N196SY
Service difficulty reports · 16
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 = 'N196SY' AND registry_match = 'registration' 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 = 'N196SY' AND registry_match = 'registration' 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 SWIA2025112400011Window · damagedR1 WINDOW HAS A LIGHTNING STRIKE. REMOVED AND REPLACED R1 WINDOW DOUBLER IAW SRM 51-40-08.SDR SWIA202511240009Seat Track · corrodedRIGHT INBD SEAT TRACK FLANGE BETWEEN FR 84 - 85 CORRODED. PERFORMED REPAIR ON THE SEAT TRACK IAW SRM 53-00-10, REPAIR 01P AND ETD2022-170-022163 REV C.SDR SWI2023F00254Unknown · corrodedMULTIPLE AREAS OF CORROSION ON RH FLOOR BEAM TOP AND BOTTOM SIDE IN AFT GALLEY AT FRAME 87 AS MARKED. (C-CHECK RO 8/18/2023) REMOVED AND REPLACED RH FLOOR BEAM BETWEEN FR 87 REF EMB SRM 51-40-08. SEE CONTINUE CARD FOR WORK PERFORMED.BEAM REPLACED WITH SDR SWI2023F00253Unknown · corrodedRH I/B SEAT TRACK AT FR 16-18 HAS 1EA SPOT OF CORROSION AS MARKED. (C-CHECK RO 8/18/2023) REMOVED AND REPLACED FWD FUSELAGE, R/H I/B SEAT TRACK BEAM BETWEEN FRAMES 12-20.WITH FACTORY REPLACEMENT PART. NO CHANGE IN WEIGHT AND BALLANCE NEEDED.SEE CONTINUASDR SWIA2023082204Unknown · corrodedCORROSION ON LH FLOOR BEAM IN AFT GALLEY AT FRAME 87 AS MARKED. (C-CHECK RO 8/18/2023) REMOVED AND REPLACED LH FLOOR BEAM IN AFT GALLEY FR 87 REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF EMB SRM 51-23-06, CPM 51-25-00-910-001-A. FACTORY PART REPSDR SWIA20230803Unknown · brokenFWD SERVICE DOOR, EMERGENCY EVACUATION SLIDE CABLE SHIELDING PULLED/ BROKEN FROM SWAGING. (C-CHECK RO 8/18/2023) REPAIRED FWD SERVICE DOOR, EMERGENCY EVACUATION SLIDE CABLE SHIELDING WHERE PULLED/ BROKEN FROM SWAGING AS MARKED, IN REFERENCE TO RS-2022-3SDR SWIA202308221Unknown · damagedAFT PASSENGER-DOOR SLIDE ARMING CABLE OUTER COVERING IS PULLING AWAY ON UPPER END AS MARKED. (C-CHECK RO 8/18/2023) REPAIRED AFT PAX DOOR, EMERGENCY EVACUATION SLIDE CABLE WHERE OUTER COVERING WAS PULLING AWAY ON UPPER END, IN REFERENCE TO RS-2022-3017.SDR SWIA202054447Oven · smokeFLIGHT ATTENDANT REPORTS THAT FORWARD GALLEY OVEN WAS SMOKING WHILE IN SERVICE. SMOKE DISSIPATED UPON SHUTTING OVEN OFF. FLIGHT 3357-FILED CLOSED. TROUBLESHOT PER FIM. VERIFIED SMOKE AND BURNING SMELL TO BE COMING FROM FWD GALLEY OVEN. REMOVED AND REPLACESDR SWIA2020082552079Isolator · damagedFORWARD CARGO DOOR INTERNAL SURFACE HAS 2 EACH THREADED ISOLATORS THAT ARE DAMAGED ACROSS THE CENTER OF THE DOOR, AS MARKED. (C-CHECK 8/24/2020)REMOVED AND REPLACED ISOLATORS ATFWD CARGO DOOR REF SRM APPLIED TOP COAT SRM.SDR SWIA202008252078Isolator · damagedAFT CARGO DOOR INTERNAL SURFACE HAS 6 EACH THREADED ISOLATORS THAT ARE DAMAGED ACROSS THE CENTER OF THE DOOR. REMOVED AND REPLACED 6 EACH AFT CARGO DOOR INTERNAL SURFACE THREADED ISOLATORS IAW SRM.SDR SWIA202052077Muffler · unbondedRACK 300 - APU INLET SILENCER VANE DISBONDED AS MARKED (C-CHECK 8/24/2020) UPON FURTHER EVALUATION FOUND APU INLET SILENCER TO BE OUT OF LIMITS DUE TO LOOSE SPLITTER AND FAILURE OF FEELER GUAGE CHECK. REPLACE SILENCER IAW AMM. REPLACED AND INSTALLED APU INLETSDR SWIA202008252076Nut Plate · brokenONE BROKEN NUT PLATE AT 6 O'CLOCK POSITION WHERE THE FORWARD BELLY FAIRING AFT EDGE IS SECURED TO THE FUSELAGE. REMOVED AND REPLACED THE NUTPLATE IAW SRM.SDR SWIA202008252075Winglet · deformedRIGHT WINGLET LEADING EDGE WAS DEFORMED ALONG THE TRAILING EDGES. COMPLIED WITH ETD2020-170-025264. RECONTOURING OF RT WINGLET LEADING EDGE.SDR SWIA202008252074Structure · chafedENG 2 INBD UPPER BEAVER TAIL, FRAME AND COMPOSITE ARE CHAFED. REPAIRED THE NR 2 UPPER I/B BEAVER TAIL IAW CMM.SDR SWIA202008252073Structure · chafedENG 2 OTBD UPPER BEAVER TAIL, FRAME AND COMPOSITE ARE CHAFED. REPAIRED THE NR 2 UPPER O/B BEAVER TAIL IAW CMM.SDR SWIA202008252072Frame · chafedENGINE 1 UPPER INBD BEAVER TAIL, COMPOSITE AND FRAME ARE CHAFED. REPAIRED THE NR 1 UPPER I/B BEAVER TAIL IAW CMM.
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