# Service difficulty reports: N527VA

A list on [N527VA](https://openairdocs.org/aircraft/N527VA.md).

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

- [SDR ASAA2023060643586](https://openairdocs.org/sdr/ASAA2023060643586.md): Light · inoperative · Jun 6, 2023 · N527VA · Airbus A319112 · Emergency Lighting
  > SEAT ROW 21 ABC EMERGENCY LIGHT ON OUTBOARD SEAT INOP. GROUNDED - YES. REMOVED AND REPLACED EMERGENCY LIGHT AT SEAT ROW 21 ABC IAW AMM 33-51-19-400-003-A AND AMM 33-51-19-000-003-A AND PERFORMED GOOD OPERATIONAL TEST IAW AMM 33-51-00-710-001-A.
- [SDR ASAA2020032332487](https://openairdocs.org/sdr/ASAA2020032332487.md): Seat Track · corroded · Feb 25, 2020 · N527VA · Airbus A319112 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN, FR18 Y-1292, FLOOR BEAM CORRODED GROUNDED - YES. SEAT TRACK HAS AREAS OF CORROSION WITH 100% LOSS. REMOVED AND REPLACED SEAT TRACK P/N D5311278220201 IAW A319 SRM 51-42-11
- [SDR ASAA2020033132575](https://openairdocs.org/sdr/ASAA2020033132575.md): Shear Plate · corroded · Feb 24, 2020 · N527VA · Airbus A319112 · Fuselage Miscellaneous Structure
  > RIGHT SIDE AFT CABIN SHEAR PLATE, AT FRAME 70 AND AFT OF LONGITUDINAL FLOOR BEAM -Y1292 HAS NUMEROUS AREAS OF CORROSION. GROUNDED - YES. NO ALLOWABLE DAMAGE LIMITS FOR SHEAR PLATE IN A319 SRM. REMOVED AND REPLACED SHEAR PLATE IAW A319 SRM 51-42-11 AND A319 D
- [SDR ASAA2020022532533](https://openairdocs.org/sdr/ASAA2020022532533.md): Door Sill · corroded · Feb 24, 2020 · N527VA · Airbus A319112 · Fuselage Miscellaneous Structure
  > RIGHT AFT CABIN "R2" DOOR, DOUBLER PLATE ADJACENT TO AND UNDER THE FORWARD GIRT BAR FITTING HAS CORROSION. **AREA MARKED IN RED** GROUNDED - YES. REMOVED CORROSION-ORIGINAL THICKNESS.256 REMAINING.090, REMOVED.166 AND FOUND TO BE OUT OF LIMITS IAW A319
- [SDR ASAA2020022532532](https://openairdocs.org/sdr/ASAA2020022532532.md): Floor Support · corroded · Feb 24, 2020 · N527VA · Airbus A319112 · Fuselage Miscellaneous Structure
  > RIGHT CENTER AFT CABIN LONGITUDINAL FLOOR BEAM Y254 JUST AFT OF FRAME 70 HAS CORROSION. **AREA MARKED IN RED** GROUNDED - YES. NO ALLOWABLE LIMITS GIVEN IN A319 SRM FOR FLOOR BEAM HARD POINT. REMOVED AND REPLACED FLOOR BEAM P/N D534219720200 IAW A319 SRM
- [SDR ASAA2020022532531](https://openairdocs.org/sdr/ASAA2020022532531.md): Floor Support · corroded · Feb 24, 2020 · N527VA · Airbus A319112 · Fuselage Miscellaneous Structure
  > RIGHT SIDE AFT CABIN LONGITUDINAL FLOOR BEAM -Y765, AT FRAME 68 HAS CORROSION. **AREA MARKED IN RED** GROUNDED - YES. NO ALLOWABLE LIMITS GIVEN IN A319 SRM FOR FLOOR BEAM HARD POINT. REMOVED AND REPLACED FLOOR BEAM P/N D5347219320200 IAW A319 SRM 51-42-11
- [SDR ASAA2020022532529](https://openairdocs.org/sdr/ASAA2020022532529.md): Support Fitting · corroded · Feb 24, 2020 · N527VA · Airbus A319112 · Fuselage Main, Frame
  > LEFT SIDE AFT MAIN CABIN FRAME SUPPORT FITTING AT FRAME 70 AND ADJACENT TO THE LEFT LATERAL SHEAR PLATE HAS CORROSION ON UPPER SECTION. **AREA MARKED IN RED** GROUNDED - YES. NO ALLOWABLE DAMAGE LIMITS GIVEN FOR FRAME SUPORT IN A319 SRM. REMOVED AND
