Cessna U206

Service difficulty reports · 27

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 = 'U206'
  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 CA111124003Scoop · failed(CAN) BOTTOM OF AIR SCOOP BEHIND AIR CLEANER BROKE OUT IN SMALL PIECES WHICH WERE INGESTED INTO THE ENGINE HOLDING VALVES WHICH CAUSED ENGINE TO QUIT. HEAVY MATERIAL WAS INSTALLED IN DEFECTED AREA. WILL MONITOR. ORIGINAL MATERIAL WAS SOFT AND WAS FLEXING CAUAug 16, 2011 · Cessna U206 · Engine Air Intake SystemSDR CA090402003Screw · missing(CAN) THE PILOT NOTED HIS AILERON CONTROLS WERE SLUGGISH DURING FLIGHT AND THE CONTROL WHEEL WAS OFF CENTER DURING LEVEL FLIGHT. DURING ROUTINE INSP IT WAS FOUND THAT THE UPPER AILERON PULLEY BRACKET SCREW AND NUT WERE MISSING. THE PULLEY BRACKET WAS SLIGHTLY Mar 20, 2009 · Cessna U206 · Wing, Attach FittingsSDR CA070228003Control Arm · defective(CAN) THE SUBJECT AIRCRAFT WAS CLIMBING OUT AFTER TAKEOFF AND EXPERIENCED A SIGNIFICANT LOSS OF CLIMB POWER RELATED TO A DROP IN ENGINE RPM FROM 2700 RPM TO 1600 RPM. THE PILOT EXECUTED ALL APPROPRIATE EMERGENCY PROCEDURES/ACTIONS WITH NO IMPROVEMENT. THE PILFeb 28, 2007 · Cessna U206 · Propeller GovernorSDR ENE2006F00000Cylinder Head · separatedBOTH CYLINDERS FAILED AT TAKEOFF POWER SETTING WITHIN 2 HOURS OF EACH OTHER. FAILURE CONSISTING OF COMPLETE SEPARATION OF THE HEAD FROM THE BARREL, CAUSING DAMAGE TO THE BAFFLING. EXHAUST COLLECTOR, AND SEVERING OF THE FUEL INJECTOR LINE.Apr 19, 2006 · Cessna U206 · Reciprocating Engine Cylinder SectionSDR 2004F00401Cylinder Head · separatedCYLINDER HEAD SEPARATED FROM BARREL IN CRUISE .Sep 30, 2004 · N9417G · Cessna U206 · Reciprocating Engine Cylinder SectionSDR CA040709003Screw · worn(CAN) DURING ENGINE START, FIRST FLIGHT OF THE DAY, OIL PRESSURE WAS OBSERVED AS BEING TOO HIGH (75 PSI AT IDLE). SYSTEM BLOCKAGE WAS SUSPECTED, OIL FILTER INSPECTED (CLEAR), OIL DRAINED AND INSPECTED (CLEAR), PRESSURE CHECKED AT OTHER PRESSURE POINTS IAW MFGJul 1, 2004 · Cessna U206 · Reciprocating Engine Oil SystemSDR MK92003F00000Bar · brokenFLANGE ON RUDDER BAR BROKEN. LT SIDE, LT BRAKE PEDAL ATTACHMENT. PILOT WAS LANDING AIRCRAFT WHEN IT BROKEN. LANDED AND TAXIED SAFETLY. CLOSE INSPECTION OF ALL FLANGES AND SPRAYING PENTRATING OIL DOWN RUDDER PEDAL BAR WOULD HELP PREVENT INTERIOR CORROSION WNov 2, 2003 · N5286U · Cessna U206 · Rudder Control SystemSDR AUS20030419Control Cable · separated(AUS) THROTTLE CABLE OUTER GUIDE SEPARATED FROM SWAGED SWIVEL JOINT ALLOWING CABLE TO FAIL IN COMPRESSION.Apr 11, 2003 · Cessna U206 · Power LeverSDR AUS20030345Bearing · worn(AUS) CONNECTING ROD BIG END BEARING WORN EXCESSIVELY.Mar 7, 2003 · Cessna U206 · Reciprocating Engine Power SectionSDR AUS20010516Spring · failed(AUS) STARTER CLUTCH SPRING FAILED CAUSING DAMAGE TO THE CRANKSHAFT,CAMSHAFT GEAR AND ATTACHING HARDWARE. ROCKWELL HARDNESS TESTREVEALED INCONSISTANT HARDNESS.Apr 12, 2001 · Cessna U206 · Engine StarterSDR AU000674Impulse Coupling · faulty(AUS) MAGNETO IMPULSE COUPLINGS (2OFF) HAD LOOSE RIVETS IN THE FLYWEIGHT ASSEMBLIES. FOUND DURING INSPECTION IAW SLICK SB 1-86B. (X)Sep 1, 2000 · Cessna U206 · Magneto/DistributorSDR AU000620Cylinder · separated(AUS) NR 6 CYLINDER HEAD SEPARATED FROM BARREL. (X)Sep 1, 2000 · Cessna