N622VA

Service difficulty reports not matched to an aircraft · 19

They name N622VA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N622VA' AND registry_match IS NULL
  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 ASAA2020112533619Floorboard · delaminatedMAIN CABIN FLOOR PANEL 242KF DELAMINATED AROUND MOUNT POINT. GROUNDED-YES. FABRICATED NEW MAIN CABIN FLOOR PANEL 242KF, IAW A320 SRM 53-02-283-001 & MCG IRM 9701 REV 1.Nov 25, 2020 · N622VA · Airbus A320214 · Fuselage Floor PanelSDR ASAA2020110533528Skin · dentedDENT OBSERVED FORWARD OF THE POTABLE WATER SERVICE DOOR. GROUNDED-YES. REPAIRED DENTED AREA WITH DOUBLER BETWEEN FR 64 AND FR 65 AND STR 36L AND STR 39L, REF A320 SRM 53-41-11-300-016 CLASS A REPAIR. LIMITED CUTOUT REPAIR. THIS CLEARS MDDR 73300, CONTACTEDNov 5, 2020 · N622VA · Airbus A320214 · Fuselage Main, Plate/SkinSDR ASAA2020110133529Skin · dentedLT INBOARD FLAP DENTED 24 INCHES FROM INBOARD AND .5 INCHES FROM TRAILING EDGE. GROUNDED-YES. REPAIRED DENT ON LT INBOARD FLAP UPPER SURFACE 24 IN FROM INBOARRD EDGE AND 0.5 IN FROM TRAILING EDGE, IAW ASA A320 SRM 57-52-00-300-091. FINISH RESTORED, IAW A320Nov 1, 2020 · N622VA · Airbus A320214 · Wing, Plate/SkinSDR ASAA2019081430533Support Web · corrodedAFT CABIN RT UNDER LAV LATERAL SHEAR PLATE, SUPPORT WEB CORRODED GROUNDED - YES. REMOVED AND REPLACED SUPPORT WEB IAW SRM 51-42-11 AND DWG D53474180. NOTE: NO ALLOWABLE LIMITS FOR DISCREPANT PART FORM 337 ATTACHED. NO SRI REQUIRED.Aug 14, 2019 · N622VA · Airbus A320214 · Fuselage Miscellaneous StructureSDR ASAA2019081330542Shear Plate · corrodedAFT CABIN RT LAV, LATERAL SHEAR PLATE HAS CORROSION ON THE WEB GROUNDED - YES. REMOVED AND REINSTALLED MOTOR STARTER RELAY IAW AMM 38-31-36 & ESPM 20-33-11, OPS CK GOOD. REMOVED AND REPLACED SHEAR PLATE IAW DWG # 18D53474180 & SRM 51-42-11. REMOVED AND REINSTAug 13, 2019 · N622VA · Airbus A320214 · Fuselage Miscellaneous StructureSDR ASAA2018112427159Skin · dentedLOWER LT SKIN IS DENTED AT FR61 TO FR62 S36L GROUNDED - YES. ACCOMPLISHED REPAIR TO 2 EA DENTED AREAS BETWEEN FR61 TO FR62 STR 35L TO 37L PER SRM 53-00-11-300-029/042/043.Nov 24, 2018 · N622VA · Airbus A320214 · Fuselage Main, Plate/SkinSDR ASAA2018091826155Wire · detachedEMER ROW LIGHTS INOP AT ROWS 22 & 23. GROUNDED - YES. REATTACHED WIRES IN CONNECTOR PER AMM AWM 33-51-07 P 0249, SHT 2. OPS CHECK GOOD.Sep 13, 2018 · N622VA · Airbus A320214 · Light System WiringSDR VQI2017F00014Bushing · wornMX FOUND THE R1 DOOR GUST LOCK STICKING DUE TO WORN BUSHINGS. MX REPLACED THE BUSHINGS IAW AMM 52-11-12 AND TBN 52-10-01. OPS CHECKED GOOD.Mar 25, 2017 · N622VA · Airbus A320214 · Service DoorsSDR VQIA2016011200004Proximity Sensor · failedAIRPLANE WAS RELEASED FROM HEAVY MAINTENANCE. THE ACFT THEN TOOKOFF, AFTER TAKEOFF, THE CREW ATTEMPTED TO RETRACT THE GEARS AND RECEIVED, DOORS UNLOCKED MESSAGE ON ECAM. THE NOSE GEAR DID NOT RETRACT. THE CREW ATTEMPTED A SECOND TIME TO RETRACT THE GEARS AJan 31, 2016 · N622VA · Airbus A320214 · Landing Gear Position and WarningSDR VQI2015F00009Slide · low pressureR2 DOOR SLIDE PRESSURE GUAGE WAS FOUND IN THE RED BAND DURING PREFLIGHT CHECKS BY INFLIGHT TEAM. MAINTENANCE WAS SENT WITH SERVICEABLE SLIDE AND SLIDE WAS REPLACED IAW AMM 25-62-44 PB01 AND DOOR ASSIST