- [SDR ASAA2020022532528](https://openairdocs.org/sdr/ASAA2020022532528.md): Shear Plate · corroded · Feb 24, 2020 · N527VA · Airbus A319112 · Fuselage Miscellaneous Structure
  > LEFT SIDE AFT MAIN CABIN LATERAL SHEAR PLATE IS CRACKED ON INBOARD EDGE BETWEEN FRAMES 68 & 69, OUTBOARD OF LONGITUDINAL BEAM Y1292, AND JUST AFT OF THE "L2" DOOR. **CRACKED GROUNDED - YES. NO ALLOWABLE LIMITS GIVEN FOR SHEAR PLATE IN A319 SRM. REMOVED AND
- [SDR ASAA2020022432527](https://openairdocs.org/sdr/ASAA2020022432527.md): Shear Plate · corroded · Feb 24, 2020 · N527VA · Airbus A319112 · Fuselage Miscellaneous Structure
  > LEFT SIDE AFT MAIN CABIN LATERAL SHEAR PLATE HAS CORROSION AT FRAME 70 AND AT TRAILING END OF LONGITUDINAL FLOOR BEAM Y1162. **AREAS MARKED IN RED** GROUNDED - YES. NO ALLOWABLE DAMAGE LIMITS FOR SHEAR PLATE IN A319 SRM. REMOVED AND REPLACED SHEAR PLATE
- [SDR ASAA2020032332486](https://openairdocs.org/sdr/ASAA2020032332486.md): Floor Support · corroded · Feb 24, 2020 · N527VA · Airbus A319112 · Fuselage Miscellaneous Structure
  > RIGHT AFT CABIN LONGITUDINAL FLOOR BEAM -Y1292, JUST FORWARD OF FRAME 68 AND ADJACENT TO THE "R2" DOOR AFT GIRT BAR FITTING HAS CORROSION. **AREA MARKED IN RED** GROUNDED - YES. NO ALLOWABLE DAMAGE LIMITS GIVEN IN A319 SRM FOR "HARDPOINT LOCATION". REMOVED AND
- [SDR ASAA2020032332485](https://openairdocs.org/sdr/ASAA2020032332485.md): Shear Plate · corroded · Feb 24, 2020 · N527VA · Airbus A319112 · Fuselage Miscellaneous Structure
  > RIGHT SIDE AFT CABIN SHEAR PLATE JUST AFT OF FRAME 68 AND OUTBOARD OF LONGITUDINAL FLOOR BEAM -Y1292 HAS CORROSION. **AREA MARKED IN RED** GROUNDED - YES. NO ALLOWABLE DAMAGE LIMITS GIVEN FOR SHEAR PLATE IN A319 SRM. REMOVED AND REPLACED SHEAR PLATE P/N D53480
- [SDR ASAA2020031932467](https://openairdocs.org/sdr/ASAA2020031932467.md): Floor Support · corroded · Feb 24, 2020 · N527VA · Airbus A319112 · Fuselage Miscellaneous Structure
  > LEFT SIDE LONGDITUDINAL FLOOR BEAM Y1732, COUPLING -Y1450 HAS CORROSION JUST FORWARD OF FRAME 66 AND ADJACENT TO THE FORWARD GIRT BAR FITTING. **AREA MARKED IN RED** GROUNDED - YES. REMOVED CORROSION - ORIGINAL THICKNESS. 150,. REMAINING.109, REMOVED
- [SDR ASAA2018052024715](https://openairdocs.org/sdr/ASAA2018052024715.md): Apu · overserviced · May 20, 2018 · N527VA · Airbus A319112 · APU Oil System
  > STRONG ODOR RETURNED ON DESCENT. SMELLED LIKE OIL DROPPING ON SOMETHING HOT. MOST NOTICEABLE IN CENTER CABIN. ACFT GROUNDED. TROUBLESHOT AND FOUND A APU BLEED FAULT IAW TSM 25-00-00-810-823. RAN ENGINES AND APU BLEED OFF WITH NO OCCURENCE OF ODORS. FOUND
- [SDR VQIA2016120300001](https://openairdocs.org/sdr/VQIA2016120300001.md): Windshield · cracked · Dec 3, 2016 · N527VA · Airbus A319112 · Flight Compartment Windows
  > CAPTAIN`S WINDSHIELD CRACKED DURING FLIGHT, RETURNED TO DEPARTURE. REMOVED AND REPLACED THE WINDSHIELD IAW AMM 56-11-11. OPS TEST THE ANTI-ICE DEFOGGING SYSTEM IAW 30-42-00, TESTED GOOD.
