N855VA, cancelled Jul 30, 2024
Service difficulty reports · 21
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 = 'N855VA' AND deregistration_id = 'N855VA-2024-07-30' 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 = 'N855VA' AND deregistration_id = 'N855VA-2024-07-30' 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 ASAA2024040450033Skin · dentedRIGHT WING, DENT ON I/B FLAP LOWER SKIN, 13 CM FROM UPPER EDGE, .812 MM DEEP, 17MM DIA 220 CM FROM INNER EDGEDOT: B386 GROUNDED - YES. ALL WORK ACCOMPLISHED ON CARD G1941548. PREFORED CATEGORY A PERMANENT REPAIR ON R/W I/B FLAP LOWER SURFACE IN ZONE 2. REPAIRSDR ASAA2024040450032Skin · dentedLEFT WING, I/B FLAP HAS SEVERAL 3 DENTS ON LOWER SKIN ABOVE PYLON FAIRING 7CM LONG 2CM WIDE UNABLE TO MEASURE DEPTH DUE TO FAIRING GROUNDED - YES. REPAIRED LEFT WING I/B FLAP LOWER SKIN LOCATED 13 Ï¿½Ï¿½ FROM OUTBRD AND STOPS AT 10 Ï¿½Ï¿½ AND 8Ï¿½ FROM T/E. ISDR ASAA2024040350523Skin · gougedAFT LOWER EXTERNAL FUSELAGE, FRAME 58 TO 59 AT ANTENNA MOUNT, SKIN IS GOUGED GROUNDED - YES. REMOVED ANTENNA IAW AMM A320 34-42-11-000-001A REV 10. ORIGINAL MAT .118" IAW A320 SRM 53-41-11-42B REV 148. BLENDED DAMAGE, REMAINING MAT .115, LENGT 1.2", WIDTH .800SDR ASAA2024040350522Skin · gougedAFT LOWER EXTERNAL FUSELAGE, BELOW AFT CARGO DOOR, FRAME 55 TO 56 AT ANTENNA MOUNT, SKIN IS GOUGED GROUNDED - YES. REMOVED ANTENNA IAW A320 AMM 34-42-11-000-001-A REV 10. ORIGINAL MAT .118 IAW A320 SRM 53-41-11-42B REV 148. BLENDED DAMAGE, REMAINING MAT .110, SDR ASAA2024040250001Skin Panel · corrodedFWD LOWER EXTERNAL FUSELAGE SKIN BETWEEN FRAME 33 AND 34 HAS CORROSION AT DRAIN/VENT PORT GROUNDED - YES. REMOVED FASTENERS TO FOM CORROSION REMOVAL IAW A320 SRM 51-42-11/001, PARA ZE, REV148. REMOVED CORROSION IAW A-320 SRM 51-74-00/001, PARA 5-A3, REV148 ANDSDR ASAA2024032950069Door Frame · corrodedAFT CARGO BAY FLOOR ON DOOR FRAME AT C53R CORRODED. GROUNDED - YES. REMOVED 2EA FASTENERS IAW A320 SRM 51-42-11/001/REV 148-01FEB2024. REMOVED CORROSION AND FOUND WITHIN LIMITS IAW A320 SRM 53-41-49-283-004 REV 148- 01FEB2024. ACCOMPLISHED DVI AND HFEC INSPECTSDR ASAA2024032950062Door Frame · corrodedAFT CARGO BAY FLOOR, AT DOOR FRAME FORWARD CORNER AT NET MOUNT PUCK, BETWEEN C52R AND C53R GROUNDED - YES. REMOVED 2EA FASTENERS IN CORRODED AREA IAW A320 SRM 51-42-11/001 REV 148-01FEB.2024. REMOVED CORROSION IN AREA WITH A REMAINING THICKNESS OF .087 AND FOUSDR ASAA2024032950031Web · corrodedAFT CARGO BAY FLOOR CORRODED AT STATION C53R FROM 16 TO 20 INCHES RIGHT OF CENTERLINE. GROUNDED - YES. REMOVED 6EA FASTENERS IAW A320 SRM 51-42-11/001/REV 148-01FEB2024. REMOVED CORROSION AND FOUND WITHIN LIMITS IAW A320 SRM 53-41-49-283-004 REV 148- 01FEB202SDR ASAA2024032950030Door Frame · corrodedAFT CARGO BAY FLOOR DOOR FRAME FORWARD C53R. GROUNDED - YES. REMOVED 4EA FASTENERS IAW A320 SRM 51-42-11/001/REV 148-01FEB2024. REMOVED CORROSION AND FOUND WITHIN LIMITS IAW A320 SRM 53-41-49-283-004 REV 148- 01FEB2024. ACCOMPLISHED DVI AND HFEC INSPECTION IASDR ASAA2024032950029Web · corrodedAFT CARGO BAY FLOOR ON DOOR FRAME CORRODED JUST AFT OF C54R 2 PLACES 24 INCHES RIGHT OF CENTER. GROUNDED - YES. REMOVED 2EA FASTENER IAW A320 SRM 51-42-11/001/REV 148-01FEB2024. REMOVED CORROSION