# Service difficulty reports: N524VA

A list on [N524VA](https://openairdocs.org/aircraft/N524VA.md).

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

- [SDR ASAA2019071230068](https://openairdocs.org/sdr/ASAA2019071230068.md): Controller · failed · Jul 12, 2019 · N524VA · Airbus A319112 · Cabin Pressure Controller
  > SYSTEM 1 AND SYSTEM 2 PRESSURE CONTROLLER FAIL. GROUNDED - YES. FOUND CPC 1 INOP. CPC 2 RESET ACCOMPLISHED OK. REPLACED CPC 1 PER AMM 21-31-34. PERFORMED OPERATIONAL TEST PER AMM 21-31-00-710-002. TEST OK. BOTH CPC 1 & 2 TEST OK.
- [SDR ASAA2019062329921](https://openairdocs.org/sdr/ASAA2019062329921.md): Fitting · corroded · Jun 23, 2019 · N524VA · Airbus A319112 · Emergency Equipment
  > R1 DOOR AFT GIRT FITTING CORRODED AT 2EA HOLES. GROUNDED - YES. REPAIRED AREA AT HOLE LOCATIONS IAW SRM 53-11-14. THIS REPAIR IS CATEGORY B TO BE REINSPECTED AT 60,000 FC DOT REMOVED PER ENGENEERING: SRI 5311.000059 HAS BEEN GENERATED FOR STAGE 3 APPROVAL ORI
- [SDR ASAA2019060529925](https://openairdocs.org/sdr/ASAA2019060529925.md): Skin · corroded · Jun 5, 2019 · N524VA · Airbus A319112 · Wing, Plate/Skin
  > AREA 3 BETWEEN RIBS 18 AND 19 RT WING UPPER SKIN APPROXIMATELY 13% MATERIAL LOSS FOUND USING PHASE ARRAY INSPECTION. MARKED. LOCATIN 3 SHOWN ON NDT REPORTING FORM ATTACHED TO ROUTINE CARD GROUNDED - YES. REPAIRED AREA BETWEEN RIBS 18 AND 19 RT WING UPPER SKIN
- [SDR ASAA2019060529924](https://openairdocs.org/sdr/ASAA2019060529924.md): Skin Panel · corroded · Jun 5, 2019 · N524VA · Airbus A319112 · Wing, Plate/Skin
  > AREA 1 BETWEEN RIBS 20 AND 19 LT WING, UPPER SKIN APPROXIMATELY 15% MATERIAL LOSS FOUND USING PHASE ARRAY INSPECTION, MARKED. LOCATION 1 SHOWN ON MIAMI NDT REPORTING FORM ATTACHED TO ROUTINE CARD. GROUNDED - YES. ACCOMPLISHED REPAIR TO LEFT WING UPPER SKIN T/E
- [SDR ASAA2019052529850](https://openairdocs.org/sdr/ASAA2019052529850.md): Shear Plate · corroded · May 25, 2019 · N524VA · Airbus A319112 · Fuselage Miscellaneous Structure
  > AFT MAIN CABIN LATERAL SHEAR PLATE BETWEEN FRAMES 69 & 70 APPROX: RBL 48 IS CORRODED (FLOOR LEVEL) GROUNDED - YES. REMOVED AND REPLACED LATERAL SHEAR PLATE IAW SRM 51-42-11 & DWG # D53471120. DOT REMOVED (ORIG THK.071, REMAINING 0. CORRODED 100% THRU. 2 " L
- [SDR ASAA2019052329922](https://openairdocs.org/sdr/ASAA2019052329922.md): Support Beam · corroded · May 23, 2019 · N524VA · Airbus A319112 · Fuselage Miscellaneous Structure
  > L1 DOOR AFT GIRTBAR FITTING SUPORT BEAM CORRODED AT OB ATTACH HOLES GROUNDED - YES. REPAIRED BEAM AT ATTACH HOLES AIW SRM 53-11-14. THIS REPAIR IS CATEGORY B. REPAIR TO BE INSPECTED AT 60,000 FC. REPAIR ASSIGNED SRI EC/TC SRI.5311.000058 FOR FOLLOW UP INSPECTI
- [SDR ASAA2019061739696](https://openairdocs.org/sdr/ASAA2019061739696.md): Door Frame · corroded · May 23, 2019 · N524VA · Airbus A319112 · Fuselage Main, Structure
