Cessna U206F

Service difficulty reports · 227

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 = 'U206F'
  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 96ZZZX4316Hose · leakingHOSE ASSY FAILED AFTER 2 YEARS AND LESS THAN 200 HOURS OF OPERATION. HOSE TSO: C531, MFG DATE A1094, LOT NR 06827.Jul 31, 1996 · N2316U · Cessna U206F · Engine Fuel DistributionSDR 96ZZZX4318Nut · fracturedLIFT STRUT HAS 5 BOLTS, AN5, THROUGH TOP AND BOTTOM. TOTAL OF '5' NUTS HAD FAILED (FIFTY PERCENT). RIGHT LIFT STRUT ALL NORMAL. CAUSE UNKNOWN, NUT P/N NAS679AW.Jul 10, 1996 · N50939 · Cessna U206F · Wing StructureSDR AU960974Battery · leaking(AUS) ELT BATTERY PACK LEAKING - CORROSIVE MATERIAL FROM THE BATTERY HAD LEAKED ONTO THE AIRFRAME STRUCTURE CAUSING CORROSION - EXPIRRATION DATE OF BATTERY IS 22 MAY 1996Jul 3, 1996 · Cessna U206F · Emergency Locator BeaconSDR AU960996Bulkhead · cracked(AUS) FORWARD DOORPOST BULKHEAD CRACKEDJun 26, 1996 · Cessna U206F · Fuselage Main, BulkheadSDR AU960993Hub · cracked(AUS) PROPELLER HUB CRACKED AND LEAKING IN TWO PLACESJun 26, 1996 · Cessna U206F · Propeller Hub SectionSDR 96ZZZX3441Ring · brokenTEMPORARY POWER LOSS DURING CRUISE. SUSPECT CAUSE: BROKEN PISTON RING WHICH BECAME WEDGED BETWEEN PISTON AND CYLINDER WALL. REPLACED COMPLETE CYLINDER ASSY.Jun 24, 1996 · N33247 · Cessna U206F · Reciprocating Engine Cylinder SectionSDR CA970527012Blade · cracked(CAN) PROPELLER RECEIVED FOR OVERHAUL. PROPELLER BLADE WAS FOUND WITH CRACKED THREADS. PROPELLER WAS NEW IN 1986, CORROSION INSPECTION CARRIED OUT IN 1992. THIS WAS THE FIRST OVERHAUL, NOT REQUIRED BY CARS, BUT DONE AT CUSTOMERS REQUEST. THE PROPELLER WAS SCRAMay 22, 1996 · Cessna U206F · Propeller Blade SectionSDR AU961004Crankcase · cracked(AUS) CRANKCASE CRACKED FROM NO2 CYLINDER MOUNT PADMay 8, 1996 · Cessna U206F · Reciprocating Engine Power SectionSDR AU960862Mount · deteriorated(AUS) FORWARD LH RUBBER ENGINE MOUNT PERISHED AND HOLED - SUSPECT CAUSED BY EXHAUST AFTER PROTECTIVE HEAT SHROUD FELL OFFApr 30, 1996 · Cessna U206F · Engine Mount SectionSDR CA960424021Rod End · broken(CAN) BOW WHEEL FAILED TO RETRACT, FOUND ROD END HAD BEEN BROKEN NEXT TO THE CENTRE BALL ALLOWING THE ROD END TO PULL AWAY FROM THE BALL END. SUSPECT INCORRECT RIGGING DUE TO THE 1/4 INCH DISTANCE OF THE ROD END FROM THE GEAR WITH THE GEAR MANUALLY RETRACTED UApr 9, 1996 · Cessna U206F · Landing Gear Door Retract SectionSDR 96ZZZX2454Servo · leads shortingSERVO MOTOR LEADS SHORTING TO FRAME OF PITCH SERVO ONLY WHEN TORQUE APPLIED ON MOTOR WHICH CAUSES PITCH OSCILLATION, PLUS OR MINUS 1,500 FEET/MINUTE. SUBMITTER RECOMMENDS ROUTING TO PREVENT TOUCHING FRAME.Mar 22, 1996 · N2216U · Cessna U206F · Autopilot Main ServoSDR 96ZZZX1480Torque Plate · bushing partedDURING AN ANNUAL INSPECTION, GUIDE BUSHING ON BRAKE TORQUE PLATE FOUND SEPARATED.Mar 8, 1996 · N1523U · Cessna U206F · Landing Gear Brake SystemSDR CA960223005Reinforcement · cracked(CAN)LEFT HAND HORIZONTAL STABILIZER REINFORCEMENT PART #12326231 FOUND CRACKED.Feb 15, 1996 · Cessna U206F · Horizontal Stabilizer StructureSDR 96ZZZX1995Hub · crackedINSPECTION FOUND CRACK IN