Cessna 402C

Service difficulty reports · 1,782

Newest first. General aviation reporting is voluntary.

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 aircraft_model_key = '402C'
  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 HYIA20170221001Pump · leakingTHE PILOT REPORTED HEATER FAILED IN FLIGHT, MAY WORK ON THE GROUND. ADDITIONALLY INDICATED AN ODOR OF GAS ON CLIMB OUT. MAINTENANCE INSPECTED THE HEATER AND FOUND THE HEATER FUEL PUMP LEAKING. REMOVED AND REPLACED THE HEATER FUEL PUMP. AFTER CONDUCTING AN OPFeb 20, 2017 · N548GA · Cessna 402C · Heating SystemSDR HYIA20170208002Valve Guide · damagedPILOT REPORTED ENGINE MANIFOLD PRESSURE ERRATIC DURING TAKE OFF ROLL. MAINTENANCE INSPECTED AND FOUND THE EXHAUST VALVE GUIDE ON THE NR 5 CYLINDER DAMAGED.Feb 7, 2017 · N300SN · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20170208001Valve Guide · damagedPILOT REPORTED RIGHT ENGINE SURGE 1 INCH MANIFOLD PRESSURE DURING TAKE OFF POWER USE. MAINTENANCE INSPECTED AND REPLACED THE NR 3 CYLINDER ASSEMBLY, AS WELL AS THE NR 1 & NR 3 CYLINDER EXHAUST AND INTAKE HYDRAULIC LIFTERS. FURTHER DISASSEMBLY OF THE CYLINDER AFeb 2, 2017 · N160PB · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20170203001Beam · crackedTHE RIGHT NACELLE CROSSOVER BEAM ASSEMBLY WAS FOUND TO BE CRACKED AT AFT FACE IN THE AREA OF TURBOCHARGER MOUNT BRACKET HOLE LOCATIONS DURING DURING DISASSEMBLY OF TURBO CHARGER ASSEMBLY TO FACILITATE OTHER MAINTENANCE. CRACK LOCATED ADJACENT TO OB MOST TURBOCFeb 1, 2017 · N57PB · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYIA20170124002Exhaust Valve · burnedPILOT REPORTED THE LEFT ENGINE RUNNING ROUGH, AND CHT SHOWING 175 ON LEFT ENGINE. MAINTENANCE INSPECTED AND FOUND THE LEFT ENGINE CYLINDER NR 3 EXHAUST VALVE BURNT AND THE NR 4 CYLINDER EXHAUST VALVE BROKEN; BOTH CYLINDERS HAS A TOTAL TIME IN SERVICE OF 1382.Jan 20, 2017 · N747WS · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20170124001Exhaust Valve · burnedPILOT REPORTED THE LEFT ENGINE RUNNING ROUGH, AND CHT SHOWING 175 ON LEFT ENGINE. MAINTENANCE INSPECTED AND FOUND THE LEFT ENGINE CYLINDER NR 3 EXHAUST VALVE BURNED AND THE NR 4 CYLINDER EXHAUST VALVE BROKEN. BOTH CYLINDERS WERE REPLACED WITH NO FURTHER ISSUJan 20, 2017 · N747WS · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20170828004Fitting · crackedDURING A ROUTINE INSPECTION, A CRACK WAS DISCOVERED ON THE RT OUTBOARD NACELLE FITTING. THE CRACK WAS FOUND ON THE INBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THE CRACK MEASURED .171 IN LENGTH.Jan 12, 2017 · N258PB · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYIA20170828003Fitting · crackedDURING A ROUTINE INSPECTION, A CRACK WAS DISCOVERED ON THE LT OUTBOARD NACELLE FITTING THE CRACK WAS DISCOVERED ON THE INBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THE CRACK WAS .108 IN LENGTH.Jan 12, 2017 · N258PB · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYIA20170828007Fitting · crackedDURING A ROUTINE INSPECTION, THREE CRACKS WERE FOUND ON THE RT OUTBOARD NACELLE FITTING. TWO OF THE CRACKS WERE FOUND ON THE INBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. MEASURED .050 AND .090 IN LENGTH. THE THIRD CRACK WAS FOUND ON THE OUTBOAJan 9, 2017 · N1376G · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20170828017Fitting · crackedDURING A ROUTINE INSPECTION, TWO CRACKS WERE FOUND IN THE RT OUTBOARD NACELLE FITTING. THESE CRACKS WERE FOUND ON THE INBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THEY MEASURED .119 AND .146 IN LENGTH.Jan 4, 2017 · N514NC · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20170828015Fitting · crackedDURING A ROUTINE INSPECTION, A CRACK WAS FOUND IN THE RT INBOARD NACELLE FITTING. THE CRACK WAS FOUND ON THE INBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THE CRACK MEASURED .049 IN LENGTH.Jan 4, 2017 · N991AA · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20161229001Manifold · low pressurePILOT REPORTED THAT DURING FLIGHT, MANIFOLD PRESSURE