  > L2 DOOR CUTOUT, LOWER FWD, UNDER THE FWD GIRT BAR, HAS CORROSION AROUND 2 THRESHOLD ATTACH HOLES (CIRCLED IN RED) GROUNDED - YES. REMOVED CORROSION AND FOUND WITHIN LIMITS IAW A319 SRM 53-41-14. ORIG.098, REMOVED.013, REMAINING.085. ALODINED AND PRIMED IA
- [SDR ASAA2019052229884](https://openairdocs.org/sdr/ASAA2019052229884.md): Shear Plate · corroded · May 22, 2019 · N524VA · Airbus A319112 · Fuselage Miscellaneous Structure
  > AFT MAIN CABIN LATERAL SHEAR PLATE BETWEEN FRAMES 69 & 70 APPROX. LBL 48 IS CORRODED ( FLOOR LEVEL) GROUNDED - YES. SHEAR PLATE WAS CORRODED 100% THRU (ORIG THK.071 REM. 0) REMOVED DAMAGED SHEAR PLATE, INSTALLED NEW LATERAL SHEAR PLATE PER DWG D53474180002 &
- [SDR ASAA2019052429787](https://openairdocs.org/sdr/ASAA2019052429787.md): Floor Support · corroded · May 22, 2019 · N524VA · Airbus A319112 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT STRUCTURE AT FRAME 16 APPROX. RBL 10 IS CORRODED GROUNDED - YES. EVALUATED CORROSION IAW A319 SRM 53-11-14. DAMAGE DEPTH IS 0.037", LENGTH 3.06", WIDTH IS 1.17", FOUND TO BE OUT OF LIMITS. REPAIRED CORRODED FLOOR BEAM SECTION IAW A319
- [SDR ASAA2019062029753](https://openairdocs.org/sdr/ASAA2019062029753.md): Floor Support · corroded · May 22, 2019 · N524VA · Airbus A319112 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT STRUCTURE JUST AFT OF FRAME 66 APPROX RBL56 IS CORRODED GROUNDED - YES. REPAIRED STRUCTURE IAW A319 SRM 53-41-14. DOT REMOVED.THIS IS CATEGORY A REPAIR. ORIGINAL MAT. THICKNESS.098 REMOVED.030 REMAINING.068. OUT OF LIMITS IAW A319
- [SDR ASAA2019061729695](https://openairdocs.org/sdr/ASAA2019061729695.md): Floor Support · corroded · May 22, 2019 · N524VA · Airbus A319112 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT STRUCTURE JUST AFT OF FRAME 66 APPROX. RBL30 IS CORRODED GROUNDED - YES. REMOVED AND REPLACED SEAT TRACK SECTION IAW AIRBUS DWG 185D53472201, 18D53472040, 18D53472209, AND 17D534724660
- [SDR ASAA2019061729694](https://openairdocs.org/sdr/ASAA2019061729694.md): Floor Support · corroded · May 22, 2019 · N524VA · Airbus A319112 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT STRUCTURE AT FRAME 16 APPROX. RBL50 IS CORRODED GROUNDED - YES. REMOVED CORROSION AND EVALUATED IAW A319 SRM 53-11-14. DAMAGE DIMENSIONS: 1.63" LENGTH, 0.5" WIDTH, 0.046" DEPTH, FOUND OUT OF LIMITS. REMOVED AND REPLACED FLOOR BEAM FROM
- [SDR ASAA2019061729693](https://openairdocs.org/sdr/ASAA2019061729693.md): Floor Support · corroded · May 22, 2019 · N524VA · Airbus A319112 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT AT FRAME 16 APPROX. RBL30 IS CORRODED GROUNDED - YES. REMOVED CORROSION AND EVALUATED IAW SRM 53-11-14. DAMAGE FOUND OUT OF LIMITS REMOVED AND REPLACED FLOOR SUPPORT FROM FRAME 12 TO FRAME 24 IAW A319 SRM 51-42-11 AND DWG D53110920, R
- [SDR ASAA2019061029618](https://openairdocs.org/sdr/ASAA2019061029618.md): Floor Support · corroded · May 22, 2019 · N524VA · Airbus A319112 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT STRUCTURE AT FRAME 16 APPROX. RBL 52 IS CORRODED GROUNDED - YES. EVALUATE CORROSION ON PLATE ASSY IAW A319-111 SRM 53-11-14 AREA FOUND TO BE OUT OF LIMITS. ORIGINAL MATERIAL.55", MATERIAL REMOVED.011, MATERIAL REMAINING.044" REMOVE
