# Service difficulty reports: N660CA A list on [N660CA](https://openairdocs.org/aircraft/N660CA.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR HYIA20191011002](https://openairdocs.org/sdr/HYIA20191011002.md): Beam · cracked · Oct 11, 2019 · N660CA · Cessna 402C · Nacelle/Pylon, Main Frame > DURING 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 - [SDR HYIA20180202001](https://openairdocs.org/sdr/HYIA20180202001.md): Bearing · fragmented · Feb 1, 2018 · N660CA · Cessna 402C · Engine Starter > PILOT 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. - [SDR HYIA20161108188](https://openairdocs.org/sdr/HYIA20161108188.md): Exhaust Valve · damaged · Oct 25, 2016 · N660CA · Cessna 402C · Reciprocating Engine Cylinder Section > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20160725001](https://openairdocs.org/sdr/HYIA20160725001.md): Selector Valve · malfunctioned · Jul 21, 2016 · N660CA · Cessna 402C · Fuel Selector/Shut-Off Valve > PILOT REPORTED ENGINE FAILURE WHEN LEANING MIXTURE. RESTARTED WITH RIGHT FUEL PUMP ON. MAINTENANCE TROUBLESHOT THE RIGHT FUEL SELECTOR VALVE. REPLACED FUEL SELECTOR VALVE. - [SDR HYIA20160712003](https://openairdocs.org/sdr/HYIA20160712003.md): Lifter · collapsed · Jul 3, 2016 · N660CA · Cessna 402C · Reciprocating Engine Cylinder Section > PILOT 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. - [SDR HYIA201608003016](https://openairdocs.org/sdr/HYIA201608003016.md): Exhaust Valve · damaged · Jun 28, 2016 · N660CA · Cessna 402C · Reciprocating Engine Cylinder Section > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA201608003015](https://openairdocs.org/sdr/HYIA201608003015.md): Exhaust Valve · damaged · Jun 27, 2016 · N660CA · Cessna 402C · Reciprocating Engine Cylinder Section > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA201608003014](https://openairdocs.org/sdr/HYIA201608003014.md): Exhaust Valve · damaged · Jun 27, 2016 · N660CA · Cessna 402C · Reciprocating Engine Cylinder Section > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA201608003013](https://openairdocs.org/sdr/HYIA201608003013.md): Exhaust Valve · damaged · Jun 27, 2016 · N660CA · Cessna 402C · Reciprocating Engine Cylinder Section > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE CRACKED AND DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20160104003](https://openairdocs.org/sdr/HYIA20160104003.md): Fuel Line · defective · Dec 31, 2015 · N660CA · Cessna 402C · Heating System > PILOT REPORTED STRONG SMELL OF GAS WHEN HEATER IS OPERATING. R & R HEATER FUEL LINE FROM HEATER FUEL PUMP TO HEATER. LEAK CHECKED GOOD. - [SDR HYIA20130320001](https://openairdocs.org/sdr/HYIA20130320001.md): Pump · malfunctioned · Mar 18, 2013 · N660CA · Cessna 402C · Engine Fuel Pump > FLIGHT 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 SHUTOF - [SDR HYIA20130124001](https://openairdocs.org/sdr/HYIA20130124001.md): Spar · cracked · Jan 24, 2013 · N660CA · Cessna 402C · Fuselage Main, Structure > DURING 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. - [SDR HYIA20140414019](https://openairdocs.org/sdr/HYIA20140414019.md): Drag Brace · cracked · Aug 30, 2012 · N660CA · Cessna 402C · Landing Gear Retraction/Extension System > AT 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 & A - [SDR HYIA20140415030](https://openairdocs.org/sdr/HYIA20140415030.md): Drag Brace · cracked · Feb 11, 2011 · N660CA · Cessna 402C · Landing Gear Retraction/Extension System > AT 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 O - [SDR HYIA20140415004](https://openairdocs.org/sdr/HYIA20140415004.md): Drag Brace · cracked · Jan 19, 2011 · N660CA · Cessna 402C · Landing Gear Retraction/Extension System > AT 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 O - [SDR HYIA660CADB2](https://openairdocs.org/sdr/HYIA660CADB2.md): Drag Brace · broken · May 22, 2010 · N660CA · Cessna 402C · Nose/Tail Landing Gear > DURING 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. - [SDR HYIA660CADRAGBRAC](https://openairdocs.org/sdr/HYIA660CADRAGBRAC.md): Drag Brace · broken · May 22, 2010 · N660CA · Cessna 402C · Nose/Tail Landing Gear > DURING 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. - [SDR HYIA660CA](https://openairdocs.org/sdr/HYIA660CA.md): Beam · cracked · Dec 17, 2008 · N660CA · Cessna 402C · Nacelle/Pylon, Main Frame > RIGHT ENGINE'S INBOARD ENGINE BEAM CRACKED AT AFT UPPER WEB. REMOVAL AND REPLACEMENT OF ENGINE BEAM. - [SDR 1350516N660CA](https://openairdocs.org/sdr/1350516N660CA.md): Circuit Breaker · defective · Jul 8, 2006 · N660CA · Cessna 402C · DC Power Distribution System > CREW REPORTED AVIONICS MASTER SWITCH INOP. MX CHANGED CIRCUIT BREAKER SWITCH. - [SDR HYI2001F00001](https://openairdocs.org/sdr/HYI2001F00001.md): Master Switch · failed · Oct 2, 2001 · N660CA · Cessna 402C · DC Power Distribution System > WHILE 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. - [SDR 95ZZZX3810](https://openairdocs.org/sdr/95ZZZX3810.md): Pump · defective · Jul 7, 1995 · N660CA · Cessna 402C · Fuel Boost Pump > DURING 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 ## 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 = 'N660CA' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N660CA/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.