N911VV
Service difficulty reports not matched to an aircraft · 23
They name N911VV, 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 = 'N911VV' 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 = 'N911VV' 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 VJ9800514Skin · chafedVERTICAL SKIN ON LT AND RT UPPER AND LOWER BANANA FAIRING CHAFED. RT UPPER BANANA FAIRING SKIN CHAFED OUT OF LIMIT IAW DC9 SRM 55-01. REMOVED SKIN, FABRICATED AND INSTALLED NEW SKIN IAW DC9 SRM 51-10-4, 51-10-3, 51-30-2 AND 55-01.SDR VJ9800445Skin · gougedGOUGE IN FUSELAGE SKIN AT FS 967, L21-22R, BEYOND LIMIT IAW DC9 SRM 53-04, FIG 8. BLENDED AREA, FABRICATED AND INSTALLED DOUBLER REPAIR IAW DC9 SRM 51-10-3, 53-31-0 FIG 8 AND 53-04 FIG 38.SDR VJ9800482Spar · magnetizedREPAIR ON AFT SIDE REAR SPAR LWR CAP XRS 525 DETERMINED TO BE MAGNETIC WITHIN 5 FEET FLUX VALVE. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 51-10-3, 51-10-4 AND AIRTRAN RES 981625.SDR VJ9800513Tab · corrodedRT ELEVATOR GEAR TAB HAS 1 INCH DIAMETER CORROSION SPOT. CUT OUT CORROSION, CLEANED AREA, FABRICATED AND INSTALLED DOUBLER IAW DC9 SRM 51-70-2.SDR VJ9800538Fitting · corrodedAFT CABIN FLOORBEAM AT FS 996 RIGHT SIDE FITTING CORRODED. REPLACED FITTING IAW DC9 SRM 51-30-5, 51-10-4, 51-10-3 AND 53-01 FIG 1.SDR VJ9800547Panel · lightning strikeLIGHTNING STRIKE LT WINDOW PANEL AT 465 TO 484. REMOVED PANEL, CUT OUT SECTION, FABRICATED DOUBLERS AND FILLERS PLUS TWO INTERNAL DOUBLERS. INSTALLED REPAIR PARTS AND WINDOW PANEL IAW DC9 SRM 53-04 FIG 34.SDR VJ9800512Window Panel · lightning strikeRT WINDOW PANE HAS LIGHTNING STRIKE OUT OF LIMIT AT FS 813 TO 869. REPLACED WINDOW PANEL IAW DC9 SRM 51-30-2, 51-10-4, 51-10-3 AND 53-05, FIG 111.SDR VJ9800479Spar · corrodedRT WING LOWER REAR SPAR XW 530 VERTICAL LEG CORRODED. FABRICATED, INSTALLED REPAIR DOUBLER IAW DC9 SRM 51-30-1, 51-10-4, 53-22-1, AND AIRTRAN RES 981582.SDR VJ9800548Bulkhead Doubler · corrodedUPPER RT DOUBLER AT BULKHEAD WEB FS 996 CORRODED. REMOVED CORRODED DOUBLER, FABRICATED AND INSTALLED NEW DOUBLER IAW DC9 SRM 51-10-3, 51-10-2 AND 53-02 FIG 2.SDR VJ9800444Skin · gougedSKIN AT FS 962, L25R, GOUGED BEYOND LIMIT IAW DC9 SRM 53-04, FIG 38. CUT OUT GOUGE, FABRICATED AND INSTALLED EXTERNAL AND FINGER DOUBLERS IAW DC9 SRM 53-04, FIG 38, 51-10-3 AND 51-30-2.SDR VJ9800549Skin · corrodedFUSELAGE SKIN AT FS 579, L30, CORRODED. CUT OUT SECTION OF SKIN, FABRICATED AND INSTALLED EXTERNAL DOUBLER AND FINGER DOUBLERS IAW DC9 SRM 53-04 FIG 12B, 51-10-3, 51-30-1.SDR VJ9800478Frame · crackedMAIN FRAME RT FS 966 CRACKED. REPLACED FRAME IAW AIRTRAN EO 12-5311-29-B1044 