- [SDR ASAA2019052229617](https://openairdocs.org/sdr/ASAA2019052229617.md): Floor Support · corroded · May 22, 2019 · N524VA · Airbus A319112 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT STRUCTURE JUST FWD OF FRAME 68 APPROX. RBL52 IS CORRODED GROUNDED - YES. REPAIRED FLOOR SUPPORT IAW A319 SRM 53-41-14
- [SDR ASAA2019061029616](https://openairdocs.org/sdr/ASAA2019061029616.md): Floorbeam · corroded · May 22, 2019 · N524VA · Airbus A319112 · Fuselage Main, Floor Beam
  > AFT MAIN CAIN FLOOR SUPPORT STRUCTURE AT FRAME 68 APPROX. LBL 48 IS CORRODED GROUNDED - YES. REPAIRED SUPPORT STRUCTURE IAW A319 SRM53-41-14. REMOVED AND REINSTALLED WEB IAW A319 SRM 51-42-11 & DWG # D53480019
- [SDR ASAA2019021428184](https://openairdocs.org/sdr/ASAA2019021428184.md): Comparator · failed · Feb 14, 2019 · N524VA · Airbus A319112 · Pneumatic Indicating System
  > ENGINE 2 BLEED FAULT - PACK 2 TEMP HIGH, GROUNDED - YES. R&R BMC NR 2 REF LP 1213095 ITEM 1. PERFORMED OPERATIONAL TEST OF THE BLEED AIR SYS REF AMM 36-11-00-710-003-A. OPS TEST CHECK NORMAL. NO FAULTS NOTED.
- [SDR VQIA2017081000047](https://openairdocs.org/sdr/VQIA2017081000047.md): Power Supply · malfunctioned · Oct 27, 2016 · N524VA · Airbus A319112 · Flight Control System
  > DIVERTED DUE TO A FLT CONTROL SEC 3 FAULT. RESET SEC 3 POWER SUPPLY CIRCUIT BREAKER IAW TSM 24-00-00-81-08-18. ACFT OK FOR SERVICE. NO RECENT HISTORY OF SEC 3 PROBLEMS HAS BEEN NOTED ON THIS ACFT.
- [SDR VQI2014F00012](https://openairdocs.org/sdr/VQI2014F00012.md): Hmu · malfunctioned · Dec 17, 2013 · N524VA · Airbus A319112 · Fuel Controlling System
  > DURING CRUISE, CREW RECEIVED NR 1 ENGINE, NR 2 ENGINE OVER LIMIT ECAM EMESSAGE WITH ASSOCIATED FUEL CONTROL FAULT AND HMU, FMV, ENGINE 1A, 1B, CREW FOLLOWED SHUTDOWN PROCEDURE FOR NR 1 ENGINE AND SENT ACARS MESSAGE TO DISPATCH WITH MSG " ENGINE 1 PRECAUTION SH
- [SDR VQI2014F00000](https://openairdocs.org/sdr/VQI2014F00000.md): Engine · malfunctioned · Dec 17, 2013 · N524VA · Airbus A319112 · Engine (Turbine/Turboprop)
  > DURING CRUISE, RECEIVED NR 1 ENGINE N2 ENGINE OVER LIMIT ECAM MESSAGE WITH ASSOCIATED FUEL CTL FAULT AND HMU, FMV, ENGINE 1A, 1B. SHUTDOWN NR 1 ENGINE, DIVERTED. ACFT LANDED WITHOUT DECLARING AN EMERGENCY. FADEC TEST AND N2 MAX VALUE WAS RECORDED AT 106.7
- [SDR 2013FA0000393](https://openairdocs.org/sdr/2013FA0000393.md): Floor Support · corroded · Jun 8, 2013 · N524VA · Airbus A319112 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT FR66-68, Y765 HAS CORROSION BEYOND LIMITS. FLOOR SUPPORT FR66-70 R & R IAW SRM 51-42-11.
- [SDR 2013FA0000392](https://openairdocs.org/sdr/2013FA0000392.md): Floor Support · corroded · Jun 8, 2013 · N524VA · Airbus A319112 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT FR68, Y512.5 HAS CORROSION BEYOND SRM LIMITS. FLOOR SUPPORT FR 67-70 AT Y512.5 R & R IAW SRM 51-42-11.
