# Service difficulty reports: N326CA A list on [N326CA](https://openairdocs.org/aircraft/N326CA.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR TIMA20171004014](https://openairdocs.org/sdr/TIMA20171004014.md): Powerpack · failed · Oct 4, 2017 · N326CA · Beech 99 · Hydraulic System, Main > LANDING 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. - [SDR TIMA20170926013](https://openairdocs.org/sdr/TIMA20170926013.md): Powerpack · failed · Sep 26, 2017 · N326CA · Beech 99 · Hydraulic System, Main > LANDING GEAR STARTED COMING DOWN IN FLIGHT, HAD TO MANUALLY PUMPED DOWN. FURTHER INVESTIGATION REVEALED THAT THE PROBLEM WAS WITH THE HYDRAULIC POWER PACK. - [SDR 2017F00167](https://openairdocs.org/sdr/2017F00167.md): Unknown · malfunctioned · Sep 26, 2017 · N326CA · Beech 99A · Landing Gear Retraction/Extension System > LANDING GEAR STARTED COMING DOWN IN FLIGHT, HAD TO MANUALLY PUMPED DOWN. TROUBLE SHOOTING UNDERWAY. - [SDR TIMA20170119001](https://openairdocs.org/sdr/TIMA20170119001.md): Actuator · defective · Jan 19, 2017 · N326CA · Beech 99A · Landing Gear Actuator > FOLLOWING 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. - [SDR TIMA20161108018](https://openairdocs.org/sdr/TIMA20161108018.md): Clevis · broken · Nov 8, 2016 · N326CA · Beech 99A · Landing Gear Actuator > DURING 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 - [SDR TIMA20140410010](https://openairdocs.org/sdr/TIMA20140410010.md): Rib · cracked · Apr 10, 2014 · N326CA · Beech 99A · Elevator, Spar/Rib > INSPECTION REVEALED 4 CRACKS IN THE LT ELEVATOR LE RIB. THE RIB WAS REPLACED WITH A NEW RIB. - [SDR TIMA20120501007](https://openairdocs.org/sdr/TIMA20120501007.md): Battery · leaking · May 1, 2012 · N326CA · Beech 99A · Battery/Charger System > DURING 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. - [SDR KGBR2011052501](https://openairdocs.org/sdr/KGBR2011052501.md): Skin Panel · cracked · May 25, 2011 · N326CA · Beech 99A · Trailing Edge Flaps > CRACK 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. - [SDR TIMA2010000016](https://openairdocs.org/sdr/TIMA2010000016.md): Spar · cracked · Aug 11, 2010 · N326CA · Beech 99A · Wing Spar > WING SPAR CRACKED IN UPPER AFT OTBD FITTING. - [SDR TIMR200600002](https://openairdocs.org/sdr/TIMR200600002.md): Fcu · malfunctioned · Jul 6, 2006 · N326CA · Beech 99A · Fuel Control/Turbine Engines > PILOT 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 FC - [SDR 2006FA0000631](https://openairdocs.org/sdr/2006FA0000631.md): Line · ruptured · Jun 2, 2006 · N326CA · Beech 99A · Hydraulic System, Main > DURING 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 - [SDR TIM2005F00009](https://openairdocs.org/sdr/TIM2005F00009.md): Fire Detector · false indication · Jul 29, 2005 · N326CA · Beech 99A · Fire Detection > THE 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. TH - [SDR 2005FA0000004](https://openairdocs.org/sdr/2005FA0000004.md): Inverter · malfunctioned · Nov 19, 2004 · N326CA · Beech 99A · Engine (Turbine/Turboprop) > ON 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 DRO - [SDR TIM2002F00015](https://openairdocs.org/sdr/TIM2002F00015.md): Attach Fitting · cracked · Sep 24, 2002 · N326CA · Beech 99A · Wing, Attach Fittings > CRACK 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) - [SDR TIM2002F00014](https://openairdocs.org/sdr/TIM2002F00014.md): Attach Fitting · cracked · Sep 24, 2002 · N326CA · Beech 99A · Wing, Attach Fittings > CRACK FOUND IN RIGHT WING, CENTER SECTION UPPER FORWARD ATTACH FITTING. - [SDR 2000ZZZX231](https://openairdocs.org/sdr/2000ZZZX231.md): Directional Gyro · broken · Dec 18, 1999 · N326CA · Beech 99A · Directional Gyro and Indicating System > DIRECTIONAL GYRO BECAME INOPERABLE. CHECK OF PITOT SYSTEM FOUND BROKEN CONNECTOR ON BACK OF GYRO. UPON REMOVAL OF GYRO, FOUND ALL THREE LINE CONNTIONS BROKEN. - [SDR 96ZZZX3559](https://openairdocs.org/sdr/96ZZZX3559.md): Latch Pin · binding · Jul 2, 1996 · N326CA · Beech 99A · Passenger/Crew Doors > KING 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 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/aircraft/N326CA/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.