Cessna U206F

Service difficulty reports · 227

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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 AUS20030598Spar Cap · corroded(AUS) RT WING SPAR CAP RIVET HEADS MISSING. INVESTIGATION FOUND THE SPAR CAP EXTENSIVELY CORRODED.Apr 24, 2003 · Cessna U206F · Wing SparSDR AUS20030617Line · chafed(AUS) FUEL LINE CHAFED BY AILERON CABLE.Apr 2, 2003 · Cessna U206F · Aircraft Fuel Distribution SystemSDR CA030726006Rivet · loose(CAN) LOOSE RIVETS ON BOTH WINGS AT AILERON HINGE BRACKET REPLACED.Mar 5, 2003 · Cessna U206F · AileronsSDR AUS20030079Filter · contaminated(AUS) ENGINE FUEL FILTER CONTAMINATED WITH WATER.Jan 14, 2003 · Cessna U206F · Engine Fuel DistributionSDR CA030726005Alternator · failed(CAN) LOSS OF ALTERNATOR POWER. ALTERNATOR OVERHAULED.Oct 9, 2002 · Cessna U206F · DC Generator-AlternatorSDR 2002FA0001249Cylinder · crackedPILOT NOTED ROUGH RUNNING ENGINE AND MADE PRECAUTIONARY LANDING. LATER INSPECTION REVEALED NR 1 CYLINDER CRACKED AND A HOLE BLOWN THROUGH THE EXHAUST SIDE.Oct 5, 2002 · N8300Q · Cessna U206F · Reciprocating Engine Cylinder SectionSDR FMAA2002003Wheel · crackedTHE NOSE WHEEL IS MADE UP OF 3 MAJOR COMPONENTS, THE 2 WHEEL FLANGES AND THE HUB. THE SCREWS HAVE NO LOCKING DEVICE, AND AFTER MANY HOURS OF USE THE SCREWS BACK OUT OF THE HUB AND OR THE SCREW HOLES IN THE HUB CRACK AND ALLOW THE THREADED HOLE TO GET LARGER ASep 7, 2002 · N8515Q · Cessna U206F · Wheel/Ski/FloatSDR AUS20020858Bolt · loose(AUS) ALTERNATOR THROUGH BOLTS LOOSE. ROTOR RUBBING ON FIELD WINDINGS CAUSING DAMAGE TO STATOR. SUSPECT CAUSED BY FAILURE TO RETORQUE BOLTS AFTER FIFTEEN HOURS OPERATION.Jul 4, 2002 · Cessna U206F · DC Generator-AlternatorSDR CA030726003Throttle · malfunctioned(CAN) NEW THROTTLE INSTALLED DUE TO MALFUNCTION.Jun 18, 2002 · Cessna U206F · Power LeverSDR AUS20020631Pump · cracked(AUS) ENGINE OIL PUMP HOUSING CRACKED. CRACK APPEARS TO ORIGINATE FROMA CASTING MARK. FOUND WHEN OIL FILTER ADAPTER WAS REMOVED FOR RECTIFICATION OF AN OIL LEAK.Jun 14, 2002 · Cessna U206F · Reciprocating Engine Oil SystemSDR CA020529003Hinge · cracked(CAN) CRACK FOUND IN LOWER ATTACH FLANGE DURING SPECIAL INSPECTION PER CESSNA CONTINUED AIRWORTHINESS PROGRAM.THIS WAS LEFT HAND INBOARD HINGE. ALSO FOUND RIGHT HAND INBOARD HINGE CRACKED. OUTBOARD LEFT HAND HINGE HAD BEEN RECENTLY REPLACED.May 14, 2002 · Cessna U206F · Wing, Control Surface Attach FittingsSDR CHI2002F00003Rod End · shearedNOSE GEAR WAS PROBABLY TURNED BEYOND LIMITS REPEATEDLY OVERTIME PUT STRESS ON THREADED PORTION OF THE ROD END.Mar 14, 2002 · N77CR · Cessna U206F · Landing Gear Steering SystemSDR 2002FA0000413Impulse Coupling · defectiveTHE WOODRUFF KEY (M2536) THAT LOCKS THE IMPULSE COUPLING ON THE SHAFT WAS FOUND LODGED UNDERNEATH THE IMPULSE COUPLING PAWL, RENDERING ONE OF THE TWO PAWLS IMMOBILE. THE PIN ATTACHING THE PAWL WAS BENT AND THE GAP BETWEEN THE PAWL BOSS AND PLATE WAS NEAR LIMIFeb 21, 2002 · N1003V · Cessna U206F · Magneto/DistributorSDR CA020226008Roll Pin · sheared(CAN) FUEL SELECTOR WOULD NOT ROTATE VALVE. DISASSEMBLED AND FOUND PIN SECTION MISSING ALLOWING HOUSING YOKE TO ROTATE ON SHAFT. PIN REPLACED.Feb 20, 2002 · Cessna U206F · Fuel Selector/Shut-Off ValveSDR AUS20020111Filter · burned(AUS) ENGINE AIR FILTER BURNT.Feb 7, 2002 · Cessna U206F · Engine Air Intake SystemSDR 2002FA0000109Distributor · burnedMAGNETO HAD FAILED 9.3 HOURS AFTER BEING SUPPLIED AS A PART OF A FACTORY REBUILT ENGINE. IT WAS DISASSEMBLED AND THE DISTRIBUTOR, COIL, CAPACITOR AND BREAKER WERE REPLACED. MAGNETO WAS CHECKED OK. 2.5 HOURS AFTER THIS REPAIR THE MAGNETO FAILED AGAIN. THE DDec 7, 2001 · Cessna U206F · Magneto/DistributorSDR AUS20011403Mount · cracked(AUS) LT AND RT REAR ENGINE MOUNT SUPPORT BRACKETS CRACKED FROM REAR INBOARD BEND RADIUS. NUMEROUS RIVETS IN SURROUNDING STRUCTURE FRETTING.Nov 29, 2001 · Cessna U206F · Engine Mount SectionSDR AUS20011010Distributor · burned(AUS) MAGNETO DISTRIBUTOR BLOCK BADLY BURNT DUE TO TRACKING FROM DISTRIBUTOR WHEEL SPRING TO MAGNETO HOUSING.Sep 10, 2001 · Cessna U206F · Magneto/DistributorSDR CA010523006Placard · reversed(CAN) THE DECAL ON THE ELEVATOR TRIM WHEEL APPEARS TO HAVE BEEN FABRICATED. WHEN IT WAS INSTALLED, THE "NOSE UP" AND "NOSE DOWN" DECALS WERE REVERSED. WHEN THE PILOT THOUGHT HE WAS TRIMMING THE NOSE DOWN, HE WAS ACTUALLY TRIMMING IT UP. THE LOCATION OF THE DECMay 14, 2001 · Cessna U206F · Placards and MarkingsSDR AUS20010426Fitting · cracked(AUS) LT AFT TAILPLANE ATTACHMENT REINFORCEMENT CRACKED.May 7, 2001 · Cessna U206F · Horizontal Stabilizer, Attach FittingsSDR 20010423CW016Line · leakingFOUND FUEL RETURN LINE LEAKING THROUGH THE STEEL BRAID. HOSE IS LESS THAN 3 YEARS OLD, WITH NO VISIBLE DAMAGE. EVEN THOUGH THIS TYPE HOSE IS APPROVED FOR FUEL, AVIATION FUEL SEEMS TO DETERIOATE IT. HOSE HAS STEEL BRAID EXTERIOR.Apr 4, 2001 · N5VA · Cessna U206F · Aircraft Fuel Distribution SystemSDR AU010132Exhaust Valve · leaking(AUS) ENGINE EXHAUST VALVE LEAKING.Feb 2, 2001 · Cessna U206F · Reciprocating Engine Cylinder SectionSDR AUS20010433Flap Track · corroded(AUS) FLAP TRACKS CONTAINED EXFOLIATION AND INTERGRANNULAR CORROSIONLOCATED IN THE FORWARD END OF THE LOWER SLOT.Jan 15, 2001 · Cessna U206F · Trailing Edge FlapsSDR AUS20010432Bulkhead · cracked(AUS) HORIZONTAL STABILISER ATTACHMENT BULKHEAD CRACKED THROUGH TOP RIVET HOLE. CRACK LENGTH 19.05MM (0.75IN).Jan 15, 2001 · Cessna U206F · Fuselage Main, BulkheadSDR AUS20010431Seat Track · cracked(AUS) SEAT TRACKS CRACKED THROUGH STOP PIN HOLES.Jan 15, 2001 · Cessna U206F · Fuselage, Seat/Cargo Attach FittingsSDR AU001071Engine · overspeed(AUS) ENGINE OVERSPED IN EXCESS OF 3,300 RPM. (X)Nov 8, 2000 · Cessna U206F · Engine (Reciprocating)SDR AU001050Switch · failed(AUS) LANDING GEAR LIMIT MICROSWITCHES PN 1SE1-3 FAILED. THE RUBBER INSERT HOLDING THE PLUNGER AND SEALING THE SWITCH HAD EXPANDED AND DISINTEGRATED APPROXIMATELY EIGHT TO TWELVE HOURS AFTER LUBRICATION WITH LPS1 