N402VN

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 = 'N402VN' 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 HYIA20210712001Strap · corrodedDURING SID 57-10-16 INSPECTION, 3 AREAS OF CORROSION WERE IDENTIFIED ON THE RIGHT SPAR STRAP OF N402VN. THESE AREAS ARE LOCATED ON THE OUTBOARD END OF THE STRAP BETWEEN APPROXIMATE WING STATIONS, 145.87-155.62, AND ARE BEYOND LIMITS FOR REPAIR AS OUTLINED IN SJul 1, 2021 · N402VN · Cessna 402C · Wing Main, Frame StructureSDR HYIA20191112001Skin · delaminatedLEFT AILERON SKIN DE-LAMINATED IN FLIGHT. THE FLIGHT LANDED SAFELY WITH NO EMERGENCY ACTION. THE AILERON AND TRIM TAB WERE REPLACED WITH NO FURTHER DEFECTS NOTED.Nov 8, 2019 · N402VN · Cessna 402C · AileronsSDR HYIA20190315005Relay · stuckPILOT REPORTED ON START-UP THE LEFT ENGINE STARTER STUCK. MAINTENANCE INSPECTED AND FOUND THE STARTER RELAY STUCK IN THE CLOSED POSITION. THE STARTER RELAY WAS REPLACED WITH NO FURTHER DEFECTS NOTED.Mar 11, 2019 · N402VN · Cessna 402C · Engine StarterSDR HYIA20190315006Cylinder · damagedPILOT REPORTED RIGHT ENGINE SURGES, SHUTTERS AND VIBRATES ON ALL POWER SETTINGS. MAINTENANCE INSPECTED AND FOUND CYLINDER NR 4 WEAR IN EXHAUST VALVE KEEPER AREA, AS WELL AS INTAKE AND EXHAUST LIFTERS NOT WORKING PROPERLY. REMOVED AND REPLACED CYLINDER #4 AS WEMar 7, 2019 · N402VN · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20190307003Uplock Hook · brokenPILOT REPORTED THE LEFT MAIN GEAR WOULD NOT RETRACT. MAINTENANCE INSPECTED AND FOUND THE LEFT MAIN LANDING GEAR UPLOCK HOOK BROKEN. THE PART WAS REPLACED WITH NO FURTHER DEFECTS NOTED.Mar 1, 2019 · N402VN · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20180314001Blower · seizedPILOT REPORTED, HEATER GIVES A MELTING PLASTIC SMELL IN FLIGHT. MAINTENANCE INSPECTED AND FOUND THE HEATER COMBUSTION BLOWER HAD SEIZED, THE BLOWER WAS REPLACED WITH NO FURTHER DEFECTS NOTED.Mar 10, 2018 · N402VN · Cessna 402C · Heating SystemSDR HYIA20180215002Beam · crackedWHILE PERFORMING OTHER MAINTENANCE, A CRACK WAS DISCOVERED IN THE RT CANTED BEAM ASSEMBLY (CROSSOVER BEAM) ON THE AFT RIGHT HAND SIDE, AROUND ONE OF THE TURBO BRACKET MOUNTING HOLES. IT APPEARS THE CRACK WAS CAUSED BY PRE-LOADING OF THE TURBO BRACKET. BEAM ASFeb 13, 2018 · N402VN · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYIA20170719003Rib · crackedDURING A ROUTINE INSPECTION, SIX CRACKS WERE FOUND IN THE LT CLOSE OUT RIB (P/N 5122155-55.) THESE CRACKS WERE LOCATED AT EACH OF THE SIX VERTICAL ATTACHING HOLES OF THE FORWARD ROW OF THE AFT TRUNNION SUPPORT. EACH CRACK IS TWO INCHES IN LENGTH. UPON REMOVAJul 19, 2017 · N402VN · Cessna 402C · Wing, Rib/BulkheadSDR HYIA20170719002Rib · crackedDURING A ROUTINE INSPECTION, A CRACK (.250 IN LENGTH) WAS FOUND IN THE RT CLOSE OUT RIB (P/N 5122155-56.) THIS CRACK WAS FOUND IN THE FORWARD LOWER MOST HOLE OF THE FORWARD TRUNNION SUPPORT. UPON REMOVAL, ALL FASTENERS HOLES WERE FOUND TO BE WITHIN TOLERANCE Jul 19, 2017 · N402VN · Cessna 402C · Wing, Rib/BulkheadSDR HYIA2014040400001Pedal · failedRIGHT RUDDER PEDAL ON GROUND. R & R RUDDER PEDAL.Feb 27, 2014 · N402VN · Cessna 402C · Rudder Control SystemSDR HYIA20140414036Drag 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 & ANov 29, 2012 · N402VN · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415076Drag 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 WITHIN ALLOWABLE LIMIT OF MEB91-11R1. THIS UNIT HAS BEEN REPAIRED IAWJan 19, 2012 · N402VN · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA402VNSMOKEDimmer · failedTHE PILOT REPORTED THAT ON APPROACH, THEY TURNED ON THE INSTRUMENT PANEL LIGHTS. SHORTLY AFTER TURNING THE PANEL LIGHTS ON, THEY SMELLED AN ELECTRICAL BURNING SMELL AND NOTICED A SMALL AMOUNT OF SMOKE COMING OUT OF THE RT RHEOSTAT. THEY IMMEDIATELY TURNED THE Aug 25, 2011 · N402VN · Cessna 402C · Instrument PanelSDR HYIA20140414004Drag 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 & AApr 14, 2011 · N402VN · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA402VNRTRUNNBarrel · unserviceableCREW REPORTED, RT MAIN GEAR SHEARED OFF ON LANDING ROLL. MX FOUND RT MAIN GEAR UPPER BARREL AND TRUNNION ASSY SHEARED JUST BELOW MLG ACTUATOR ATTACH POINT. MX IS IN THE PROCESS OF REPLACING RT MLG ASSY, RT ENGINE, RT PROPELLER, RT SIDE INBD AND OTBD FLAP PANEJul 27, 2010 · N402VN · Cessna 402C · Main Landing Gear Strut/Axle/TruckSDR HYI2003F00019Seal · unserviceableDURING FLIGHT, CREW NOTICED FUEL ESCAPING FROM RT UPPER ACCESS PANEL. ENGINES RUNNING NORMAL, EMERGENCY WAS DECLARED, LANDED WITHOUT INCIDENT. MECHANIC REMOVED AND REPLACED PANEL SEALS AND RELEASED AIRCRAFT BACK TO SERVICE.Nov 7, 2003 · N402VN · Cessna 402C · Wing, Plate/SkinSDR HYI2002F00001Drag Brace · crackedAT REGULAR SCHEDULED INSPECTION, MECHANIC FOUND NOSE GEAR, DRAG BRACE CRACKED AT ACTUATOR ATTACH HOUSING. REMOVED AND REPLACED DRAG BRACE AND RETURNED AIRCRAFT TO SERVICE.Feb 25, 2002 · N402VN · Cessna 402C · Nose/Tail Landing Gear Strut/Axle
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