- [SDR 2013FA0000391](https://openairdocs.org/sdr/2013FA0000391.md): Floor Support · corroded · Jun 8, 2013 · N524VA · Airbus A319112 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT FR68, Y1162 HAS CORROSION BEYOND SRM LIMITS. FLOOR SUPPORT FR68-69 WAS R & R IAW SRM 51-42-11.
- [SDR 2013FA0000390](https://openairdocs.org/sdr/2013FA0000390.md): Floor Support · corroded · Jun 8, 2013 · N524VA · Airbus A319112 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT FR16, Y1292 HAS CORROSION BEYOND SRM LIMITS. FLOOR SUPPORT R & R IAW SRM 51-42-11.
- [SDR 2013FA0000389](https://openairdocs.org/sdr/2013FA0000389.md): Shear Plate · corroded · Jun 8, 2013 · N524VA · Airbus A319112 · Fuselage Miscellaneous Structure
  > LEFT LATERAL SHEAR PLATE BETWEEN S23-24L, FR 69-70 HAS CORROSION BEYOND SRM LIMITS. LT SHEAR PLATE WAS R & R IAW SRM 51-42-11.
- [SDR VQI2013F00020](https://openairdocs.org/sdr/VQI2013F00020.md): Support · corroded · Jun 8, 2013 · N524VA · Airbus A319112 · Fuselage Miscellaneous Structure
  > LEFT LATERAL SHEAR PLATE SUPPORT BETWEEN ST23L-ST24L, FR69-FR70 HAS CORROSION BEYOND SRM LIMITS. EXTENT OF DAMAGE: 2"L X 2" W, X.020 D. LT SHEAR PLATE SUPPORT WAS R & R IAW SRM 51-42-11.
- [SDR 2013FA0000387](https://openairdocs.org/sdr/2013FA0000387.md): Beam · corroded · Jun 8, 2013 · N524VA · Airbus A319112 · Fuselage Main, Structure
  > RIGHT AFT DOOR SILL BEAM HAS TWO AREAS OF CORROSION BETWEEN FR66-FR68, ST23R-ST24R AT Y1725. REPAIRED IAW SRM 53-41-14, FIG 201, SHEET 3, (K) REPAIR.
- [SDR 2013FA0000386](https://openairdocs.org/sdr/2013FA0000386.md): Floor Support · corroded · Jun 8, 2013 · N524VA · Airbus A319112 · Fuselage Miscellaneous Structure
  > CABIN FLOOR SUPPORT AT FR68, Y65 HAS CORROSION BEYOND SRM LIMITS. FLOOR SUPPORT R & R IAW SRM 51-42-11.
- [SDR 2013FA0000385](https://openairdocs.org/sdr/2013FA0000385.md): Floorbeam · corroded · Jun 8, 2013 · N524VA · Airbus A319112 · Fuselage Main, Floor Beam
  > CABIN FLOORBEAM AT FR66, Y765 HAS CORROSION BEYOND SRM LIMITS. FLOORBEAM WAS FABRICATED IAW DWG D6347220. INSTALLED IAW SRM 51-42-11.
- [SDR VQI2011F00012](https://openairdocs.org/sdr/VQI2011F00012.md): Gust Lock · malfunctioned · Jul 2, 2011 · N524VA · Airbus A319112 · Service Doors
  > DURING GROUND SERVICING OF THE ACFT ON A TURN, THE CATERING CREW NOTED THAT THE R1 DOOR GUST LOCK (DOOR STAY) MECHANISM DID NOT ENGAGE AND AND NOTIFIED THE CAPT. THE CAPT NOTIFIED OPS OF THE ISSUE, WHO IN TURN, CALLED OUT MX. THE TECHS CARRIED OUT A NORMAL O
- [SDR VQI2011F00006](https://openairdocs.org/sdr/VQI2011F00006.md): Bushing · out of alignment · Apr 22, 2011 · N524VA · Airbus A319112 · Passenger/Crew Doors
  > DURING GROUND SERVICING OF THE ACFT THE CATERING CREW NOTED THAT THE R1 DOOR GUST LOCK (DOOR STAY) MECHANISM WAS NOT ENGAGING AND NOTIFIED THE CAPTAIN. THE CAPT NOTIFIED MX CONTROL ABOUT THE ISSUE AT 1930Z. MX WAS CALLED. UPON INSP, FOUND THE GUST LOCK RELE

## 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 = 'N524VA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N524VA/reports

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