BOTTLE SERVICED ACFT, TOOK A 176 MINUTE DELAY.Mar 11, 2015 · N622VA · Airbus A320214 · Escape SlideSDR VQI2014F00035Hose · leakingDURING APPROACH, REPORTED LOSS OF GREEN SYSTEM HYDRAULIC FLUID. MAINTENANCE DISCOVERED A MLG DOOR ACTUATOR HOSE ON THE LT SIDE LEAKING. R & R IAW AMM 32-31-39-401, NO LEAKS NOTED AFTERWARD, ALL OPS CHECKS NORMAL AND THE ACFT WAS PLACED BACK INTO SERVICE AT 1Nov 17, 2014 · N622VA · Airbus A320214 · Hydraulic System, MainSDR VQIA2013112200033Fan · failedPLASTIC BURNING ODOR DETECTED IN COCKPIT WITH AMBER FAN ANNUNCIATED ON THE COND PAGE. MX ACCOMPLISHED TSM 24-00-00810-823A FOR BURNING ODOR WITH NO DEFECTS FOUND. TROUBLESHOOTING REVEALED, RECIRCULATION FAN FIN 15HG TO BE FAULTED.Oct 24, 2013 · N622VA · Airbus A320214 · Air Distribution FanSDR VQI2012F00009Switch · defectiveACFT WAS ON A TURN, AFTER FLIGHT. DURING THE PREFLIGHT, THE FLIGHT CREW NOTED THAT THE EMERGENCY EXIT LIGHTS STAYED ILLUMINATED WITH THE SWITCH IN THE "ARMED" POSITION. MX WAS CALLED OUT AFTER SEVERAL RESET ATTEMPTS THROUGH MX CONTROL WERE UNSUCCESSFUL. MXApr 19, 2012 · N622VA · Airbus A320214 · Emergency LightingSDR VQI2011F00027Pin · unserviceableUPON ARRIVAL, A LOG ENTRY WAS MADE NOTING THAT THE L2 DOOR INDICATED DISARMED ON THE LOWER ECAM PAGE DURING CRUISE FLIGHT. THIS WAS AREPEAT ITEM BEING MONITORED AND COULD NOT BE DEFERRED DUE TO MEL DAYLIGHT ONLY FLYING RESTRICTIONS. THE ACFT WAS TAKEN OUT OFDec 5, 2011 · N622VA · Airbus A320214 · Passenger/Crew DoorsSDR VQI2011F00031Floor Support · corrodedREMOVED CORROSION AT CABIN FLOOR PANEL SUPPORT UPPER SURFACE BETWEEN FRAMES 68-70, RBL 6" IAW SRM 51-74-00. PERFORMED UT THICKNESS INSP OF REWORKED AREA, FOUND TO BE AT UPPER SURFACE 0.150 MAX, 0.90 MIN USED DAKOTA MX-3 SN 3B264 IAW A320 NDTM 51-10-04. R & RNov 17, 2011 · N622VA · Airbus A320214 · Fuselage Miscellaneous StructureSDR VQI2011F00030Floor Support · corrodedREMOVED CORROSION AT MAIN CABIN FLOOR SUPPORT UPPER SURFACE BETWEEN FR 67 TO 68, LBL 46" REF SRM 51-74-00. ACCOMPLISHED A UT THICKNESS INSP AFTER REWORK MAX 0, 110, MIN 0.078, MATERIAL REMOVED 0.042. MX-3 SN 38265, CAL DATE 17, DEC 11, FOUND OUT OF LIMITS IANov 11, 2011 · N622VA · Airbus A320214 · Fuselage Miscellaneous StructureSDR VQI2011F00028Floor Support · corrodedREMOVED CORROSION AT CABIN FLOOR SUPPORT UPPER SURFACE BETWEEN FR 68 AND 69, LBL 66. FOURN OUT OF LIMITS IAW SRM 53-00-14. R & R FLOORBEAM SUPPORT IAW SRM 53-0014 AND 51-42-11, 51-21-11.Nov 8, 2011 · N622VA · Airbus A320214 · Fuselage Miscellaneous StructureSDR VQI2011F00029Floor Panel · corrodedCABIN FLOOR PANEL 262FF HAS CORROSION SPOTS NEAR R-2 DOOR ENTRANCE AND AROUND FWD GIRT BAR LATCH. (REMOVED CORROSION, ACCOMPLISHED AUT THICKNESS. FOUND OUT OF LIMITS, CORROSION LEVEL 2) REPLACED BY NEW PART FLOOR PANEL 262FF, PN D5367180500500 IAW A320, SRM Oct 31, 2011 · N622VA · Airbus A320214 · Fuselage Floor PanelSDR VQI2009F00002Computer · malfunctionedFLIGHT DEPARTED 3 MINUTES EARLY AT 0422Z, WITH T/O AT 0433Z. ALSO AT 0433Z THE ACFT REPORTED ELAC 1 AND 2 AILERON ORDER DISAGREE THRU EFCS 1 AND 2 AS FAILURE MESSAGES. SHORTLY AFTER THIS, CAPT CONTACTS MX VIA AIRCELL. MX CONCURS WITH CAPT TO RETURN TO DEPAROct 22, 2009 · N622VA · Airbus A320214 · Elevator Control System
Back to N622VA