Cessna U206G

Service difficulty reports · 415

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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 = 'U206G'
  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 CA000614017Hub · cracked(CAN) FIELD MAINTENANCE FOUND SUSPECTED CRACK, N.D.T. CONFIRMED CRACK. HUB REPLACED, PROPELLER RETURNED TO SERVICE.Jun 2, 2000 · Cessna U206G · Propeller Hub SectionSDR 20000602SH002Crankshaft · unserviceablePER TCM MSB 00-5, CRANKSHAFT WAS REJECTED BY TELEDYNE CONTINENTAL MOTORS. (X)May 12, 2000 · N2216F · Cessna U206G · Reciprocating Engine Power SectionSDR 20000712SH020Spar · crackedDURING ROUTINE INSP, NOTED THE RT WING AFT SPAR WEB CRACKED IN 5 PLACES AND THE ROLL SERVO ATTACH BRACKET 60931 CRACKED AT THE OTBD SERVO ATTACH HOLE. ALL CRACKS ARE IN VICINITY OF S-TEC ROLL SERVO BRACKET ATTACHMENT BOLTS. S-TEC TWO AXIS AUTOMATIC FLIGHT GUApr 24, 2000 · N783 · Cessna U206G · Wing SparSDR AU000242Spark Plug · faulty(AUS) NR 3 CYLINDER SPARK PLUGS (2 OFF) BRIDGED ACROSS ELECTRODES.Apr 23, 2000 · Cessna U206G · Spark Plug/IgniterSDR AU000176Control Panel · burned(AUS) ALTERNATOR CONTROL UNIT INTERNAL FAULT.Feb 7, 2000 · Cessna U206G · DC Generating SystemSDR 2000ZZZX645Hose · leakingDURING ANNUAL INSPECTION, FOUND ABOVE MENTIONED HOSE LEAKING PROFUSELY. THE HOSE APPEARED TO BE SUPPORTED PROPERLY. WHEN FUEL PRESSURE WAS APPLIED WITH AIRCRAFT ELECTRIC BOOST PUMP, FUEL BEGAN COMING OUT OF BRAIDED, CRIMPED AREA NEAR THE END OF THE HOSE. ADFeb 2, 2000 · N68RS · Cessna U206G · Aircraft Fuel Distribution SystemSDR 99ZZZX4699Magneto · failedPILOT REPORTED MINOR ENGINE ROUGHNESS IN-FLIGHT AT HIGH ALTITUDES. IN-FLIGHT MAGNETO CHECK SHOWED MAGNETO ON LEFT SIDE TO BE COMPLETELY DEAD. POINTS AND ROTOR AND CONDENSER ARE OK.Dec 13, 1999 · N995RA · Cessna U206G · Magneto/DistributorSDR CA991229016Bolt · broken(CAN) DURING 100 HOUR INSPECTION, MAINTENANCE PERSONNEL CHECKED THE BOLT AT THE AFT END OF THE NOSE GEAR DRAG STRUT, WITH A WRENCH. LIGHT PRESSURE FRACTURED THE BOLT HEAD FROM THE SHANK. THE SUBMITTER HAS FOUND A NUMBER OF THESE BOLT HEADS BROKEN OFF IN VARIOUDec 12, 1999 · Cessna U206G · Nose/Tail Landing GearSDR 99ZZZX4217Engine · failedIN-FLIGHT FAILURE OF ENGINE. APPARENT BROKEN CRANKSHAFT. NOTE: AD 99-09-17 C/W BY FACTORY. INSTALLATION OF NEW CRANKSHAFT 5-26-99. NO DAMAGE TO AIRCRAFT DUE TO SUCCESSFUL EMERGENCY LANDING.Oct 18, 1999 · N496K · Cessna U206G · Engine (Reciprocating)SDR CA991027040Crankshaft · failed(CAN) CRANKSHAFT FAILED - THERE ARE