N627VA
Service difficulty reports not matched to an aircraft · 28
They name N627VA, 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 = 'N627VA' 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 = 'N627VA' 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 ASAA2020042232664Beam · corrodedAFT MAIN CABIN HAD CORROSION AT FR 68 Y -1162 GROUNDED - YES. REMOVED AND REPLACED MAIN CBIN LONGITUDINAL BEAM AT FR 68 Y -1162 IAW AIRBUS DWG D53472780SDR ASAA2020042232663Door Sill · corrodedAFT MAIN CABIN HAD SEVERAL AREAS OF CORROSION ON UPPER SURFACE OF R2 DOOR SILL BEAM AT FR 68 Y -1180 GROUNDED - YES. ACCOMPLISHED PERMANENT REPAIR ON R2 DOOR SILL BEAM IAW A320 SRM 53-41-14-300-001SDR ASAA2020040932662Shear Plate · corrodedAFT CABIN FLOOR RH SHEAR PLATE FR 68-69 Y -1180 HAD CORROSION GROUNDED - YES. REMOVED AND REPLACED CABIN RH SHEAR PLATE FR 68-69 Y -1180 IAW A320 SRM 51-42-11SDR ASAA2020042232661Beam · corrodedAFT MAIN CABIN R/H LONGITUDINAL BEAM HAD CORROSION ON UPPER SURFACE BETWEEN FR 68 AND FR 69 Y -1162 GROUNDED - YES. REMOVED AND REPLACED AFT MAIN CABIN LONGITUDINAL BEAM BETWEEN FR 68-69 Y -1162 IAW AIRBUS DWG D53472458 AND D53472089SDR ASAA2020042232660Splice Angle · corrodedAFT MAIN CABIN R/H LONGITUDINAL BEAM LWR I/B UPPER SPLICE ANGLE HAD CORROSION AROUND FASTENER HOLES AT FR 68 Y -1162 GROUNDED - YES. REMOVED AND REPLACED AFT MAIN CABIN R/H LONGITUDINAL BEAM LWR I/B UPPER SPLICE ANGLE AT FR 68 Y -1162 IAW AIRBUS DWG D53472458SDR ASAA2018110826778Door Frame · corrodedR1 DOOR CUTOUT, FWD LOWER CORNER AT FR16, STRUCTURE BELOW GIRT BAR FITTINGS/BLANKING PLATES HAS CORROSION IN 2 AREAS. GROUNDED - YES. REWORKED 2 EA FASTENER HOLES R1 DOOR CUTOUT, FWD LOWER CORNER GIRT BAR ATTACH POINTS IAW A320 SRM 53-11-14-283-005.SDR ASAA2018110826777Door Frame · corrodedL1 DOOR CUTOUT, AFT LOWER CORNER AT FR20, STRUCTURE BELOW GIRT BAR FITTINGS/BLANKING PLATES HAS CORROSION IN MULTIPLE AREAS. GROUNDED - YES. REWORKED 3 EA FASTENER HOLES AT L1 DOOR AFT LOWER CORNER, GIRT BAR FITTING ATTACH POINTS IAW A320 SRM 53-11-14-283-005.SDR ASAA2018110826776Door Sill · corrodedL-2 DOOR LOWER SILL, AFT END, SCREW HOLES CORRODED. GROUNDED - YES. CUTOUT DAMAGE AND REPAIRED WITH FILLER AND DOUBLER PER AIRBUS A320 SRM 53-41-14 AT L-2 DOOR SILL AFT ENDSDR ASAA2018110826775Seat Track · corrodedMAIN CABIN SEAT TRACK CORRODED ON SCALLOPS AT GALLEY MOUNT FR20, -Y765. GROUNDED - YES. CORROSION FOUND TO BE OUT OF LIMITS IAW A320 SRM 53-00-15-283-001. REMOVED AND REPLACE SEAT TRACK IAW A320 SRM 51-42-11.SDR ASAA2018110826774Floor Support · corrodedAFT WET AREA FLOOR BEAM BETWEEN FR66 AND FR70 AT Y464 HAS CORROSION AT MOUNT HARD POINT. GROUNDED - YES. REMOVED FLOOR BEAM AND REPLACED WITH NEW PER AIRBUS A320 SRM 53-41-14.SDR ASAA2018110896773Seat Track · corrodedMAIN CABIN FWD BELOW FLOOR WET AREA, FRAME C16, BL20R, CORROSION ON UPPER FACE OF FLOOR BEAM. GROUNDED - YES. TRIMMED OUT THE CORRODED SECTION OF THE FLOOR SUPPORT AND ACCOMPLISHED A CATEGORY 'A' REPAIR IAW A320 SRM 53-00-14-300-007.SDR ASAA2018110896771Seat Track · corrodedMAIN CABIN, FWD BELOW FLOOR WET ARE AT FR16, -Y1292 HAS CORROSION ON UPPER FACE OF FLOOR BEAM. GROUNDED - YES. REMOVED AND REPLACED SEAT TRACK FROM FR12-FR24 AT -Y1292 IAW A320 SRM 51-42-11.SDR ASAA2018110896770Floor Support · corrodedMAIN CABIN