N527VA

Service difficulty reports · 29

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR ASAA2023060643586Light · inoperativeSEAT 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.Jun 6, 2023 · N527VA · Airbus A319112 · Emergency LightingSDR ASAA2020032332487Seat Track · corrodedMAIN 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 51-42-11Feb 25, 2020 · N527VA · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA2020033132575Shear Plate · corrodedRIGHT 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 DFeb 24, 2020 · N527VA · Airbus A319112 · Fuselage Miscellaneous StructureSDR ASAA2020022532533Door Sill · corrodedRIGHT 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 Feb 24, 2020 · N527VA · Airbus A319112 · Fuselage Miscellaneous StructureSDR ASAA2020022532532Floor Support · corrodedRIGHT 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 Feb 24, 2020 · N527VA · Airbus A319112 · Fuselage Miscellaneous StructureSDR ASAA2020022532531Floor Support · corrodedRIGHT 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 51-42-11Feb 24, 2020 · N527VA · Airbus A319112 · Fuselage Miscellaneous StructureSDR ASAA2020022532529Support Fitting · corrodedLEFT 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 ANDFeb 24, 2020 · N527VA · Airbus A319112 · Fuselage Main, FrameSDR ASAA2020022532528Shear Plate · corrodedLEFT 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 Feb 24, 2020 · N527VA · Airbus A319112 · Fuselage Miscellaneous StructureSDR ASAA2020022432527Shear Plate · corrodedLEFT 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 PLATEFeb 24, 2020 · N527VA · Airbus A319112 · Fuselage Miscellaneous StructureSDR ASAA2020032332486Floor Support · corrodedRIGHT 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 ANDFeb 24, 2020 · N527VA · Airbus A319112 · Fuselage Miscellaneous StructureSDR ASAA2020032332485Shear Plate · corrodedRIGHT 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 D53480Feb 24, 2020 · N527VA · Airbus A319112 · Fuselage Miscellaneous StructureSDR ASAA2020031932467Floor Support · corrodedLEFT 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, REMOVEDFeb 24, 2020 · N527VA · Airbus A319112 · Fuselage Miscellaneous StructureSDR ASAA2018052024715Apu · overservicedSTRONG 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. FOUNDMay 20, 2018 · N527VA · Airbus A319112 · APU Oil SystemSDR VQIA2016120300001Windshield · crackedCAPTAIN`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.Dec 3, 2016 · N527VA · Airbus A319112 · Flight Compartment WindowsSDR VQIA2017081000043Acm · failedBROWN 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 REPEATESep 22, 2016 · N527VA · Airbus A319112 · Cabin Cooling SystemSDR VQI2015F00036Packing · failedACFT 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. Nov 19, 2015 · N527VA · Airbus A319112 · Hydraulic System, MainSDR VQIA2015072400027Unknown · odorAIRCRAFT 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.Jul 15, 2015 · N527VA · Airbus A319112 · Air Distribution SystemSDR XE4R2014030700143Shear Plate · corrodedAFT CABIN, LT SHEAR PLATE CORRODED BEYOND LIMITS. REPLACED SHEAR PLATE FRAME 70 LT.Feb 6, 2014 · N527VA · Airbus A319112 · Fuselage Miscellaneous StructureSDR XE4R2014030700142Floor Support · corrodedCABIN FLOOR SUPPORT CORRODED AT FRAMES 66-68, Y-160.5 FOUND BEYOND LIMITS. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.Feb 6, 2014 · N527VA · Airbus A319112 · Fuselage Miscellaneous StructureSDR XE4R2014030700141Floor Support · corrodedCABIN FLOOR SUPPORT CORRODED AT FRAMES 68-69, Y-1162.5, OUT OF LIMITS. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.Feb 6, 2014 · N527VA · Airbus A319112 · Fuselage Miscellaneous StructureSDR XE4R2014030700140Shear Plate · corrodedAFT CABIN RT SHEAR PLATE CORROSION BEYOND LIMITS. REPLACED RT SHEAR PLATE, FRAMES 69-70 RT.Feb 6, 2014 · N527VA · Airbus A319112 · Fuselage Miscellaneous StructureSDR XE4R2014030700139Floor Support · corrodedCABIN FLOOR SUPPORT CORRODED AT FRAMES 66-68, Y-160.5 FOUND OUT OF LIMITS. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.Feb 6, 2014 · N527VA · Airbus A319112 · Fuselage Miscellaneous StructureSDR XE4R2014030700138Floor Support · corrodedCABIN FLOOR SUPPORT CORRODED AT FRAMES 64-66. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.Feb 6, 2014 · N527VA · Airbus A319112 · Fuselage Miscellaneous StructureSDR VQI2011F00019Bushing · failedACFT 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 TROUBLESHOAug 31, 2011 · N527VA · Airbus A319112 · Passenger/Crew DoorsSDR VQI2011F00018Gust Lock · malfunctionedACFT 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 TROUBLESHOAug 31, 2011 · N527VA · Airbus A319112 · Passenger/Crew DoorsSDR VQI2011F00015Insulation · out of positionARRIVED 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 HAug 8, 2011 · N527VA · Airbus A319112 · Passenger/Crew DoorsSDR VQIA2011F00000Lock · lack of lubeL1 DOOR WIL NOT LOCK IN OPEN POSITION. LUBRICATED DOOR UNLOCKING MECHANISM IAW AMM 52-11-12-000-001.Jul 9, 2011 · N527VA · Airbus A319112 · Passenger/Crew DoorsSDR VQI2011F00011Mechanism · lack of lubeACFT 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 INVESTIJun 20, 2011 · N527VA · Airbus A319112 · Passenger/Crew DoorsSDR VQI2008F00001Wire Harness · damagedIN 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.May 14, 2008 · N527VA · Airbus A319111 · Turbine Engine System Wiring
Back to N527VA