N660CA

Service difficulty reports · 21

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 = 'N660CA' 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 HYIA20191011002Beam · crackedDURING ULTRASONIC INSPECTION PERFORMED IAW AAS-ALS-15-002 REV. B PART 2 PAGES 1-13 IAW AMOC TO SATISFY AD 2015-07-03, A CRACK WAS IDENTIFIED ON THE TOP FACE OF THE RIGHT HAND OUTBOARD ENGINE BEAM. THIS CRACK WAS MEASURED AT .125" LONG AND IS TRAVELLING ACROSS Oct 11, 2019 · N660CA · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYIA20180202001Bearing · fragmentedPILOT REPORTED THE LEFT ENGINE HAD LOW OIL PRESSURE, BELOW GREEN ARC AT 1700 RPM. DEBRIS WAS FOUND IN THE OIL FILTER, FURTHER INSPECTION DISCOVERED THE STARTER ADAPTER SHAFT NEEDLE BEARING TO BE SEVERELY DAMAGED. THE ENGINE WAS REPLACED.Feb 1, 2018 · N660CA · Cessna 402C · Engine StarterSDR HYIA20161108188Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Oct 25, 2016 · N660CA · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20160725001Selector Valve · malfunctionedPILOT REPORTED ENGINE FAILURE WHEN LEANING MIXTURE. RESTARTED WITH RIGHT FUEL PUMP ON. MAINTENANCE TROUBLESHOT THE RIGHT FUEL SELECTOR VALVE. REPLACED FUEL SELECTOR VALVE.Jul 21, 2016 · N660CA · Cessna 402C · Fuel Selector/Shut-Off ValveSDR HYIA20160712003Lifter · collapsedPILOT REPORTED THE RIGHT ENGINE WAS VIBRATING AND SURGING ABOVE 30 INCHES OF MANIFOLD PRESSURE. MAINTENANCE INVESTIGATED, CLEANED THE RIGHT ENGINE FUEL NOZZLES, AND REPLACED THE RIGHT ENGINE NR 6 CYLINDER EXHAUST LIFTER DUE TO IMMOBILITY.Jul 3, 2016 · N660CA · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA201608003016Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Jun 28, 2016 · N660CA · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA201608003015Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Jun 27, 2016 · N660CA · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA201608003014Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Jun 27, 2016 · N660CA · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA201608003013Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE CRACKED AND DISPLAYS EVIDENCE OF HEAT DAMAGE.Jun 27, 2016 · N660CA · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20160104003Fuel Line · defectivePILOT REPORTED STRONG SMELL OF GAS WHEN HEATER IS OPERATING. R & R HEATER FUEL LINE FROM HEATER FUEL PUMP TO HEATER. LEAK CHECKED GOOD.Dec 31, 2015 · N660CA · Cessna 402C · Heating SystemSDR HYIA20130320001Pump · malfunctionedFLIGHT CREW REPORTED THAT PRIOR TO TAKEOFF ALL INDICATIONS WERE NORMAL. SHORTLY AFTER TAKEOFF WHILE CLIMBING, THE CREW REPORTED THAT THE RT ENGINE SURGED AND THEN BEGAN TO LOSE POWER, AT WHICH POINT THE CREW NOTICED A SPIKE IN FUEL FLOW (295 PPH). CREW SHUTOFMar 18, 2013 · N660CA · Cessna 402C · Engine Fuel PumpSDR HYIA20130124001Spar · crackedDURING A SCHEDULED MX EVENT, CRACKS WERE DISCOVERED ON THE REAR SPAR WEBS FORWARD AND AFT AT FLOOR ATTACH POINTS. DAMAGE WAS MAPPED AND SENT. REPAIRS WERE CARRIED OUT IAW REPAIR PLANS SUPPLIED AND SUBSTANTIATED.Jan 24, 2013 · N660CA · Cessna 402C · Fuselage Main, StructureSDR HYIA20140414019Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5, WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & AAug 30, 2012 · N660CA · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415030Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE OEM PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OFeb 11, 2011 · N660CA · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415004Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE OEM PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OJan 19, 2011 · N660CA · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA660CADB2Drag Brace · brokenDURING LANDING ROLLOUT, NOSE GEAR COLLAPSED. ALL INDICATIONS WERE NORMAL. MX FOUND NOSE GEAR DRAG BRACE BROKEN AT ACTUATOR ATTACH POINT. MX PERFORMED TEMPORARY REPAIRS, REPLACED PROPELLERS, FERRIED ACFT BOS FOR PERMENANT REPAIRS.May 22, 2010 · N660CA · Cessna 402C · Nose/Tail Landing GearSDR HYIA660CADRAGBRACDrag Brace · brokenDURING LANDING ROLLOUT, NOSE GEAR COLLAPSED. ALL INDICATIONS WERE NORMAL. MX FOUND NOSE GEAR DRAG BRACE BROKEN AT ACTUATOR ATTACH POINT. MX PERFORMED TEMPORARY REPAIRS, REPLACED PROPELLERS, FERRIED ACFT BOS FOR PERMENANT REPAIRS.May 22, 2010 · N660CA · Cessna 402C · Nose/Tail Landing GearSDR HYIA660CABeam · crackedRIGHT ENGINE'S INBOARD ENGINE BEAM CRACKED AT AFT UPPER WEB . REMOVAL AND REPLACEMENT OF ENGINE BEAM.Dec 17, 2008 · N660CA · Cessna 402C · Nacelle/Pylon, Main FrameSDR 1350516N660CACircuit Breaker · defectiveCREW REPORTED AVIONICS MASTER SWITCH INOP. MX CHANGED CIRCUIT BREAKER SWITCH.Jul 8, 2006 · N660CA · Cessna 402C · DC Power Distribution SystemSDR HYI2001F00001Master Switch · failedWHILE AIRCRAFT WAS TAXING, AVIONICS SYSTEM FAILED. CREW ENGAGED EMERGENCY AVIONICS BY PASS SWITCH, AND RETURNED TO THE GATE. MECHANICS REMOVED AND REPLACED AVIONICS MASTER SWITCH AND RELEASE AIRCRAFT BACK TO SERVICE.Oct 2, 2001 · N660CA · Cessna 402C · DC Power Distribution SystemSDR 95ZZZX3810Pump · defectiveDURING CRUISE FLIGHT, PLACED RIGHT FUEL SELECTOR TO LEFT MAIN FUEL TANK, BOTH RIGHT AND LEFT ENGINES SHOWED SIGNS OF FUEL STARVATION (ENGINES SURGING). PUT LEFT FUEL BOOST PUMP ON LOW AND WAS OK. FOUND LEFT AUXILIARY BOOST PUMP INLET CHECK BALL STUCK ON SEAT Jul 7, 1995 · N660CA · Cessna 402C · Fuel Boost Pump
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