AFT WET AREA R/H SIDE, FLOOR STRUCTURE HAS CORROSION AROUND BLIND RIVET SHOP HEADS. GROUNDED - YES. REMOVED AND REPLACED FRAME SUPPORT IAW A320 SRM 51-42-11.SDR ASAA2018110896769Floorbeam · corrodedMAIN CABIN AFT WET AREA BELOW FLOOR, FR70 AT Y765 MOUNT HOLE IS GALLED. GROUNDED - YES. REMOVED AND REPLACED FLOOR BEAM IAW A320 SRM 51-42-11.SDR ASAA2018033124100Oil System · leakingSTRONG OIL ODOR IN COCKPIT DURING DESCENT, ACFT GROUNDED. OIL LEAKING FROM LOAD COMPRESSOR DRAIN. APU R & R IAW TASKCARD 4911.000002 & 4911.000003 IN WO 370325, AND OPS AND LEAK CHECKED OK.SDR ASAA2018031823950Unknown · odorODOR IN THE CABIN, FROM ENGINE START TO TOP OF DESCENT. MORE NOTICEABLE IN AFT CABIN. ACFT GROUNDED. IAW TSM 05-50-00-810-831-A RAN THE NR 1 ENGINE, ODOR PRESENT ON THE NR 2 ENGINE. IAW TSM 71-00-00-810-802-A COMPLETED TROUBLESHOOTING. FOUND NO ODSDR 2017FA0000329Pin · failedEXPERIENCED THE FOLLOWING ISSUE DURING LANDING ROLL-OUT. ON LANDING AT 70KTS, THE NOSE OF THE ACFT BEGAN A SIGNIFICANT SHIMMY AND ONCE SLOWED ACFT WAS DIFFICULT TO STEER AS LONG AS TAXI SPEED WAS SLOW, WE COULD TAXI/STEER. UPON INSPECTION THE NOSE LANDING GESDR VQI2017F00012Relay · failedDURING OVERNIGHT MX, EMERGENCY GENERATOR TEST FAILED. R & R RELAY FIN 20XE IAW TSM 242400810804A.SDR VQIA2017081000045Unknown · odorREPORTED AN UNUSUAL ODOR IN THE CABIN. THE INFLIGHT TEAM SHUTDOWN THE IFE AND THE ODOR DISSIPATED. ON ARRIVAL TECHNICIANS ACCOMPLISHED TSM TASK 05-50-00-81-08-31A WITH NO FINDINGS, THE ITEM WAS CLEARED AND THE ACFT WAS RETURNED TO SERVICE. NO ODOR REPORTED SDR VQI2015F00021Control Valve · failedACFT LANDED AFTER OPERATING FLIGHT. AFTER PULLING OFF RUNWAY HAD THE FOLLOWING DEFECT: AFTER LANDING, PARKING BRAKE WOULD NOT RELEASE WITH PARKING BRAKE SWITCH IN "OFF" POSITION. PARKING BRAKE PRESSURE STILL OBSERVED ON BRAKE PRESSURE GAUGE AND "PARKING BRAKSDR VQI2013F00002Wire · brokenACFT WAS HAVING AN OPS TEST OF THE EMERGENCY LIGHT SYSTEM PERFORMED IAW TASK 33-51-00-710-001-A FOLLOWING THE REMOVAL AND REPLACEMENT OF THE R1 SLIDE. DURING THE OPS TEST, THE R1 DOOR PASSED BUT THE L1 DOOR SLIDE INDICATION FAILED THE TEST. UPON REMOVAL OF TSDR VQI2013F00000Transponder · faultyAT FL320, ABOUT 45 MIN INTO FLIGHT, CREW SMELLED BURNING LIKE WIRING AND THEN SAW SMOKE COME INTO COCKPIT. RECEIVED AVIONICS SMOKE MSG ECAM, FOLLOWED ECAM AND QRH PROCEDURE WHICH INCLUDED PLACING BLOWER FAN IN OVERRIDE POSITION AND SMOKE AND SMELL DISSIPATED.SDR VQI2012F00026Wheel · gougedWHILE ACCOMPLISHING MPD TASK 322127-01-1, FOUND GOUGE DAMAGE TO NR 4 MLG WHEEL, PN 20195162, SN 34235/34235 INNER HEAT SHROUD AND WEAR DAMAGE TO NR 4 MLG BRAKE ASSY, PN C202255, SN 04712 MOST INBD DISK. IT APPEARS THAT THE 2 AREAS WERE CHAFING TOGETHER. THE SDR VQI2012F00023Floor Support · corrodedACFT CABIN FLOOR SUPPORT UNDER SHEAR PLATE AT FR 69-70 AFT LT CORRODED.SDR VQI2012F00025Floor Support · corrodedAFT CABIN FLOOR SUPPORT BEAM HAS CORROSION AT FR, RBL10.SDR VQI2012F00024Support · corrodedAFT CABIN SUPPORT BEAM HAS CORROSION BETWEEN FR66-68 AT RBL50.SDR VQI2012F00022Floor Support · corrodedMAIN CABIN FLOOR SUPPORT BEAM AT FR16, LBL8 IS CORRODED.SDR VQI2012F00021Floor Support · corrodedAFT CABIN FLOOR SUPPORT UNDER SHEAR PLATE AT FR 69-70, AFT RT CORRODED.
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