DROPPED EIGHT INCHES FROM 29-21. LANDED WITH NO INCIDENT. OPEN.Dec 28, 2016 · N499CA · Cessna 402C · Engine (Reciprocating)SDR 2017F00014Line · failedDURING LANDING, NOTED THAT RIGHT HAND BRAKES WERE UNRESPONSIVE. SLOWED AIRCRAFT AS BEST AS POSSIBLE AND ROLLED OFF END OF RUNWAY INTO A GRASS FIELD. AIRCRAFT SUSTAINED DAMAGE TO FUSELAGE AND LANDING GEAR.Dec 27, 2016 · N402R · Cessna 402C · Landing Gear Brake SystemSDR HYIA20170828012Fitting · crackedDURING A ROUTINE INSPECTION, THREE CRACKS WERE FOUND IN THE RT OUTBOARD NACELLE FITTING. TWO CRACKS WERE FOUND ON THE INBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THEY MEASURED .161 AND .088 IN LENGTH. THE THIRD CRACK WAS FOUND ON THE OUTBOARDec 26, 2016 · N818AN · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20170828014Fitting · crackedDURING A ROUTINE INSPECTION, A CRACK WAS DISCOVERED IN THE LT INBOARD NACELLE FITTING. THE CRACK WAS DISCOVERED ON THE OUTBOARD SIDE, JUST FORWARD OF THE SPAR STRAP. CRACK LENGTH IS .117.Dec 23, 2016 · N160PB · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20161223001Unknown · odorPILOT REPORTED AN ELECTRICAL BURNING ODOR IN COCKPIT AFTER TAKE OFF. MAINTENANCE INSPECTED ALL ELECTRICAL COMPONENTS AND BREAKERS & RAN THE HEATER WITH NO EVIDENCE OF BURNING ELECTRICAL SMELL. AIRCRAFT WAS RETURNED TO SERVICE.Dec 21, 2016 · N706CA · Cessna 402C · Air Distribution SystemSDR HYIA20170822001Rib · crackedDURING A ROUTINE INSPECTION, A CRACK WAS LOCATED AT RIB AT RT WS 106.79. THE CRACK ORIGINATED FROM A LOCK FASTENER. REPAIRED IAW MAINTENANCE MANUAL.Dec 16, 2016 · N7037E · Cessna 402C · Wing StructureSDR HYIA20161212001Motor · burned outTHE PILOT REPORTED "BURNING ODOR WHEN CABIN HEATING SYSTEM IN USE DURING FLIGHT AND BLOWER NOT BLOWING ON GROUND." AFTER INSPECTING, MAINTENANCE FOUND THE HEATER BLOWER MOTOR BURNED OUT. THE HEATER BLOWER WAS REMOVED AND REPLACED AND OPS CHECKED GOOD.Dec 9, 2016 · N991AA · Cessna 402C · Heating SystemSDR HYIA20161209001Gasket · leakingPILOT REPORTED FUEL ODOR IN CABIN WITH HEATER TURNED ON. MAINTENANCE REPLACED THE HEATER FUEL FILTER BOWL GASKET. FURTHER DETAILS ABOUT THE CONDITION OF THE GASKET WILL BE ADDED ONCE THE MECHANIC WHO REPLACED THE GASKET IS BACK TO WORK.Dec 8, 2016 · N2615G · Cessna 402C · Heating SystemSDR HYIA12062016002Fitting · crackedDURING A ROUTINE INSPECTION, CRACKS WERE IDENTIFIED AT RT OB NACELLE FITTING P/N 5292029-10. JUST FWD OF LWR FWD WING SPAR STRAP (REFERENCE MEB02-5 CURRENTLY AT REVISION 2 AND SERVICE KIT SK402-47A/B). THE MAJORITY OF THIS NACELLE FITTING IS NOT ACCESSIBLE FODec 5, 2016 · N6875D · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA12062016001Fitting · brokenDURING A ROUTINE INSPECTION, A CRACK WAS IDENTIFIED AT RT IB ENGINE BEAM ASSEMBLY P/N 5654109-7 AND THE BEAM WAS REMOVED. AT REMOVAL, THE RT NACELLE IB FITTING P/N 5292029-12 WAS FOUND TO BE BROKEN IN HALF JUST FWD OF LWR FWD WING SPAR STRAP (REFERENCE MEB02-5Dec 5, 2016 · N6875D · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20161205001Exhaust Valve · failedPILOT REPORTED "LEFT ENGINE RUNNING ROUGH AND WON'T IDLE BELOW 500 RPM". UPON INSPECTION MAINTENANCE FOUND THE NR 5 CYLINDER WAS READING ZERO COMPRESSION DUE TO AN EXHAUST VALVE CRACKED IN HALF. MAINTENANCE REPLACED THE CYLINDER AND PISTON ASSEMBLY WITH NO FURDec 1, 2016 · N401TJ · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20161121001Display · failedPILOT REPORTED A BURNING SMELL IN CABIN, AND RADAR WENT OFF. THE CABIN CIRCUIT BREAKER WAS THEN PULLED. MAINTENANCE INSPECTED AND REPLACED THE WEATHER RADAR DISPLAY WITH NO FURTHER DEFECTS NOTED.Nov 18, 2016 · N764EA · Cessna 402C · Weather Radar SystemSDR HYIA20161109209Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Nov 7, 2016 · N375R · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20161109208Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Nov 7, 2016 · N1361G · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20161109207Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Nov 