U206 · Reciprocating Engine Cylinder SectionSDR 20000908SH008Points · failedDURING PRE-INSPECTION RUN-UP BY MECHANIC, FOUND UNUSUAL MAG DROP ON RIGHT MAGNETO REMOVED FOR TROUBLESHOOTING. FOUND THE POINT ASSY CONTACT LOOSE AND FALLING OUT OF SPRING ARM. REPLACED CONTACT ASSY. OPS CHECKED GOOD. THIS MAG HAD 184 HOURS SINCE A TCM OVEAug 15, 2000 · N527NR · Cessna U206 · Magneto/DistributorSDR 98ZZZX4656Condenser · failedCONDENSER FAILED 20.0 HOURS AFTER OVERHAUL. THIS CAUSED THE POINTS TO BURN RESULTING IN EXCESSIVE MAGNETO DROP. DATE CODE: 96-47.Nov 1, 1998 · Cessna U206 · Magneto/DistributorSDR 97ZZZX3810Bulkhead · crackedINSPECTION FOUND TAIL CONE BULKHEAD AT BS 230.187 CRACKED. REPLACED WITH P/N 1212130-2.Aug 18, 1997 · N8030Z · Cessna U206 · Fuselage Main, BulkheadSDR 97ZZZX3709Trim Tab · out of balancePARACHUTING FLIGHT - AFTER JUMP TRIMMED NOSE DOWN, IN DESCENT 150 MPH, ELEVATOR VIBRATION WHICH DISAPPEARED WHEN SPEED 130 MPH. TRIM TAB UNDERSIDE SKIN WAS DEFORMED UNDER BRACKET ASSEMBLY AND TRIM ACTUATOR WAS LOOSE FROM FASTENERS. ELEVATOR MASS BALANCE WASJun 1, 1997 · N2FOR · Cessna U206 · Elevator, Tab StructureSDR 97ZZZX3708Trim Tab · core soakedPARACHUTING FLIGHT - FL 100, AFTER JUMP IN DESCENT SPEED 100 MPH ELEVATOR FLUTTER, FAST AND HEAVY MOVEMENTS 2-3 SECONDS, DISAPPEARED WHEN SPEED 80 MPH. TRIM ACTUATOR WAS LOOSE FROM BROKEN STABILIZER BRACKET, FREE MOVEMENT 2 INCHES. NEARBY RIB WAS ALSO BROKENJun 1, 1997 · N2FOR · Cessna U206 · Elevator, Tab StructureSDR PNSA970301Engine · low powerAIRCRAFT DID NOT CLIMB WELL AFTER TAKEOFF. RETURNED TO BASE. NO DEFECTS NOTED WITH ENGINE, TEST FLIGHT OK.Mar 12, 1997 · N690PA · Cessna U206 · Engine (Turbine/Turboprop)SDR EY2R9601269Retainers · corrodedRETAINERS FOUND CORRODED.Dec 1, 1996 · Cessna U206 · Propeller AssemblySDR EY2R9601268Bearings · corrodedBEARINGS FOUND CORRODED.Dec 1, 1996 · Cessna U206 · Propeller AssemblySDR EY2R9601267Hub · corrodedHUB CORRODED.Dec 1, 1996 · Cessna U206 · Propeller Hub SectionSDR 96ZZZX3544Pulley · separatedDRIVE PULLEY FOUND SEPARATED FROM VENT FAN DURING UNSCHEDULED MAINTENANCE. ALTERNATOR, 386.7 HOURS SINCE OVERHAUL. PULLEY TIME UNKNOWN. CORROSION EVIDENT ON MATING SURFACES OF DETACHED PIECES.Jun 17, 1996 · N8013Z · Cessna U206 · DC Generator-AlternatorSDR EY2R9600644Dowel · corrodedDOWEL CORRODED.May 1, 1996 · Cessna U206 · Propeller AssemblySDR 96ZZZX2299V-Channel · crackedV-CHANNEL CRACKED WHERE AILERON HINGE RIVETED TO IT. DIFFICULT TO SEE CRACK. SUSPECT DEFECTIVE IF MOVEMENT NOTICED WHEN PRESSURE APPLIED UPWARD TO FLAT OF AILERON LOWER SURFACE.Apr 4, 1996 · N569QL · Cessna U206 · Wing Miscellaneous StructureSDR 96ZZZX2152Cylinder · crackedNR 3, NR 2, AND NR 5 CYLINDERS WERE FOUND CRACKED AT INTAKE SEAT.Mar 20, 1996 · N244PL · Cessna U206 · Reciprocating Engine Cylinder SectionSDR 96ZZZX2151Cylinder · crackedNR 4 AND NR 1 CYLINDERS WERE FOUND CRACKED AT INTAKE SEAT.Mar 1, 1996 · N4672U · Cessna U206 · Reciprocating Engine Cylinder SectionSDR 95ZZZX5038Lever · brokeTHROTTLE LEVER BROKE AT END OF LEVER WHERE THROTTLE ROD END ATTACHES ALLOWING THROTTLE TO DISCONNECT FROM ENGINE. AIRCRAFT LANDED WITHOUT DAMAGE OR INJURY.Aug 30, 1995 · N8467Q · Cessna U206 · Power Lever
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