N326CA

Service difficulty reports · 17

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 = 'N326CA' 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 TIMA20171004014Powerpack · failedLANDING GEAR DID NOT EXTEND WHEN SELECTED. PUMPED GEAR DOWN MANUALLY. LANDED WITHOUT INCIDENT. FURTHER INVESTIGATION REVEALED THAT THE PROBLEM WAS WITH THE HYDRAULIC POWER PACK.Oct 4, 2017 · N326CA · Beech 99 · Hydraulic System, MainSDR TIMA20170926013Powerpack · failedLANDING GEAR STARTED COMING DOWN IN FLIGHT, HAD TO MANUALLY PUMPED DOWN. FURTHER INVESTIGATION REVEALED THAT THE PROBLEM WAS WITH THE HYDRAULIC POWER PACK.Sep 26, 2017 · N326CA · Beech 99 · Hydraulic System, MainSDR 2017F00167Unknown · malfunctionedLANDING GEAR STARTED COMING DOWN IN FLIGHT, HAD TO MANUALLY PUMPED DOWN. TROUBLE SHOOTING UNDERWAY.Sep 26, 2017 · N326CA · Beech 99A · Landing Gear Retraction/Extension SystemSDR TIMA20170119001Actuator · defectiveFOLLOWING GEAR RETRACTION AFTER TAKEOFF THE PILOT HEARD A LOUD THUD. THE LEFT GEAR LIGHT SHOWED GREEN & THE NOSE AND RT GEAR INDICATORS SHOWED UNSAFE. THIS WAS CONFIRMED BY A RED LIGHT IN GEAR HANDLE. THE EMERGENCY GEAR EXTENSION CHECKLIST WAS ACCOMPLISHED.Jan 19, 2017 · N326CA · Beech 99A · Landing Gear ActuatorSDR TIMA20161108018Clevis · brokenDURING TAKEOFF, THE LANDING GEAR WERE RETRACTED. A FEW SECONDS LATER A LOUD THUD OCCURRED FOLLOWED BY THE RT GEAR GREEN LIGHT ILLUMINATED. THE RED "GEAR UNSAFE" LIGHT IN THE HANDLE WAS NOT ILLUMINATED. PRIOR TO LANDING, GEAR WERE SELECTED “DOWN”. ALL THREE Nov 8, 2016 · N326CA · Beech 99A · Landing Gear ActuatorSDR TIMA20140410010Rib · crackedINSPECTION REVEALED 4 CRACKS IN THE LT ELEVATOR LE RIB. THE RIB WAS REPLACED WITH A NEW RIB.Apr 10, 2014 · N326CA · Beech 99A · Elevator, Spar/RibSDR TIMA20120501007Battery · leakingDURING ENGINE START ALL ELECTRICAL POWER FAILED. CAUSE WAS FOUND TO BE ACID LEAK THROUGH AT THE NEGATIVE POST OF THE AIRCRAFT LEAD ACID BATTERY WHICH CAUSED CORROSION OF THE CONNECTOR.May 1, 2012 · N326CA · Beech 99A · Battery/Charger SystemSDR KGBR2011052501Skin Panel · crackedCRACK ON SKIN PANEL AT THE ATTACHMENT BRACKET AT 18 INCHES OUTBOARD OF THE INBOARD EDGE OF THE FLAP ASSEMBLY. ALSO 2 CRACKS ON THE SPAR WEB AT 10 INCHES AND 11 INCHES OUTBOARD OF THE INBOARD EDGE OF THE FLAP.May 25, 2011 · N326CA · Beech 99A · Trailing Edge FlapsSDR TIMA2010000016Spar · crackedWING SPAR CRACKED IN UPPER AFT OTBD FITTING.Aug 11, 2010 · N326CA · Beech 99A · Wing SparSDR TIMR200600002Fcu · malfunctionedPILOT NOTICED THAT