N296SW, cancelled Jul 3, 2017

Service difficulty reports · 110

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 = 'N296SW' AND deregistration_id = 'N296SW-2017-07-03'
  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.

SDR SWIA200110112Valve · leakingAFTER TAKE OFF, RIGHT DUCT LEAK LIGHT CAME ON. FOLLOWED QRH PROCEDURE AND AFTER 3 MINUTES WE SHUT DOWN THE RIGHT ENGINE IN FLIGHT. RETURNED TO FAT REPLACED RIGHT PRESSURE REGULATING VALVE. OPS CHECK GOOD. PERFORMED EXTENSIVE GROUND RUNS, NO DUCT LEAK LIGHAug 19, 2001 · N296SW · Emb EMB120ER · Airfoil Anti/De-ice SystemSDR SWIA972338Uplock Switch · out of adjWHEN LANDING GEAR WAS SELECTED UP THE RIGHT GEAR INDICATOR TWO RED LIGHTS, NO GREEN, AND WE COULD HEAR THAT A GEAR DOOR WAS OPEN. NORMAL INDICATIONS WHEN GEAR SELECTED DOWN. RETURNED TO MRY. ADJUSTED RIGHT MLG UPLOCK SWITCH IAW MM 32-61-01. SWUNG GEAR SEVEFeb 5, 2001 · N296SW · Emb EMB120ER · Landing Gear Position and WarningSDR SWIA972064Actuator · failedDURING LEVEL OFF AT FL 240 FROM 250 ELEVATOR TRIM WHEELS MOVED FORE AND AFT RAPIDLY AND APPEARED TO BE JAMMED. THEN GOT A TRIM FAIL MAP WARNING. DISENGAGED THE AUTO PILOT AND CONFIRMED TRIM WHEELS WERE FROZEN. CONSULTED QRH AND HAND FLEW TO BELOW THE FREEZIOct 30, 2000 · N296SW · Emb EMB120ER · Elevator Tab Control SystemSDR SWIA971630Control Unit · failedFLAP CONTROL FAULT ILLUMINATED IN FLIGHT AND WOULD NOT RESET. RETURNED TO LAX. REPLACED FLAP CONTROL UNIT. OPS CHECKS GOOD, SN ON 0057, SN OFF 0031.Dec 19, 1999 · N296SW · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA971542Panel · looseENGINE PANEL ON TOP WAS NOT SECURE. RETURNED TO FAT. INSPECTED AREA AROUND ENGINE COWL ACCESS PANEL AND OBSERVED NO DAMAGE. SECURED PANEL.Aug 9, 1999 · N296SW · Emb EMB120ER · Engine Cowling SystemSDR SWIA971204Strap · corrodedNUMEROUS AREAS OF CORROSION IN AFT CENTER FLOOR BUTT STRAP. REPLACED AFT CENTER FLOOR BUTT STRAP IAW SRM 51-40-02.May 5, 1998 · N296SW · Emb EMB120ER · Fuselage Miscellaneous StructureSDR SWIA971203Frame · corrodedCORROSION PITTING ON CROSS FRAME JUST AFT OF RIGHT AFT SEAT TRACK. REPLACED CROSS FRAME UPPER MEMBER SRM 51-40-02.May 5, 1998 · N296SW · Emb EMB120ER · Fuselage Main, FrameSDR SWIA971202Strap · corrodedNUMEROUS AREAS OF CORROSION ON RIGHT AFT FLOOR BUTT STRAP, REPLACED STRAP. REPLACED RIGHT AFT BUTT STRAP SRM 51-40-02.May 5, 1998 · N296SW · Emb EMB120ER · Fuselage Miscellaneous StructureSDR SWIA971167Bulbs · failedSERVICE DOOR LIGHT REMAINS LIT AFTER TAKEOFF. RETURNED TO FIELD. MEL 52-70-1. INSTALLED NEW BULBS IN SERVICE DOOR LIGHT. LIGHT CHECKS GOOD AT THIS TIME.Apr 10, 1998 · N296SW · Emb EMB120ER · Door Warning SystemSDR XC4R9720736Brush · failedSTART/GEN BRUSHES FAILED AFTER 277.0 HOURS OF FLIGHT TIME. THE BRUSH SHUNT LEADS WERE BURNED AND BROKEN OFF. THIS WAS A NEW AIRCRAFT, THIS WAS A NEW STARTER GENERATOR WITH ONLY 277.0 HOURS SINCE NEW. SUBMITTER RECOMMENDS RE-DESIGNING DEFECTIVE BRUSHES. NOTFeb 8, 1997 · N296SW · Emb EMB120ER · Starter-Generator
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