AND RES 981533.SDR VJ9800551Floorbeam · corrodedAFT RT LAV FLOORBEAM AT FS 996 CORRODED FROM FUSELAGE TO LAV ENTRANCE. REMOVED RT CABLE RUN AND RT O/B PULLEY TOWER. CUT OUT CORRODED SECTION, TREATED AREA, FABRICATED AND INSTALLED FLOORBEAM SPLICE, FLOORBEAM WEB, ATTACH ANGLE, ANGLES AND ATTACH ANGLE BRACKSDR VJ9800550Z Section · corrodedAFT CABIN CENTER Z SECTION AT FS 945, RBL 2-20 AND LBL 2-20, CORRODED FROM BULKHEAD TO BULKHEAD. CORROSION OUT OF LIMIT IAW DC9 SRM 53-01, FIG 1. BROKE CABLE TENSION ON RUNS 129 AND 130 AND REMOVED CABLE BRACKETS. FABRICATED AND INSTALLED Z SECTION REPAIRS SDR VJ9800554Skin · dentedTHE AFT VENTRAL STAIRS CONTAINED 27 DENTS TOO CLOSE TOGETHER IAW DC9 SRM 51-50-1, FIG 1-2A. REPLACED LOWER SKIN AND CORRODED FITTING IAW DC9 SRM 51-30-5, 51-30-0, 51-10-4 AND MM 52-63-0 PG 501.SDR VJ9800553Floor · corrodedAFT GALLEY FLOOR PANEL CORRODED. REMOVED FLOOR PANEL, FABRICATED AND INSTALLED NEW HAT SECTIONS AND FLOOR PANEL IAW DC9 SRM 51-20-0, 51-30-2, 53-21-0, FIG 4 AND 51-10-3.SDR VJ9800552Longeron · corrodedFORWARD PIT UNDER AUX TANK AT FS 579, L30, CORRODED. REPLACED L30 AT FS 579 IAW DC9 SRM 53-02 FIG 14.SDR VJ9800511Skin · corrodedAFT VENTRAL STAIRS HAD DENTS TOO CLOSE TOGETHER IAW DC9 SRM 51-50-1, FIG 1-2A. REPLACED LOWER SKIN AND CORRODED FITTING IAW DC9 SRM 51-30-5, 51-30-0, 51-10-4 AND MM 52-63-0, PG 501.SDR VJ9800555Seat Track · corrodedFOUND CORROSION AROUND FASTENER HOLES ON SEAT TRACK AT FS 917 TO 996 LT. REPLACED SEAT TRACK IAW DC9 SRM 53-01 FIG 1, 51-10-4, 51-30-1 AND 51-10-3.SDR 96ZZZM998Oxygen Line · looseON FLT 230 - DFW-ATL - THE CABIN OXYGEN SYSTEM MANUALLY SURGED, OXYGEN MASKS DOORS DID NOT OPEN. CONNECTED SUPPLY LINE TO AFT FLIGHT ATTENDANT PSU AND OPERATED CABIN OXYGEN SYSTEM, ALL PSU DOORS DROPPED, OPS CHECK GOOD.SDR 96ZZZM997Controller · malfunctionedON FLT 230 - DFW-ATL - THE CABIN ALTITUDE ROSE TO 12000 FEET AND WAS UNCONTROLLABLE AT FLIGHT LEVEL 330 FEET, INITIATED EMERGENCY DESCENT. THE FLIGHT HAD BEEN IN PRECIPITATION AT 33000 FEET FOR APPROXIMATELY 30 MINUTES, CABIN ALTITUDE CONTROL WAS REGAINED AT SDR 96ZZZM822Csd · malfunctionedFLT 520 - ATL-ATL, AIR RETURN FOR MTC CONVENIENCE, THE RIGHT CSD ROSE INTO THE CAUTION RANGE, APPROACHING THE RED LINE. LEFT GENERATOR PREVIOUSLY ON MEL. CLEARED MEL ON LEFT GENERATOR BY ADJUSTING CSD FREQUENCY PER 24-10 AND ASSIGNED MEL TO RIGHT CSD. (M)SDR 95ZZZX4173Coffee Maker · overheatingATL - FLT 166 - SMOKE IN COCKPIT ON APPROACH TO ATL. FOUND TO BE FORWARD GALLEY COFFEE MAKER OVERHEATING. REMOVED COFFEE MAKER AND PLACED ON MEL.
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