- [SDR VQIA2017081000043](https://openairdocs.org/sdr/VQIA2017081000043.md): Acm · failed · Sep 22, 2016 · N527VA · Airbus A319112 · Cabin Cooling System
  > BROWN SMOKE AND BURNING ODOR FROM COCKPIT AIR VENTS, TEMP IN CABIN INCREASED TO 110 DEGREES. ACCOMPLISHED TSM`S 055000810831A AND 240000810823. DEBRIEFED FLT CREW. COCKPIT TEMP REACH 135 DEGREES. ON ARRIVAL THE NR 1 PACK OVERHEAT. TROUBLESHOT AND REPEATE
- [SDR VQI2015F00036](https://openairdocs.org/sdr/VQI2015F00036.md): Packing · failed · Nov 19, 2015 · N527VA · Airbus A319112 · Hydraulic System, Main
  > ACFT EXPERIENCED LOSS OF YELLOW HYDRAULIC SYS PRESSURE AND FLUID QUANTITY. THE FLIGHT CREW SECURED THE YELLOW HYDRAULIC SYS AND CONTINUED TO DESTINATION. UPON LANDING THE CREW EXPERIENCED SIGNIFICANT MLG VIBRATION AT TOUCH BEFORE THE APPLICATION OF BRAKES.
- [SDR VQIA2015072400027](https://openairdocs.org/sdr/VQIA2015072400027.md): Unknown · odor · Jul 15, 2015 · N527VA · Airbus A319112 · Air Distribution System
  > AIRCRAFT ARRIVED AT DESTINATION, STRONG BURNING ODOR, REAR OF ACFT ON DESCENT. PERFORMED TSM 05-50-00-810-831-A, NO ODOR NOTED AT THIS TIME.
- [SDR XE4R2014030700143](https://openairdocs.org/sdr/XE4R2014030700143.md): Shear Plate · corroded · Feb 6, 2014 · N527VA · Airbus A319112 · Fuselage Miscellaneous Structure
  > AFT CABIN, LT SHEAR PLATE CORRODED BEYOND LIMITS. REPLACED SHEAR PLATE FRAME 70 LT.
- [SDR XE4R2014030700142](https://openairdocs.org/sdr/XE4R2014030700142.md): Floor Support · corroded · Feb 6, 2014 · N527VA · Airbus A319112 · Fuselage Miscellaneous Structure
  > CABIN FLOOR SUPPORT CORRODED AT FRAMES 66-68, Y-160.5 FOUND BEYOND LIMITS. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.
- [SDR XE4R2014030700141](https://openairdocs.org/sdr/XE4R2014030700141.md): Floor Support · corroded · Feb 6, 2014 · N527VA · Airbus A319112 · Fuselage Miscellaneous Structure
  > CABIN FLOOR SUPPORT CORRODED AT FRAMES 68-69, Y-1162.5, OUT OF LIMITS. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.
- [SDR XE4R2014030700140](https://openairdocs.org/sdr/XE4R2014030700140.md): Shear Plate · corroded · Feb 6, 2014 · N527VA · Airbus A319112 · Fuselage Miscellaneous Structure
  > AFT CABIN RT SHEAR PLATE CORROSION BEYOND LIMITS. REPLACED RT SHEAR PLATE, FRAMES 69-70 RT.
- [SDR XE4R2014030700139](https://openairdocs.org/sdr/XE4R2014030700139.md): Floor Support · corroded · Feb 6, 2014 · N527VA · Airbus A319112 · Fuselage Miscellaneous Structure
  > CABIN FLOOR SUPPORT CORRODED AT FRAMES 66-68, Y-160.5 FOUND OUT OF LIMITS. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.