BLADE RETENTION THREAD OF HUB SOCKET.Feb 14, 1996 · N8498Q · Cessna U206F · Propeller Hub SectionSDR CA960430201Crankshaft · failed(CAN) FOUND CRACK IN CRANKCASE AT #2 CYLINDER. #4 CONNECTING ROD DEPARTED CRANKSHAFT CAUSING INTERNAL ENGINE DAMAGE. DISASSEMBLY OF ENGINE FOUND ALL MAIN BEARING BABBITT OVERLAYS WERE SMEARED FROM OIL STARVATION. ALL CONNECTING ROD BEARINGS SMEARED FROM LUB DIJan 19, 1996 · Cessna U206F · Reciprocating Engine Power SectionSDR 96ZZZX2787Bulkhead · crackedDURING ROUTINE ANNUAL INSP, DISCOVERED FWD CABIN DOORPOST BULKHEAD CRACKED ON LT AND RT SIDES AT WING LIFT STRUT ATTACH FITTINGS. INSP WAS DONE IAW CESSNA SEB 93-5 R1. PREVIOUS INSP OF THIS AREA DURING ANNUAL AND WHEN C/W CESSNA SEB 93-5, FAILED TO FIND THISJan 5, 1996 · N1372V · Cessna U206F · Fuselage Main, BulkheadSDR EY2R9600243Hub · corrodedPROP ASSY HUB IS CORRODEDJan 1, 1996 · Cessna U206F · Propeller Hub SectionSDR EY2R9600242Nut · corrodedPROP ASSY NUT IS CORRODEDJan 1, 1996 · Cessna U206F · Propeller AssemblySDR EY2R9600241Ferrule · corrodedPROP ASSY FERRULE IS CORRODEDJan 1, 1996 · Cessna U206F · Propeller AssemblySDR EY2R9600240Ferrule · corrodedPROP ASSY FERRULE IS CORRODEDJan 1, 1996 · Cessna U206F · Propeller AssemblySDR EY2R9600239Retain Bearing · corrodedPROP ASSY RETAIN BEARING IS CORRODEDJan 1, 1996 · Cessna U206F · Propeller AssemblySDR EY2R9600238Blade · corrodedBLADE SN KK041YSI CORRODEDJan 1, 1996 · Cessna U206F · Propeller Blade SectionSDR CA951221013Mount · cracked(CAN)WHILE CARRYING OUT ROUTINE INSPECTION, BOTH REAR ENGINE MOUNTS WERE FOUND CRACKED. CRACKS WERE APPROXIMATELY ONE INCH LONG. NEW MOUNTS INSTALLED AND AIRCRAFT RETURNED TO SERVICE.Nov 30, 1995 · Cessna U206F · Engine Mount SectionSDR CA951114009Hub · cracked(CAN)PROPELLER HAD PERSISTENT "RED DYE" OIL LEAKS SINCE SEPTEMBER 1989, PROPELLER REMOVED SIX TIMES FOR LEAKS. LAST REMOVAL/INSPECTION HUB THREADS FOUND CRACKED AND PROPELLER REMOVED FROM SERVICE.Aug 29, 1995 · Cessna U206F · Propeller Hub SectionSDR 95ZZZX2378Cylinder · misinstalledTOTAL TIME 1067.8 SMOH. TIME SINCE TOP OVERHAUL 125.0. DURING MAINTENANCE TO REPAIR BURNED VALVES UPON CYLINDER REMOVAL, FOUND CYLINDERS GLUED ON AT BASE. (IT TOOK OVER AN HOUR USING AIR PRESSURE AND PULLING AND PRYING TO REMOVE ONE CYLINDER). IT SEEMS THAApr 24, 1995 · N7144Q · Cessna U206F · Reciprocating Engine Cylinder SectionSDR 95ZZZX1426Impulse Coupling · stop brokeTHE IMPULSE COUPLING STOP ON LEFT MAG BROKE OFF AND FELL DOWN INTO OIL SUMP. IT MADE THE IMPULSE COUPLING INOPERATIVE FOR STARTING, BUT DID NOT HARM NORMAL OPERATION OF MAG. THE STOP PIECES COULD HAVE DAMAGED ACCESSORY DRIVE GEARS, BUT DID NOT. SUBMITTER RECFeb 28, 1995 · N7487Q · Cessna U206F · Magneto/DistributorSDR 95ZZZX1097Line · corrosionDURING AN ANNUAL INSPECTION OF ACFT, LT WING TIP FUEL TANK (FLINT AERO) FUEL LINE TO TRANSFER PUMP FOUND TO HAVE FUEL STAINS IN SEVERAL PLACES & WAS WET TO THE TOUCH. UPON REMOVAL OF FUEL LINE FOR INSP, FOUND SEVERAL PIN HOLES IN AREAS OF THE FUEL STAINS & COJan 4, 1995 · N8295Q · Cessna U206F · Aircraft Fuel Distribution System
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