MAINTENANCE LOG ENTRIES OF PREVIOUS PROP STRIKE.Oct 10, 1999 · Cessna U206G · Reciprocating Engine Power SectionSDR CA991027039Bolt · sheared(CAN) DURING MAINTENANCE, NOSE GEAR DRAG LINK, AFT ATTACH BOLT FOUND WITH BOLT HEAD SHEARED OFF.Oct 10, 1999 · Cessna U206G · Nose/Tail Landing Gear Attach SectionSDR AU991027Actuator · worn(AUS) ELEVATOR TAB ACTUATOR SPROCKET LOCATING PINS MIGRATED PREVENTING THE TAB FROM MOVING. INVESTIGATION FOUND WEAR IN THE GROOVE PIN HOLES.Oct 8, 1999 · Cessna U206G · Elevator Tab Control SystemSDR AU991080Piston Pin · failed(AUS) NR 2 CYLINDER PISTON PIN END CAP SHEARED OFF. ENGINE OIL SYSTEM CONTAMINATED WITH METAL.Sep 10, 1999 · Cessna U206G · Reciprocating Engine Cylinder SectionSDR 99ZZZX3475Hinge Assy · crackedBOTH INBOARD AND OUTBOARD AILERON HINGE BRACKET ASSYS ON THE RIGHT WING WERE CRACKED ON THE BOTTOM AND HAD LOOSE OF SHEARED RIVETS WHERE THEY ATTACH TO THE REAR SPAR. THIS DAMAGE CANNOT BE SEEN WITHOUT REMOVING THE FALSE SPAR, BUT CAN BE DETECTED BY LOOSENESSAug 13, 1999 · N733KD · Cessna U206G · AileronsSDR 99ZZZX3491Hub · crackedET INDICATIONS IN BLADE SOCKETS 2 AND 3 IN EXCESS OF 350 MICRORAMPS.Aug 2, 1999 · N756BB · Cessna U206G · Propeller Hub SectionSDR 99ZZZX3139Engine · failedPILOT REPORTED ENGINE VIBRATING BADLY AND LOSING POWER ON CLIMB-OUT. AIRCRAFT MADE A SAFE LANDING AT DEPARTURE AIRPORT. OIL WAS ALL ALONG THE RIGHT SIDE OF THE AIRCRAFT. ON REMOVING THE COWL, A HOLE APPROXIMATELY 2 INCHES BY 3 INCHES WAS IN THE CASE AND A CJul 15, 1999 · N995RA · Cessna U206G · Engine (Reciprocating)SDR 99ZZZX2544Rod End · brokenROD END BROKE WHERE IT EXITS SPACER ASSY, PN 1260632-3, WHICH IS THE RUDDER TRIM SPROCKET AT THE END OF THE STEERING BUNGEE. SUBMITTER STATED THIS IS THE THIRD ONE KNOWN TO BREAK IN 10 YEARS. NO NOSE WHEEL STEERING, BUT STILL RUDDER STEERING.Jun 22, 1999 · N46374 · Cessna U206G · Rudder Control SystemSDR AU990679Blade · misrigged(AUS) PROPELLER BLADE SETTINGS INCORRECT. FINE PITCH SET AT 12.5 DEGREES INSTEAD OF AT 11.2 DEGREES.Jun 17, 1999 · Cessna U206G · Propeller Blade SectionSDR 99ZZZX1638Head · crackedHEAD CRACKED, STARTING FROM THE EXHAUST VALVE SEAT AND TRAVELING UP ABOVE THE SPARK PLUG BOSS AND BACK DOWN APPROXIMATELY ONE INCH FROM THE INTAKE VALVE SEAT. THE ENTIRE LENGTH OF THE CRACK WAS APPROXIMATELY FOUR INCHES. A .1250 INCH BY ONE INCH HOLE HAD OPEApr 1, 1999 · N6400X · Cessna U206G · Reciprocating Engine Cylinder SectionSDR 99ZZZX953Bracket · corrodedANNUAL INSPECTION OF AIRCRAFT USED EXTENSIVELY IN SALT