THE LT TORQUE INDICATION SLOWLY AND CONTINUALLY DECREASED. WHEN POWER ADJUSTMENTS PRODUCED NO EFFECT AND ADVERSE YAW CONFIRMED POWER LOSS THE PILOT FEATHERED THE PROP AND SHUTDOWN THE ENGINE. SUBSEQUENT INVESTIGATION DETERMINED THAT THE FCJul 6, 2006 · N326CA · Beech 99A · Fuel Control/Turbine EnginesSDR 2006FA0000631Line · rupturedDURING CLIMBOUT THE (GEAR IN TRANSIT) AND (DO NOT REVERSE) ANNUNCICATOR ILLUMINATED AND THEN THE LANDING GEAR CIRCUIT BREAKER POPPED. PILOT CONTINUED, HAND PUMPED THE GEAR TO GET 3 GREEN. LANDED OK. INVESTIGATION DETERMINED THAT HYDRAULIC HOSE ON THE LT UP Jun 2, 2006 · N326CA · Beech 99A · Hydraulic System, MainSDR TIM2005F00009Fire Detector · false indicationTHE RT ENGINE FIRE DETECTION LIGHT CAME ON BRIEFLY ON FINAL APPROACH TO THE AIRPORT. THE RT ENGINE WAS RECENTLY CHANGED AND WAS WASHED TO CHECK FOR POSSIBLE OIL LEAKS. WATER FROM THE WASH CAN ENTER THE ENGINE FIRE DETECTORS AND CAUSE FALSE FIRE WARNINGS. THJul 29, 2005 · N326CA · Beech 99A · Fire DetectionSDR 2005FA0000004Inverter · malfunctionedON CLIMB OUT, RT ENGINE TORQUE DROPPED TO 500. AC RETURNED, WHERE THE TORQUE SYSTEM WAS JET CAL, GAUGES SWAPPED SIDE TO SIDE AND ALL SYSTEMS WORKED AS REQUIRED. MAINTENANCE SUSPECTS AN ELECTRICAL SPIKE FROM THE NR 1 INVERTER. THE GAUGES STUCK ON 500 BUT DRONov 19, 2004 · N326CA · Beech 99A · Engine (Turbine/Turboprop)SDR TIM2002F00015Attach Fitting · crackedCRACK FOUND IN RT WING ATTACH FITTING. (BATH TUB FITTINGS) LOCATION CENTER SECTION UPPER FORWARD ATTACH FITTING. RECURRING INSPECTION INTERVAL (SUPER SPAR) 1000 HOURS OR 3 YEARS WHICHEVER OCCURS FIRST. (CONTROL NUMBER 004)Sep 24, 2002 · N326CA · Beech 99A · Wing, Attach FittingsSDR TIM2002F00014Attach Fitting · crackedCRACK FOUND IN RIGHT WING, CENTER SECTION UPPER FORWARD ATTACH FITTING.Sep 24, 2002 · N326CA · Beech 99A · Wing, Attach FittingsSDR 2000ZZZX231Directional Gyro · brokenDIRECTIONAL GYRO BECAME INOPERABLE. CHECK OF PITOT SYSTEM FOUND BROKEN CONNECTOR ON BACK OF GYRO. UPON REMOVAL OF GYRO, FOUND ALL THREE LINE CONNTIONS BROKEN.Dec 18, 1999 · N326CA · Beech 99A · Directional Gyro and Indicating SystemSDR 96ZZZX3559Latch Pin · bindingKING CARGO SYSTEMS COCKPIT CREW DOOR, STC SA1438GL. PILOT HAD DIFFICULTY LATCHING DOOR. TOOK OFF, DOOR CAME OPEN DURING CLIMB. AIRCRAFT LANDED WITHOUT INCIDENT. EXAMINATION FOUND LATCH PINS BINDING IN GUIDES; LUBRICATED AND INSTALLED LIGHT SPRINGS TO HOLD Jul 2, 1996 · N326CA · Beech 99A · Passenger/Crew Doors
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