AND FOUND WITHIN LIMITS IAW A320 SRM 53-41-49-283-004 REV 148- SDR ASAA2024032950005Web · corrodedAFT CARGO BAY FLOOR DOOR FRAME CORRODED FORWARD OF C54R 2 PLACES 24 INCHES RIGHT OF CENTER GROUNDED - YES. REMOVED 1EA FASTENER IAW A320 SRM 51-42-11/001/REV 148-01FEB2024. REMOVED CORROSION AND FOUND WITHIN LIMITS IAW A320 SRM 53-41-49-283-004 REV 148- 01FEB2SDR ASAA2024032950004Web · corrodedAFT CARGO BAY FLOOR JUST INSIDE DOOR NEAR AFT DOOR FRAME CORRODED AT AND AROUND NET MOUNT PUCK AT STATION 56R 20 INCHES RIGHT OF CENTER. GROUNDED - YES. REMOVED 1EA FASTENER IAW A320 SRM 51-42-11/001/REV 148-01FEB2024. REMOVED CORROSION AND FOUND WITHIN LIMITSSDR ASAA2024032950003Door Frame · corrodedAFT CARGO BAY FLOOR ON DOOR FRAME CORRODED AT STATION C55R GROUNDED - YES. REMOVED 1EA FASTENER IAW A320 SRM 51-42-11/001/REV 148-01FEB2024. REMOVED CORROSION AND FOUND WITHIN LIMITS IAW A320 SRM 53-41-49-283-004 REV 148- 01FEB2024. ACCOMPLISHED DVI AND HFEC ISDR ASAA2024032950002Torque Box · corrodedAFT CARGO BAY FLOOR JUST INSIDE DOOR NEAR AFT DOOR FRAME CORRODED AT LOCK FASTENER, JUST FORWARD OF STATION C5624 INCHES RIGHT OF CENTERLINE GROUNDED - YES. REMOVED 3EA FASTENERS IAW A320 SRM 51-42-11/001/REV 148-01. REMOVED CORROSION AND FOUND WITHIN LIMITS ISDR ASAA2024031550036Skin · dentedLESSOR ITEM: MULTIPLE LOWER FLAP DENTS BEHIND RIGHT MAIN WHEEL, MAP AND MEASURE ALL. GROUNDED - YES. PERFORMED CATEGORY A PERMANENT REPAIR IN 2EA AREAS ON R/W I/B FLAP LOWER SURFACE IN ZONE 2.AREA 1 REPAIR MEASURES 55" FROM I/B EDGE, 6" FROM T/E REPAIR DOUBLESDR ASAA2024031550035Skin · dentedLESSOR ITEM: MULTIPLE LOWER FLAP DENTS BEHIND LEFT MAIN WHEEL, MAP AND MEASURE ALL GROUNDED - YES. REPAIRED CLUSTER 1 DENTS ON L/W LOWER FLAP, FINAL MEASUREMENT OF REPAIR IS 14.4" X 11.4" LOCATED 45.25" FROM INBOARD AND STOPS 59.65". CLUSTER 2 IS BEING TRACKSDR ASAA2022110140679Skin · gougedFWD CARGO DOOR, OUTER SKIN FWD EDGE BENT/DENT WITH A GOUGE IN THE MIDDLE AT 29" FROM LOWER EDGE. GROUNDED - YES. ACCOMPLISHED A CATEGORY "B" REPAIR ON THE FORWARD CARGO COMPARTMENT DOOR, PART # D5237175000800, SERIAL # UH15179 IAW ASA EA # CMPT-52EA-01622 REV SDR VQIA2018F00018Unknown · odorSTRONG CHEMICAL ODOR LIKE BURNED HYDRAULIC FLUID OR OIL COMBINATION DURING TAKEOFF AND DESCENT. PERFORMED TSM 055000810831A, NO DEFECTS NOTED.SDR VQIA2017F00060Control Lever · failedON 10/20/17 A/C N855VA OPERATING VX1067 AN AIRBUS A320-314 WITH 19772 FLT HOURS AND 5977 CYCLES HAD THE FOLLOWING DEFECT ON APPROACH TO SFO: LANDING GEAR WOULD NOT EXTEND WHEN HANDLE PLACED DOWN. PERFORMED MANUAL GEAR EXTENSION. CREW LANDED SAFELY AND DID NSDR VQIA2017080900033Fmc · failedON SELECTING FLAPS 0 AFTER TAKEOFF, LOST FMA INFORMATION AND ENGS TRIED TO SLOW TO IDLE. RESET A/P & A/T, SYSTEMS NORMAL AFTER THAT, NO ECAM. PERFORMED OPS TEST OF AFS IAW AMM 22-96-00-71-00-01A, BITE TEST OF EFCS IAW AMM 27-96-00-74-00-01A. PERFORMED OPSSDR VQI20140822000019Fan · failedACFT ENCOUNTERED A VENT BLOWER FAULT IN FLIGHT, COMPLIED WITH ECAM. ELECTRICAL SMOKE FUMES WERE PERCEIVED FOR APPROXIMATELY 5 MINUTES. ON ARRIVAL, MAINTENANCE ACCOMPLISHED INSPECTION FOR ELECTRICAL SMOKE ODOR IAW TSM 05-50-00-810-831-A. VERIFIED INOPERATI
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