N26514

Service difficulty reports · 16

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 = 'N26514' 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 HYIA20210611003Strap · corrodedDURING MAINTENANCE, INTERGRANULAR CORROSION WAS VISUALLY DISCOVERED ON THE RIGHT HAND SPAR STRAP OF N26514 AS PART OF SK402-47B (P/N: 5292029-2). THIS CORROSION IS LOCATED AT APPROXIMATE RIGHT WING STATION 106.79 NEAR THE OUTBOARD ENGINE BEAM NACELLE FITTING, Jun 10, 2021 · N26514 · Cessna 402C · Wing SparSDR HYIA20190604001Wire · disconnectedPILOT REPORTED LEFT AND RIGHT ALTERNATOR LIGHTS ON IN FLIGHT. UPON INSPECTION MAINTENANCE DETERMINED THE LEFT ALTERNATOR FIELD WIRE HAD BECOME DISCONNECTED AT LEFT ALTERNATOR SWITCH. THE WIRE WAS RE-CONNECTED AND OPERATIONALLY CHECKED WITH NO FURTHER DEFECTS NMay 31, 2019 · N26514 · Cessna 402C · Electrical Power System WiringSDR HYIA20190524001Bearing · crackedPILOT REPORTED LEFT PROPELLER VIBRATES ABOVE 2500 RPM. MAINTENANCE INSPECTED AND FOUND THE LEFT ENGINE #1 CYLINDER EXHAUST VALVE ERODED AND RECESSED INTO CYLINDER HEAD, AND #4 THE CYLINDER TO HAVE LOW COMPRESSION AND THE #4 CONNECTING ROD BEARING TO HAVE A CRAMay 17, 2019 · N26514 · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20181218001Rod · brokenPILOT REPORTED RIGHT OUTBOARD FLAP DID NOT EXTEND. INSPECTION FOUND THE RIGHT OUTBOARD FLAP ACTUATING ROD BROKEN AT THREADS. ROD WAS REPLACED WITH NO FURTHER DEFECTS NOTED.Dec 14, 2018 · N26514 · Cessna 402C · Trailing Edge Flap Control SystemSDR HYIA20171031001Cylinder · damagedDURING CLIMB OUT OF STT THE CREW REPORTED A DECREASE RT ENGINE MANIFOLD PRESSURE. SUBSEQUENT INCREASE IN RT THROTTLE LEVER DID NOT INCREASE MANIFOLD PRESSURE THOUGH MANIFOLD PRESSURE STABILIZED AT 26". THE FLIGHT WAS CONTINUED. RT ENGINE OIL TEMPERATURE BEGOct 28, 2017 · N26514 · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20170307001Master Switch · odorPILOT REPORTED BURNING RUBBER SMELL IN MAIN CABIN, MAINTENANCE INSPECTED AND REPLACED THE AVIONICS MASTER SWITCH DUE TO SUSPECTED INTERNAL FAILURE (SUSPECTED DUE TO ODOR- NON REPAIRABLE PART).Mar 4, 2017 · N26514 · Cessna 402C · AC Power Distribution SystemSDR HYIA20121205001Actuator · stuckPILOT REPORTED THAT DURING FLIGHT CONTROL CHECK ON TAXI OUT FOR DEPARTURE, THEY NOTED THAT THE AILERON TRIM WAS STUCK IN THE LT WING DOWN POSITION WHEN THEY ATTEMPTED TO ADJUST IT. THE PILOT RETURNED TO THE GATE. UPON MX INSPECTION, THE AILERON TRIM HINGE ANDDec 2, 2012 · N26514 · Cessna 402C · Aileron Tab Control SystemSDR HYIA20121003001Turbocharger · malfunctionedPILOT REPORTED DURING CLIMB AT ABOUT 400 FT AGL, STARTED TO LOSE POWER AND ENCOUNTERED ROUGHNESS FROM THE LT ENGINE. PILOT SHUTDOWN THE ENGINE, FEATHERED PROP, AND RETURNED TO THE FIELD. ON MX INSPECTION, REMOVED AND REPLACED THE TURBOCHARGER. OPENOct 1, 2012 · N26514 · Cessna 402C · Exhaust TurbochargerSDR HYIA20110902001Relay · failedPILOT REPORTED THAT WHILE TAXIING OUT TO RUNWAY 8, NOTICED A FAINT SMELL IN THE CABIN. THEY INITIALLY THOUGHT IT WAS COMING FROM OUTSIDE THE ACFT. THEY THEN REALIZED THE SMELL WAS FROM INSIDE THE CABIN WHEN THEY NOTICED SMOKE COMING FROM BEHIND A PANEL TO THESep 2, 2011 · N26514 · Cessna 402C · AC Power Distribution SystemSDR HYIA20140415051Drag 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 PROCEDUREApr 18, 2011 · N26514 · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415036Drag 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 PROCEDUREMar 11, 2011 · N26514 · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA26514AP1128Computer · shortedCREW REPORTED, ON FINAL APPROACH, A SMALL PUFF OF SMOKE CAME FROM THE NAV/COM PANEL. CREW ACCOMPLISHED SMOKE IN COCKPIT CHECKLIST, SMOKE QUICKLY SUBSIDED AND NO FURTHER SIGNS OF THE PROBLEM EXISTED. ADVISED THE TOWER, AND LANDED WITHOUT INCIDENT. MX INSPECTNov 28, 2010 · N26514 · Cessna 402C · Autopilot ComputerSDR HYIA26514Switch · unserviceableDURING PREFLIGHT, CREW REPORTED AVIONICS MASTER SWITCH INOP. MAINTENANCE REMOVED AND REPLACED SWITCH.Apr 10, 2009 · N26514 · Cessna 402C · Electrical Power SystemSDR HYI2005F00002Bolt · shearedUPON ENGINE START, AFTER SEVERAL ROTATIONS, PROP STOPPED AND WOULD NOT TURN. MECHANIC FOUND CRANKSHAFT LARGE GEAR ATTACH BOLTS SHEARED AND GEAR DISLODGED FROM CRANKSHAFT. MECHANIC REMOVED AND REPLACED ENGINE AND RETURNED AIRCRAFT TO SERVICE. (NE01200502601)Jan 31, 2005 · N26514 · Cessna 402C · Main Landing GearSDR HYI2004F00002Gear · failedUPON START, RT ENGINE FAILED TO TURN. MECHANIC FOUND PROP COULD NOT BE TURNED BY HAND EITHER. LATER INSPECTION FOUND CRANKSHAFT LARGE GEAR MISSING TEETH, AND STARTER ADAPTER MISSING TEETH ON DRIVE GEAR. MECHANIC TO REMOVE AND REPLACE ENGINE.Apr 19, 2004 · N26514 · Cessna 402C · Reciprocating Engine Power SectionSDR 99ZZZX4252Circuit Breaker · failedCREW DECLARED EMERGENCY EN ROUTE ACK/BOS WHEN SMOKE CAME FROM AFT SIDE PANEL AFTER RE-SETTING AVIONICS MASTER SWITCH, FOR AVIONICS FAILURE. USING EMERGENCY AVIONIC SWITCH, RESUMED COMMUNICATIONS WITH BOS. APPROACH, LANDED WITHOUT INCIDENT. MAINTENANCE REPLAAug 10, 1999 · N26514 · Cessna 402C · AC Power Distribution System
Back to N26514