N626VA
Service difficulty reports not matched to an aircraft · 22
They name N626VA, 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 = 'N626VA' 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.
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 = 'N626VA' AND registry_match IS NULL ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR ASAA2020042732681Beam · corrodedAFT MAIN CABIN LONGITUDINAL BEAM AT FR 67 LBL 3 HAD CORROSION. GROUNDED - YES. REMOVED AND REPLACED AFT MAIN CABIN LONGITUDINAL BEAM AT FR 67 LBL 3 IAW A320 SRM 51-42-11SDR ASAA2020042732680Support Fitting · corrodedAFT MAIN CABIN FLOOR SUPPORT FITTING AT FR 68 RBL 8 HAD CORROSION. GROUNDED - YES. REMOVED AND REPLACED AFT MAIN CABIN FLOOR SUPPORT FITTING AT FR 68 RBL 8 IAW A320 SRM 51-42-11 AND AIRBUS DWG D53472097.SDR ASAA2020042732679Beam · corrodedAFT MAIN CABIN LONGITUDINAL BEAM BETWEEN FR 68-70 RBL 7 HAD CORROSION. GROUNDED - YES. REMOVED AND REPLACED AFT MAIN CABIN LONGITUDINAL BEAM BETWEEN FR 68-70 RBL7 IAW A320 SRM 51-42-11SDR ASAA2020042732678Beam · corrodedAFT MAIN CABIN LONGITUDINAL BEAM AT FR 68 RBL 29 HAD CORROSION. GROUNDED - YES. REMOVED AND REPLACED AFT MAIN CABIN LONGITUDINAL BEAM AT FR 68 RBL 29 IAW A320 SRM 51-42-11.SDR ASAA2020042732677Beam · corrodedAFT MAIN CABIN LONGITUDINAL BEAM AT FR 68 RBL 46 HAD CORROSION. GROUNDED - YES. REMOVED AND REPLACED AFT MAIN CABIN LONGITUDINAL BEAM AT FR 68 RBL 46 IAW A320 SRM 51-42-11 AND AIRBUS DWG D53472458.SDR ASAA2020042432670Floor Support · corrodedAFT MAIN CABIN FLOOR SUPPORT FITTING AT FR 68 LBL 8 HAS CORROSION GROUNDED - YES. REMOVED AND REPLACED AFT MAIN CABIN FLOOR SUPPORT FITTING AT FR 68 LBL 8 IAW AIRBUS DWG D53472096000 AND A320 SRM 51-42-11SDR ASAA2020042432669Beam · corrodedAFT CABIN LONGITUDINAL BEAM BETWEEN FR 68-70 LBL 7 HAD CORROSION GROUNDED - YES. REMOVED AND REPLACED AFT MAIN CABIN LONGITUDINAL BEAM BETWEEN FR 68-70 LBL 7 IAW AIRBUS DWG D5347209600, DWG D53472780000 AND A320 SRM 51-42-11SDR ASAA2020042732676Beam · corrodedAFT MAIN CABIN L/H LONGITUDINAL BEAM BETWEEN FR 69-70 Y=+638 HAD CORROSION. GROUNDED - YES. REMOVED AND REPLACED AFT MAIN CABIN L/H LONGITUDINAL BEAM BETWEEN FR 69-70 Y=+638 IAW A320 SRM 51-42-11, AIRBUS DWG D53472837 AND EA A320-53EA-00469.SDR ASAA2020042732675Beam · corrodedAFT MAIN CABIN R/H LONGITUDINAL BEAM HAD CORROSION ON UPPER SURFACE BETWEEN FR 67-68 Y=-765. GROUNDED - YES. REMOVED AND REPLACED AFT MAIN CABIN R/H LONGITUDINAL BEAM BETWEEN FR 67-68 Y=-765 IAW A320 SRM 51-42-11 AND AIRBUS DWG D53472093 AND D53472836.SDR ASAA2020042732674Beam · corrodedAFT MAIN CABIN R/H LONGITUDINAL BEAM BETWEEN FR 66-68 Y=-1162 HAD SEVERAL CORRODED AREAS. GROUNDED - YES. REMOVED AND REPLACED AFT MAIN CABIN R/H LONGITUDINAL BEAM BETWEEN FR 66-68 Y=-1162 IAW A320 SRM 51-42-11, AIRBUS DWG 53472836 AND EA A320-53EA-00469.SDR ASAA2019011327779Light · inoperativeFOUND EMERGENCY AISLE LIGHT INOP AT ROW 6 FOUND EMERGENCY AISLE LIGHT INOP AT ROW 29 GROUNDED - YES. R/R SEAT MOUNTED EMERGENCY LIGHT IAW AMM 33-51-19. OPS CHECK GOOD, OK FOR SERVICE. BUTT SPLICE EMERGENCY AISLE LIGHT