400-003-A
- [SDR ASAA2022102041113](https://openairdocs.org/sdr/ASAA2022102041113.md): Blanking Plate · corroded · Oct 20, 2022 · N835VA · Airbus A320214 · Service Doors
  > CORROSION ON AFT R/H PASSENGER DOOR LOWER PLATE BELOW AFT GIRT BAR FITTING. GROUNDED - YES. REMOVED AND REPLACED BLANKING PLATE IAW A320 AMM 52-16-31-400-003-A AND AMM 52-13-00-800-001-A.
- [SDR ASAA2022102040955](https://openairdocs.org/sdr/ASAA2022102040955.md): Support Frame · corroded · Oct 20, 2022 · N835VA · Airbus A320214 · Fuselage Main, Structure
  > FWD CARGO L/H FLOOR SUPPORT FRAME HAS CORROSION ON UPPER SKIN AND RIVET SHEARED FR31 TO FR34 GROUNDED - YES. REMOVED AND REPLACED FWD CARGO L/H OUTBD FLOOR SUPPORT FRAME AT FR31 TO FR34 Y=765 IAW A320 SRM 53-21-41-03-A REV 142 01 AUG 2022 AND SRM 51-42-11 REV
- [SDR ASAA2022102040873](https://openairdocs.org/sdr/ASAA2022102040873.md): Floor Support · cracked · Oct 20, 2022 · N835VA · Airbus A320214 · Fuselage Main, Structure
  > FWD CARGO L/H OUTBD FLOOR SUPPORT FRAME IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED FWD CARGO L/H OUTBD FLOOR SUPPORT BETWEEN FR28 - FR31 AND Y = 765 IAW A320-200 SRM REV. 142 DATE 01 AUG 2022 TASK 51-72-11-911-002 AND SRM 53-21-14-03-A ITEM 005.
- [SDR ASAA2022102040872](https://openairdocs.org/sdr/ASAA2022102040872.md): Web · corroded · Oct 20, 2022 · N835VA · Airbus A320214 · Cargo/Baggage Doors
  > AFT CARGO DOOR SILL BOX UPPER WEB CORRODED AT FR53. GROUNDED - YES. REMOVED AND REPLACED AFT CARGO SILL UPPER WEB BETWEEN FR52 - FR56 PER A320 SRM 53-51-49-07-A.
- [SDR ASAA2022102040805](https://openairdocs.org/sdr/ASAA2022102040805.md): Web · corroded · Oct 20, 2022 · N835VA · Airbus A320214 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR SILL BOX UPPER WEB CORRODED AT FR53. GROUNDED - YES. REMOVED AND REPLACED AFT CARGO DOOR SILL UPPER WEB BETWEEN FR52 - FR56 A320 SRM 53-41-49-07-A.
- [SDR ASAA2022101840889](https://openairdocs.org/sdr/ASAA2022101840889.md): Floor Panel · delaminated · Oct 18, 2022 · N835VA · Airbus A320214 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 232DF HAS R/H FWD CORNER HAS DELAMINATION. GROUNDED - YES. ACCOMPLISHED PERMANENT REPAIR ON MAIN CABIN FLOOR PANEL 232DF AT FR20 IAW A320 SRM ADL 53-12-00-283-005 FIG 001 AND SRM 53-12-00-300-002 RV 142 01 AUG 2022.
- [SDR ASAA2022071439118](https://openairdocs.org/sdr/ASAA2022071439118.md): Sliding Window · scratched · Jul 14, 2022 · N835VA · Airbus A320214 · Flight Compartment Windows
  > F/O SLIDING WINDOW HAS MANY SCRATCHES GROUNDED - YES. REMOVED AND REPLACED F/O SLIDING WINDOW IAW A320 AMM 56-12-11-000-002-A. OPS CHECK GOOD.