6, 2016 · N678JG · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20161109206Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Nov 6, 2016 · N247GS · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20161109205Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Nov 6, 2016 · N247GS · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20161109203Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Nov 5, 2016 · N121PB · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20161109201Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Nov 5, 2016 · N6879R · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20161109204Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Nov 4, 2016 · N4630N · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20161109202Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Nov 3, 2016 · N751CA · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20161109200Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Nov 3, 2016 · N706CA · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20161109199Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Nov 3, 2016 · N706CA · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20161109198Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Nov 3, 2016 · N706CA · Cessna 402C · Reciprocating Engine Cylinder SectionSDR 8PCR20161103001Coil · fracturedDURING EXAMINATION OF ENGINE CORE FOR OVERHAUL, THE NR 5 CYLINDER EXHAUST VALVE ROTOCOIL WAS FOUND TO BE FRACTURED. THE TOP CIRCUMFERENCE OF THE ROTOCOIL STRUCTURE HAD FRACTURED FROM THE ROTOCOIL ASSEMBLY AND REMAINED CAPTURED BY THE EXHAUST ROCKER ARM WHERE Nov 3, 2016 · N991AA · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20161109197Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Nov 2, 2016 · N402HG · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20161109196Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Nov 2, 2016 · N1376G · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20161108195Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Oct 31, 2016 · N663AA · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20161108194Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Oct 30, 2016 · N4652N · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20161108193Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Oct 30, 2016 · N4652N · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20161108192Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Oct 30, 2016 · N69SC · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20161108191Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Oct 30, 2016 · N256CA · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20161108190Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Oct 30, 2016 · N1055 · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20161108189Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Oct 29, 2016 · N300SN · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20161102001Torque Tube · brokenPILOT REPORTED THE BRAKES FAILED PRIOR TO DEPARTURE. DURING INSPECTION, MAINTENANCE FOUND THE BRAKE PEDAL TORQUE TUBE CRACKED & BROKEN, REMOVED AND REPLACED TORQUE TUBE ASSEMBLY. NO FURTHER DEFECTS WERE NOTED.Oct 27, 2016 · N401TJ · Cessna 402C · Landing Gear Brake SystemSDR HYIA20161028001Spark Plug · failedPILOT REPORTED THE LEFT ENGINE WOULD NOT DEVELOP FULL POWER, STOPPED AT 26 INCHES MAP AND VIBRATION. INSPECTION OF THE LEFT ENGINE REVEALED A PREIGNITION EVENT IN THE NR 3 CYLINDER WHICH CAUSED SIGNIFICANT DAMAGE TO THE PISTON HEAD. THE CYLINDER IS IN THE PROOct 26, 2016 · N409BK · Cessna 402C · Spark Plug/IgniterSDR 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 HYIA20161108187Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Oct 24, 2016 · N524CA · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20161108186Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Oct 24, 2016 · N524CA · Cessna 402C · Reciprocating Engine Cylinder Section
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