WIRE IAW ESPM 20-43-11. OPS CHECK GOOD,SDR VQI2017F00007Warning Light · false activationCHECK SLIDE PRESSURE OVERWING BOTH SIDES. DEFECT WAS DETERMINED TO BE INDICATION ONLY. OVERWING EXIT DOORS BOTH LT AND RT SLIDE BOTTLE PRESSURE HAS BEEN VERIFIED TO HAVE THE CORRECT PRESSURE LEVEL. RESET CIDS 1 & 2, POWER UP TEST SUCCESSFUL IAW AMM 23-73-0SDR VQIA2017080800025Tube · crackedEXPERIENCED A LOSS OF YELLOW HYDRAULIC SYS QTY AND PRESSURE. THE ACFT CONTINUED TO ITS DESTINATION AND LANDED WITHOUT INCIDENT, LOSS OF NOSE WHEEL STEERING. DURING TROUBLESHOOTING TECHNICIANS DISCOVERED A CRACK IN THE YELLOW SYS PRESSURE RELIEF RETURN TUBE OSDR VQIA2016120500001Eiu · failedTHE ACFT HAD A CABIN ALTITUDE WARNING AT FL350. PERFORMED AN EMERGENCY DECENT, AND DIVERTED. ON THE GROUND PERFORMED TSM 21-31-00-810-809-A, AND FOUND THAT BOTH AIR PACK FLOW CONTROL VALVES WERE CLOSED. PERFORMED AMM 21-31-00-710-002-A, 21-31-00-710-003-A, ASDR VQI2015F00016Line · brokenACFT LANDED SAFELY AFTER LOSING GREEN HYDRAULIC SYSTEM QUANTITY AND DECLARING AN EMERGENCY. THE CREW ENTRIES: "HYD GREEN RSRV LO LEVEL IN FLIGHT" AND " HYD GREEN ENG 1 PUMP LO PR IN FLIGHT". MAINTENANCE FOUND PRESSURE RELIEF LINE BROKEN AND PROCEEDED TO REPLSDR XE4R2015FA0000203Floor Panel · corrodedR-2 ENTRY WAY DOOR FLOOR PANEL 262FF AT FRAME 68 TO 70 HAS CORROSION BEYOND LIMITS. R & R THE FLOOR PANEL IAW SRM 53-42-12.SDR VQI20150318000008Unknown · odorCREW REPORTED INBOUND, AN OIL ODOR DETECTED AT TOP OF DESCENT IN MAIN CABIN. MAINTENANCE WAS CALLED OUT AND PERFORMED THE FOLLOWING: PERFORMED 2 ENGINE RUN, 1 AT A TIME, 5 MINUTE RUN, EACH WITH BOTH PACKS ON NO SMELL NOTED. TEST IAW 71-00-00. OK FOR SERVICSDR VQI2013F00031Bushing · out of alignmentCREW NOTED L1 DOOR GUST LOCK WOULD NOT ENGAGE WHEN DOOR WAS OPENED ON ARRIVAL. EVALUATED AND REALIGNED THE NYLON BUSHING. L1 GUST LOCK OPERATED NORMALLY IAW AMM 52-10-00-06. ACFT DEPARTED AND NO FURTHER DISCREPANCIES WERE NOTED.SDR VQI2013F00030Gust Lock · damagedCABIN CREW NOTED L1 DOOR GUST LOCK WOULD NOT ENGAGE WHEN THE DOOR WAS OPENED UPON ARRIVAL AT DESTINATION. MX TECH EVALUATED AND RE-ALIGNED THE NYLON BUSHING. THE L-1 GUST LOCK OPERATED NORMALLY IAW AMM 52-10-00-06. THE ACFT DEPARTED AND NO FURTHER DISCREPANSDR VQIA2013F00027Gust Lock · contaminatedCABIN CREW REPORTED L1 DOOR GUST LOCK WOULD NOT ENGAGE. FOUND EXCESSIVE GREASE ON CATCH PIN. GREASE CLEANED. L1 DOOR GUST LOCK OPERATED NORMALLY IAW AMM 52-10-00-06.SDR VQI2012F00018Skin · delaminatedDURING D1-CHECK, RUDDER THERMOGRAPHIC INSP WAS PERFORMED IAW MPD TASK 554008-01-1, REVEALING EVIDENCE OF TRAPPED MOISTURE AT THE UPPER AND LOWER AFT HOIST POINTS ON THE RT SIDE OF THE RUDDER. RESONANCE FREQUENCY AND ULTRASONIC INSPECTIONS WERE ACCOMPLISHED IASDR VQI2008F00003Controller · failedFLIGHT PHASE 6 CLIMB DEPARTED JFK AT 1127 Z - RETURNED TO FIELD AT 1200 Z. CREW REPORTED A NORMAL DEPARTURE WITH NO ABNORMALITIES UNTIL AROUND 10,000 FT WHEN THEY NOTICED AN AIRFRAME VIBRATION. CHECKING WITH THE FLT TEAM, THEY CONFIRMED THAT A CREW REPORTED
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