- [SDR ASAA2022021537741](https://openairdocs.org/sdr/ASAA2022021537741.md): Fitting · cracked · Feb 15, 2022 · N835VA · Airbus A320214 · Nacelle/Pylon Structure
  > WHILE ACCOMPLISHING TC 545400-01-1-VAM LH UPPER SPAR.C001, FOUND OUTBD CORNER FITTING CRACKED AREA 6. GROUNDED - YES. REMOVED AND REPLACED OUTBD CORNER FITTING ON LH PYLON AFT FIXED FAIRING UPPER SPAR RIB 15. ALL WORK ACCOMPLISHED PER TC 545400-01-1-VAM. LH RE
- [SDR ASAA2022021537740](https://openairdocs.org/sdr/ASAA2022021537740.md): Fitting · cracked · Feb 15, 2022 · N835VA · Airbus A320214 · Nacelle/Pylon Structure
  > DURING TC 545400-01-1-VAM RH UPPER SPAR FOUND 3 CRACKS IN AREA 4 AND 1 CRACK IN AREA 6 OUTBOARD CORNER FITTING REF STEP 20 & 21 GROUNDED - YES. ACCOMPLISHED PERMANENT REPAIR ON RH PYLON AFT FIXED UPPER SPAR BETWEEN RIB 14-15 PER TC 545400-01-1-VAM RH REPAIRS.
- [SDR VQIA2017F00002](https://openairdocs.org/sdr/VQIA2017F00002.md): Unknown · odor · Mar 31, 2017 · N835VA · Airbus A320214 · Air Distribution System
  > SHORTLY AFTER TAKEOFF, FLIGHT CREW REPORTED ODD MUSTY ODOR, AFTER ENGINE SHUTDOWN INFLIGHT CREW REPORTED SAME ODOR. MX EVALUATED CREW REPORTING SHEET AND ODOR DECISION TABLE IAW TSM 0550009910010000A. MX REMOVED AND REPLACED RECIRC FILTER IAW AMM 212141 AND
- [SDR VQI2015F00007](https://openairdocs.org/sdr/VQI2015F00007.md): Fan · failed · Feb 28, 2015 · N835VA · Airbus A320214 · Air Distribution Fan
  > FLIGHT EXPERIENCED AN ELECTRICAL BURNING ODOR IN THE CABIN AND FLIGHT DECK, REPORTED BY FLIGHT CREW. UPON ARRIVAL, MAINTENANCE ACCOMPLISHED TSM 24-00-00-810-823-A & 21-26-00-810-809. THE EQUIPMENT COOLOING SYS EXTRACT FAN WAS FOUND FAILED AND SUBSEQUENTLY DE
- [SDR VQIA2014090500023](https://openairdocs.org/sdr/VQIA2014090500023.md): Air Data Module · faulted · Aug 26, 2014 · N835VA · Airbus A320214 · Air Data Computer
  > THE FLIGHT CREW REPORTED AN ADR 1 NAV FAULT DISPLAYED ON ECAM WITH ASSOCIATED FAULT LIGHT AND LOSS OF CAPT AIRSPEED AND ALTITUDE. THE CREW ACCOMPLISHED FCOM PROCEDURES AND CONTINUED TO DESTINATION WITHOUT FURTHER INCIDENT. OUR CONTRACT MAINTENANCE PARTNER ME
- [SDR VQI2011F00022](https://openairdocs.org/sdr/VQI2011F00022.md): Unknown · odor · Aug 31, 2011 · N835VA · Airbus A320214 · Air Distribution System
  > ACFT MADE A NORMAL DEPARTURE AT 2313Z. AT APPROX 1 HR INTO FLIGHT, THE IN-FLIGHT TEAM NOTIFIED THE FLIGHT DECK OF A HOT ELECTRICAL ODOR IN THE VICINITY OF ROWS 19-21. NO SMOKE WAS NOTED. THE CREW CONTACTED THE DISPATCHER AND MX VIA AIRCELL. CHECKLIST ITEMS

## 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 = 'N835VA' AND deregistration_id = 'N835VA-2023-03-15'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N835VA-2023-03-15/reports

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