N165YV

Service difficulty reports · 60

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 = 'N165YV' 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.

SDR 58572Propeller · stuckON POWER UP FOR TAKEOFF THE CREW NOTED THAT THE RIGHT PROP STUCK IN LOW PITCH. RETURNED TO GATE WITH NO FURTHER INCIDENT. MAINTENANCE CLEANED AND LUBED LOW PITCH SOLENOID. NO PARTS WERE USED.Feb 4, 2004 · N165YV · Beech 1900D · Propeller Controlling SystemSDR AMWA73Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, TO THE RIB FLANGES AT CANTED STAB STA 54.026 WERE FOUND CRACKED IN THREE PLACES ON THE LEFT AND THREE PLACES ON THE RIGHT. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE WITH BMM P/N 114-590021-9, 51-70-03.Nov 5, 2003 · N165YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA72Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE AT CANTED STAB STA 39.289 WAS FOUND CRACKED ONCE ON THE RIGHT SIDE. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE WITH BMM P/N 114-590021-9, 51-70-03.Nov 5, 2003 · N165YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA71Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGES AT CANTED STAB STA 69.184 WAS FOUND CRACKED, ONCE ON THE LEFT AND ONCE ON THE RIGHT SIDE. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE TO BMM P/N 114-590021-9, 51-70-03.Nov 5, 2003 · N165YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR 53080Flap · malfunctionedAFTER TAKEOFF FROM PANAMA CITY FLORIDA ON FLIGHT 5445, THE FLAPS WERE SELECTED UP, STAY AT 17 DEGREES. THE CREW DECIDED TO RETURN TO PANAMA CITY FLORIDA WITH NO FURTHER INCIDENT. THE FLAPS WERE RETRACTED TO ZERO AND MEL'D. THE AIRCRAFT WAS RETURNED TO SERVIJul 30, 2003 · N165YV · Beech 1900D · Trailing Edge Flap Control SystemSDR 049330Motor · failedON APPROACH TO KANSAS CITY, THE LANDING GEAR FAILED TO EXTEND. AFTER PERFORMING THE MANUL EXTENSION CHECK LIST THE GEAR WAS FOUND TO BE DOWN AND LOCKED. THE GEAR WAS PUMPED DOWN ALL THREE GREEN CAME ON. THE AIRCRAFT LANDED WITH NO FURTHER INCIDENT. MAINTENMar 31, 2003 · N165YV · Beech 1900D · Landing Gear Retraction/Extension SystemSDR 97ZZZX3232Attach Bracket · excess wearFLEET CAMPAIGN, 'MAINTENANCE INSPECTED THE LT AND RT OTBD FLAP ATTACHMENT BRACKETS AND THE AFT ROLLER BEARING IAW RAYTHEON ACFT CO (RAC) SAFETY COMMUNIQUE NR 137 DATED MAY, 1997. FOUND ATTACHMENT BRACKETS WITH EXCESSIVE WEAR AND AFT ROLLER BEARINGS BINDING. Jul 11, 1997 · N165YV · Beech 1900D · Trailing Edge FlapsSDR 97ZZZX3231Attach Bracket · excess wearFLEET CAMPAIGN, 'MAINTENANCE INSPECTED THE LT AND RT OTBD FLAP ATTACHMENT BRACKETS AND THE AFT ROLLER BEARING IAW RAYTHEON ACFT CO (RAC) SAFETY COMMUNIQUE NR 137 DATED MAY, 1997. FOUND ATTACHMENT BRACKETS WITH EXCESSIVE WEAR AND AFT ROLLER BEARINGS BINDING. Jul 11, 1997 · N165YV · Beech 1900D · Trailing Edge FlapsSDR MASA97037Bracket · wornFLT 5974 - PKB-CKB - ON FINAL APPROACH INTO CKB, THE FLAPS WERE DEPLOYED. THE RIGHT OUTBOARD FLAP BECAME DETACHED FROM THE FLAP AFT ROLLER BEARINGS AT THE OUTBOARD FLAP INBOARD FLAP TRACK. THE FLAP CAME IN CONTACT WITH THE AILERON INTERFERRING WITH AILERON CJun 20, 1997 · N165YV · Beech 1900D · Trailing Edge FlapsSDR 96ZZZX4777Vent Blower · failedCREW REPORTED A LIGHT HAZE IN CABIN AND FLT DK. RETURNED TO FIELD WITH NO FURTHER DIFFICULTIES. THE LIGHT HAZE DISSAPATED WHEN CREW DUMPED CABIN. UPON INITIAL INSPECTION, NO INDICATION OF SMOKE OR FLAMES OF ANY KIND WERE FOUND. ALL CIRCUIT BREAKERS WERE SEJul 26, 1996 · N165YV · Beech 1900D · Air Distribution Fan
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