WATER/FLOAT OPERATION, REVEALED BOTH OTBD ELEVATOR ATTACH BRACKETS CORRODED AND LIGHT DAMAGE TO STABILIZER REAR SPARS.Feb 18, 1999 · N22306 · Cessna U206G · Elevator StructureSDR 99ZZZX1429Valve · wornAT ENGINE TT 378.8 HOURS, REMOVED ALL CYLINDERS AND HONED DUE TO 'GLAZING'. AT ENGINE TT 380.0 HRS, PILOT REPORTED ENGINE RUNNING ROUGH. REPLACED NR 6 CYLINDER ASSY DUE TO 'LOW' COMPRESSION 20/80 PSI. FURTHER INSPECTION OF CYLINDER REVEALED EXCESSIVELY WORN IFeb 11, 1999 · N4689U · Cessna U206G · Reciprocating Engine Cylinder SectionSDR CA990223002Bolt · broken(CAN) AFT DRAG LINK BOLT FOUND WITH THE BOLT HEAD SHEARED OFF. SUBMITTER STATED THIS IS THE SECOND ONE FOUND IN 200 HOURS ON THE SAME AIRCRAFT.Feb 9, 1999 · Cessna U206G · Landing Gear Retraction/Extension SystemSDR AU990087Bracket · broken(AUS) ENGINE THROTTLE/MIXTURE CONTROL CABLE SUPPORT BRACKET BROKEN. BRACKET IS MOUNTED ON THE INDUCTION MANIFOLD.Feb 2, 1999 · Cessna U206G · Power LeverSDR CA990318027Bolt · sheared(CAN) ON INSPECTION OF THE MLG, THE FRONT RIGHT HAND BOLT ATTACHING THE GEAR LEG WAS FOUND TO BE SHEARED. OTHER BOLTS WERE INVESTIGATED WITH NO FAILURES.Feb 1, 1999 · Cessna U206G · Main Landing Gear Attach SectionSDR 99ZZZX949Line · chafed100 HOUR INSPECTION FOUND RT AILERON CABLE RUBBED THROUGH FORWARD FUEL LINE INSIDE CABIN (UPPER RT SIDE WHERE FUEL LINE ENTERS CABIN BY WINDSHIELD.) INSTALLED NEW PART, ADJUSTED AWAY FROM CABLE WHEN CONNECTED TO TANK.Feb 1, 1999 · N206JK · Cessna U206G · Fuel StorageSDR 99ZZZX1078Frame · crackedRIGHT DOOR POST JAMB HAD A CRACK IN OUTBOARD EDGE OF JAMB THROUGH A SCREW HOLE AND EXTENDING 1 INCH FROM EDGE.Feb 1, 1999 · N22306 · Cessna U206G · Fuselage Main, FrameSDR CA990318026Handle · broken(CAN) OUTSIDE LEVER ON CARGO DOOR BROKEN.Jan 8, 1999 · Cessna U206G · Cargo/Baggage DoorsSDR AU990001Nut · missing(AUS) DURING PERIODIC ENGINE INSPECTION, IT WAS DISCOVERED THAT THE BOLT (PN AN7-46A) SECURING THE ALTERNATOR TO THE ALTERNATOR MOUNT (PN 643935) WAS LOOSE AND HAD ELONGATED THE MOUNTING HOLES IN THE MOUNT AND ALTERNATOR. FURTHER INVESTIGATION REVEALED THAT TJan 4, 1999 · Cessna U206G · Alternator-Generator DriveSDR CA990318021Jackscrew · worn(CAN) EXCESSIVE PLAY FOUND IN ELEVATOR TRIM JACK WORM GEAR.Jan 1, 1999 · Cessna U206G · Elevator Control SystemSDR AU981678Switch · corroded(AUS) ON SELECTION, FLAPS FAILED TO EXTEND. INVESTIGATION FOUND CORRODED TERMINALS ON THE SELECTOR SWITCH MICROSWITCHES.Dec 24, 1998 · Cessna U206G · Trailing Edge Flap Control SystemSDR AU981679Connector · loose(AUS) MAIN LANDING GEAR 'UP' PRESSURE LINE CONNECTION TO SELECTOR FOUND NOT CORRECTLY TIGHTENED - RESULTING IN COMPLETE LOSS OF RESERVOIR OIL.Dec 22, 1998 · Cessna U206G · Hydraulic System, MainSDR AU981664Wing Tip · damaged(AUS) AFTER LANDING, THE AIRCRAFT DEPARTED RUNWAY AND RAN INTO SOFT SOIL SLIGHTLY DAMAGING BOTH DROP WING TIPS AND ONE PROPELLER BLADE.Dec 15, 1998 · Cessna U206G · Wing, Plate/SkinSDR 98ZZZX4330Bushing · damagedDEFECT MAY HAVE BEEN CAUSED BY OVERCENTER NOT GOING TO FULL TRAVEL.Oct 13, 1998 · N94EL · Cessna U206G · Wheel/Ski/FloatSDR 98ZZZX4329Bushing · damagedDEFECT MAY HAVE BEEN CAUSED BY OVERCENTER NOT GOING TO FULL TRAVEL.Oct 13, 1998 · N94EL · Cessna U206G · Wheel/Ski/FloatSDR CA981109001Bolt · missing(CAN) DURING OPS 4 INSPECTION, THE PILOTS CONTROL COLUMN WAS FOUND LOOSE. FURTHER INVESTIGATION FOUND ONE BOLT MISSING AND TWO OTHER BOLTS LOOSE. PART TC: 7,577.Sep 30, 1998 · Cessna U206G · Control Column SectionSDR 98ZZZX4260Strut Fitting · crackedDURING ANNUAL INSPECTION, FOUND THE AFT LEFT UPPER DIAGONAL STRUT FITTING CRACKED IN FIVE SEPARATE AREAS ON BOTH THE UPPER AND LOWER SURFACES ALONG THE LONGITUDINAL GRAIN. IT WAS ALSO NOTED THAT TWO CRACKS WERE LOCATED ALONG AN ORIGINAL MACHINING MARK. THE MSep 15, 1998 · N70SB · Cessna U206G · Wing Miscellaneous StructureSDR 98ZZZX4580Strut Fitting · corrodedDURING THE RECEIVING INSPECTION OF A WIPLINE 3730 FRONT STRUT JOINING FITTING, PITTING CORROSION WAS FOUND ON THE FRONT FACE SURFACE. THE PART WAS RED TAGGED AND RETURNED TO WIPAIRE, INC.Sep 14, 1998 · Cessna U206G · Wing Miscellaneous StructureSDR 98ZZZX4579Fitting · corrodedDURING RECEIVING INSPECTION OF A WIPLINE 3730 NOSE LANDING GEAR PIVOT BLOCK, CORROSION/CASTING FLAWS WERE FOUND ON THE LOWER FACE SURFACE. THE PART WAS RED TAGGED AND RETURNED TO WIPAIRE, INC.Sep 14, 1998 · Cessna U206G · Landing Gear Retraction/Extension SystemSDR AU981519Cylinder · cracked(AUS) NR 4 CYLINDER HEAD CRACKED. CRACK LENGTH APPROXIMATELY 25.4 MM (1 INCH). PART TC: 1,865.Sep 4, 1998 · Cessna U206G · Reciprocating Engine Cylinder SectionSDR AU981114Support · cracked(AUS) HORIZONTAL STABILIZER REINFORCEMENT CRACKED.Aug 31, 1998 · Cessna U206G · Horizontal Stabilizer StructureSDR CA980928006Collar · broken(CAN) ON TAKEOFF, THE STEERING COLLAR BROKE. AIRCRAFT LANDED OK. NEW PART APPEARS TO BE OF A HEAVIER MATERIAL.Aug 20, 1998 · Cessna U206G · Landing Gear Steering SystemSDR 99ZZZX301Nut · crackedDURING INSPECTION OF ENGINE FOR OIL LEAK, THE LOWER FORWARD CYLINDER FLANGE