N68391

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 = 'N68391' 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 HYIA20240426001Fitting · crackedDURING MAINTENANCE A CRACK WAS IDENTIFIED ON THE OUTBOARD LEG OF THE RIGHT HAND INBOARD NACELLE FITTING, (P/N: 5292029-22) THIS CRACK MEASURES APPROXIMATELY .100 INCHES LONG AND WAS DISCOVERED USING THE LIGHTED BORESCOPE INSPECTION PROCEDURE AS OUTLINED IN TEXApr 25, 2024 · N68391 · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYIA20210525002Cylinder · damagedTHE PILOT REPORTED ENGINE SURGING AND MANIFOLD PRESSURE DROP IN FLIGHT, AND THEN SHUT DOWN ENGINE IN-FLIGHT ACCORDING TO THE QRH. DURING THE INITIAL INSPECTION, FOUND SHINY PARTICLES IN THE OIL FILTER, AND SPARK PLUG DAMAGED, AND PARTICLES IN THE PROPELLER GOMay 20, 2021 · N68391 · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20190307001Door Frame · corrodedWHILE CONDUCTING OTHER MAINTENANCE, AN AREA OF CORROSION WAS NOTED ON THE FUSELAGE FRAME ASSEMBLY AT FS 214.00, JUST ABOVE THE 501110-12 STRIKER PLATE FOR THE LOWER PASSENGER DOOR PIN. THE 501110-12 STRIKER PLATE WAS REMOVED FOR FURTHER INSPECTION. UPON REMOVAMar 6, 2019 · N68391 · Cessna 402C · Fuselage Main, StructureSDR HYIA20180803002Engine · making metalPILOT REPORTED LT ENGINE HAD PARTIAL POWER, THEN NOTICED OIL COMING FORM COWLING UNDER THE TURBO. MAINTENANCE INSPECTED AND FOUND METAL CONTAMINATION IN ENGINE OIL FILTER AND THE #5 CYLINDER SHOWING SIGNS OF PRE-IGNITION. THE ENGINE IS TO BE REPLACED.Aug 2, 2018 · N68391 · Cessna 402C · Powerplant SystemSDR HYIA20180803001Cylinder · damagedPILOT REPORTED THE LEFT ENGINE STARTED TO RUN ROUGH DURING FLIGHT AND THE OIL PRESSURE SLOWLY DROPPED. AFTER LANDING, THE CREW REPORTED OIL DRIPPING OFF THE COWL. MAINTENANCE INSPECTED AND FOUND METAL CONTAMINATION IN ENGINE OIL SYSTEM AND THE NR 5 CYLINDER Jul 31, 2018 · N68391 · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20170602001Cable · brokenPILOT REPORTED ON LOWERING THE FLAPS AFTER THE FIFTEEN DEGREE POINT, HEARD A LOUD SNAP/BANG AND THE PLANE ABRUPTLY ROLLED TO THE RIGHT FOR A SPLIT SECOND BUT THEN STRAIGHTENED OUT. LANDED AS SOON AS POSSIBLE. MAINTENANCE INSPECTED AND FOUND THAT THE UPPER RT FMay 31, 2017 · N68391 · Cessna 402C · Trailing Edge Flap Control SystemSDR HYIA20170503002Unknown · odorPILOT REPORTED A BURNING ODOR IN THE CABIN WITH THE HEATER ON, AFTER LANDING NOTICED CABIN VENT FAN CIRCUIT BREAKER TRIPPED. OPENMay 2, 2017 · N68391 · Cessna 402C · Air Distribution SystemSDR HYIA20140414021Drag 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 & ASep 18, 2012 · N68391 · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415069Drag 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 IAWJul 29, 2011 · N68391 · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415068Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE 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 IAW PROCEDURE OUTLJul 29, 2011 · N68391 · Cessna 402C · Main Landing GearSDR HYIA20140415035Drag 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 OMar 11, 2011 · N68391 · Cessna 402C · Landing Gear Retraction/Extension SystemSDR 135N683910516Circuit Breaker · failedCREW REPORTED AVIONICS MASTER SWITCH INOP. MX CHANGED CIRCUIT BREAKER.Jun 15, 2006 · N68391 · Cessna 402C · DC Power Distribution SystemSDR HYI2003F00002Line · chafedCREW FOUND LT ENGINE OIL LEAK ON PORT FLIGHT INSPECTION. MECHANIC FOUND INTAKE BALANCE TUBE FLEX HOSE DATA TAG CHAFING ON OIL PAN. MECHANIC REMOVED AND REPLACED OIL PAN AND FLEX HOSE AND RETURNED AIRCRAFT TO SERVICE. FLEX LINE LENGTH WAS SHORTENED BY MANUFADec 10, 2002 · N68391 · Cessna 402C · Reciprocating Engine Oil SystemSDR HYI2002F00007Master Switch · failedON PRE-FLIGHT INSPECTION AVIONICS MASTER SWITCH FAILED. MAINTENANCE REPLACED SWITCH AND RETURNED AIRCRAFT TO SERVICE.Oct 29, 2001 · N68391 · Cessna 402C · Instrument PanelSDR HYI2001F00006Master Switch · failedON PREFLIGHT INSPECTION AVIONICS MASTER SWITCH AND RETURNED AIRCRAFT TO SERVICE.Oct 29, 2001 · N68391 · Cessna 402C · DC Power Distribution SystemSDR 20010604CW004Cam · damagedAFTER T/O CREW EXPERIENCED RUDDER LOCK. THROUGH MANIPULATION OF THE ELEVATOR. CONTROLLED RUDDER GUST LOCK RELEASE AND BY WORKING THE RUDDER PEDALS, THE SYSTEM WAS UNLOCKED. MECHANIC FOUND RUDDER GUST LOCK RELEASE CAM DISFIGURED, CAUSING THE RELEASE MECHANISApr 10, 2001 · N68391 · Cessna 402C · Rudder Control SystemSDR 95ZZZX3075Valve · deterioratedPILOT ABORTED TAKEOFF DUE TO ENGINE OVERBOOST. FOUND TOP SECTION OF BUTTERFLY VALVE WARPED DUE TO HEAT. FOUND THAT ON WASTEGATES OVERHAULED USING CONTINUED TIME VALVES, THIS OFTEN HAPPENS ALONG WITH VARING MANIFOLD PRESSURE. ON COMPONENTS WITH NEW VALVES INJun 5, 1995 · N68391 · Cessna 402C · Exhaust Turbocharger
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