- [SDR XE4R2014030700138](https://openairdocs.org/sdr/XE4R2014030700138.md): Floor Support · corroded · Feb 6, 2014 · N527VA · Airbus A319112 · Fuselage Miscellaneous Structure
  > CABIN FLOOR SUPPORT CORRODED AT FRAMES 64-66. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.
- [SDR VQI2011F00019](https://openairdocs.org/sdr/VQI2011F00019.md): Bushing · failed · Aug 31, 2011 · N527VA · Airbus A319112 · Passenger/Crew Doors
  > ACFT ARRIVED, WHEN OPENING THE L1 MAIN ENTRY DOOR, THE GUEST SERVICE AGENT NOTED THE LOCK STAY (GUST LOCK) WOULD NOT ENGAGE WITH THE DOOR COMPLETELY OPEN. MX WAS CALLED TO THE ACFT TO INVESTIGATE AND WAS PROVIDED THE TSM AND AMM REFERENCES TO START TROUBLESHO
- [SDR VQI2011F00018](https://openairdocs.org/sdr/VQI2011F00018.md): Gust Lock · malfunctioned · Aug 31, 2011 · N527VA · Airbus A319112 · Passenger/Crew Doors
  > ACFT ARRIVED, WHEN OPENING THE L1 MAIN ENTRY DOOR, THE GUEST SERVICE AGENT NOTED THE LOCK STAY (GUST LOCK) WOULD NOT ENGAGE WITH THE DOOR COMPLETELY OPEN. MX WAS CALLED TO THE ACFT TO INVESTIGATE AND WAS PROVIDED THE TSM AND AMM REFERENCES TO START TROUBLESHO
- [SDR VQI2011F00015](https://openairdocs.org/sdr/VQI2011F00015.md): Insulation · out of position · Aug 8, 2011 · N527VA · Airbus A319112 · Passenger/Crew Doors
  > ARRIVED AT DESTINATION, WHEN OPENING THE L1 MAIN ENTRY DOOR, IT WAS NOTED THE LOCK STAY (GUST LOCK) WOULD NOT ENGAGE WITH THE DOOR COMPLETELY OPEN. MX CALLED AND WAS PROVIDED WITH THE TSM AND AMM REFERENCES TO START TROUBLESHOOTING. UPON GAINING ACCESS TOT H
- [SDR VQIA2011F00000](https://openairdocs.org/sdr/VQIA2011F00000.md): Lock · lack of lube · Jul 9, 2011 · N527VA · Airbus A319112 · Passenger/Crew Doors
  > L1 DOOR WIL NOT LOCK IN OPEN POSITION. LUBRICATED DOOR UNLOCKING MECHANISM IAW AMM 52-11-12-000-001.
- [SDR VQI2011F00011](https://openairdocs.org/sdr/VQI2011F00011.md): Mechanism · lack of lube · Jun 20, 2011 · N527VA · Airbus A319112 · Passenger/Crew Doors
  > ACFT ARRIVED AT DESTINATION, WHEN OPENING THE L1 MAIN ENTRY DOOR, THE GUEST SERVICE AGENT NOTED THE LOCK STAY (GUST LOCK) WOULD NOT ENGAGE WITH THE DOOR COMLETELY OPEN. IT WAS TOLD TO THE CAPT, WHO NOTIFIED MX CONTROL, MX WAS CALLED TO THE AIRCRAFT TO INVESTI
- [SDR VQI2008F00001](https://openairdocs.org/sdr/VQI2008F00001.md): Wire Harness · damaged · May 14, 2008 · N527VA · Airbus A319111 · Turbine Engine System Wiring
  > IN NORMAL CRUISE, THE AIRCRAFT EXPERIENCED AN UNCOMMANDED SHUTDOWN OF THE NR 1 ENGINE. ECAM ENG1 FADEC A FAULT OCCURRED WITH ASSOCIATED MESSAGES. THE CREW RESTARTED THE ENGINE AFTER FOLLOWING QRH PROCEDURES. A/C DIVERTED INTO PDX WITH NO FURTHER FAULTS NOTED.

## 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 = 'N527VA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N527VA/reports

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