ATTACH NUT (AT THRU-BOLT) WAS FOUND CRACKED AND LOOSE ON BOLT. UNABLE TO DETERMINE CAUSE OF FAILURE.Aug 4, 1998 · N9776G · Cessna U206G · Reciprocating Engine Cylinder SectionSDR 98ZZZX3478Skin · corrodedCORROSION UNDER THE VIBRATION ABSORBING PADS DUE TO WATER BEING TRAPPED WHERE THE BONDING OF THE PAD TO THE SKIN HAS FAILED. SUBMITTER STATES THIS IS A COMMON PROBLEM WITH CESSNA AIRCRAFT.Jul 21, 1998 · N756GF · Cessna U206G · Fuselage Main, Plate/SkinSDR 98ZZZX3141Bearing · failedBEARING SHOULD HAVE 519.9 HOURS IF CHANGED AT OVERHAUL. ENGINE OVERHAULED BY T.W. SMITH ON 6-25-93. MAY HAVE ALSO BEEN CAUSED BY OVERTIGHTENING OF ALTERNATOR BELT. BEARING FAILURE RESULTED IN METAL CONTAMINATION OF THE OIL AND OIL FILTER.Jul 14, 1998 · N7433N · Cessna U206G · Starter-GeneratorSDR 98ZZZX2984Bungee · weakON TWO NON-CONSECUTIVE LANDINGS WITH THE SAME PILOT, THE A/C VEERED OFF THE RUNWAY TO THE RIGHT. PILOT EXPRESSED A LOSS OF DIRECTIONAL CONTROL OF THE A/C DUE TO AN UNSTEERABLE NOSE GEAR AND POSSIBLY A NOSE GEAR THAT MAY HAVE NOT BEEN FULLY CENTERED ON INITIALJul 14, 1998 · N7261N · Cessna U206G · Landing Gear Steering SystemSDR 98ZZZX3570Fitting · crackedFITTINGS CRACKED, BUSH OPERATIONS.Jul 13, 1998 · N5200X · Cessna U206G · Main Landing Gear Attach SectionSDR 98ZZZX3569Fitting · crackedLT MLG FITTINGS CRACKED, BUSH OPERATIONS.Jul 13, 1998 · N5200X · Cessna U206G · Main Landing Gear Attach SectionSDR 98ZZZX2357Spinner · crackedDURING A 100-HOUR INSPECTION, THE PROP SPINNER WAS FOUND CRACKED IN THREE PLACES. THE CRACKS WERE IN THE CENTER OF EACH BLADE CUT-OUT. NO OTHER DAMAGE WAS FOUND. THE PROBLEM MAY HAVE BEEN CAUSED FROM PUSHING ON THE SPINNER DURING GROUND HANDLING.Jun 8, 1998 · N756HK · Cessna U206G · Propeller Spinner SectionSDR 98ZZZX3174Fitting · crackedDURING A 200-HOUR INPSECTION, BOTH MAIN GEAR OUTBOARD ATTACHMENT FITTINGS WERE FOUND CRACKED. THIS AIRCRAFT HAD AN INCIDENT SEVERAL HUNDRED HOURS AGO, BUT NO RECENT REPORT OF A HARD LANDING. THIS ACFT IS SUBJECTED TO MANY LANDINGS ON GRAVEL STRIPS WHICH MAY Jun 4, 1998 · N756HK · Cessna U206G · Main Landing Gear Attach SectionSDR 98ZZZX3173Fitting · crackedDURING A 200-HOUR INSPECTION, BOTH MAIN GEAR OUTBOARD ATTACHMENT FITTINGS WERE FOUND CRACKED. THIS AIRCRAFT HAD AN INCIDENT SEVERAL HUNDRED HOURS AGO, BUT NO RECENT REPORT OF A HARD LANDING. THIS ACFT IS SUBJECTED TO MANY LANDINGS ON GRAVEL STRIPS WHICH MAY Jun 4, 1998 · N756HK · Cessna U206G · Main Landing Gear Attach Section
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