LUBRICANT AS SPECIFIED IN THE 3500A FLOAT SERVINov 1, 2000 · Cessna U206F · Landing Gear Position and WarningSDR 20001120SH061Casting · brokenCASTING BROKE BETWEEN MOUNTING PAD AND BARREL. (X)Oct 27, 2000 · N8515W · Cessna U206F · Vacuum Distribution SystemSDR AU000947Bulkhead · cracked(AUS) FORWARD TAIL BULKHEAD CRACKED IN THE AREA OF THE HORIZONTAL STABILIZER ATTACHMENT POINT. (X)Sep 29, 2000 · Cessna U206F · Fuselage Main, BulkheadSDR AU000821Torque Tube · corroded(AUS) ELEVATOR TORQUE TUBE CRACKED ON INBOARD END. DISASSEMBLY FOUND SIGNIFICANT CORROSION BETWEEN THE TORQUE TUBE AND THE SPAR MOUNTING BRACKET. (X)Sep 11, 2000 · Cessna U206F · Elevator, Spar/RibSDR 20001109SH010Ferrule · crackedPROPELLER SENT FOR REPAIR OF OIL LEAK. AFTER INVESTIGATION OF THE PROPELLER AND DISASSEMBLY, FOUND THE OIL LEAK OCCURRED BECAUSE ONE BLADE FERRULE HAD BEEN CRACKED IN THE BEARING AREA. (X)Sep 4, 2000 · Cessna U206F · Propeller AssemblySDR AU000743Control Cable · separated(AUS) PROPELLER CONTROL CABLE ROD END NOT CONNECTED TO CSU. BOLT MISSING. (X)Sep 1, 2000 · Cessna U206F · Propeller Controlling SystemSDR AU000678Spring · broken(AUS) ENGINE STARTER/ ADAPTER CLUTCH SPRING BROKEN EIGHT COILS FROM THE ATTACHMENT POINT TO THE CLUTCH DRUM. (X)Sep 1, 2000 · Cessna U206F · Reciprocating Engine Rear SectionSDR 20000817SH016Camshaft · making metalFERROUS MATERIAL FOUND IN OIL FILTER. ENGINE DIS-ASSEMBLED, PROBLEM FOUND TO BE FAILED CAMSHAFT AND LIFTER BODIES. (X)Aug 17, 2000 · N7138Q · Cessna U206F · Reciprocating Engine Power SectionSDR CA000906008Engine · failed(CAN) PILOT REPORTED DURING CRUISE HE HAD BRIEF VIBRATION FOLLOWED BY A LOSS OF OIL PRESSURE AND IMMEDIATE ENGINE FAILURE. AN UNEVENTFUL FORCED LANDING WAS CONDUCTED ON A LAKE 40 NAUTICAL MILES NORTHWEST OF RANKIN INLET, NUNAVUT. MAINTENANCE FOUND THE FRONT Aug 16, 2000 · Cessna U206F · Reciprocating Engine Power SectionSDR CA001122020Throttle Cable · seized(CAN) A NEW THROTTLE CABLE RECEIVED FROM CESSNA WAS INSTALLED ON THE AIRCRAFT BUT SEIZED UP WHEN THE CABLE WAS FLEXED TO ALLOW HOOKUP TO THE THROTTLE CABLE. ANOTHER NEW CABLE FROM CESSNA WAS TRIED WITH THE SAME RESULT.A THROTTLE CABLE MADE BY MCFARLANE MCC2995Jul 7, 2000 · Cessna U206F · Power LeverSDR 20000817SH020Crankshaft · inadequatePER TCM MSB 00-5B, CRANKSHAFT WAS REJECTED BY TELEDYNE CONTINENTAL MOTORS. (X)Jun 6, 2000 · N61599 · Cessna U206F · Reciprocating Engine Power SectionSDR AU000423Trim Tab · distorted(AUS) RIGHT ELEVATOR TRIM TAB DISTORTED, SPLIT AND BULGED. INVESTIGATION FOUND THAT THE CORE HAD BEEN FILLED WITH EXPANDABLE FOAM WHICH HAD CONTINUED TO EXPAND AFTER FILLING THE AVAILABLE SPACE. UNAPPROVED PART.May 31, 2000 · Cessna U206F · Elevator, Tab StructureSDR AU000403Wire · shorted(AUS) FIRE UNDER FUSELAGE FLOOR IN RT FUEL COLLECTOR TANK COMPARTMENT. EXTENSIVE DAMAGE CAUSED TO WIRING LOOM LOCATED BETWEEN THE COLLECTOR TANK AND THE FLOOR PANEL. SUSPECT CAUSED BY SPARKS FROM THE RIGHT EXHAUST TAILPIPE IGNITING LEAKING BOOST PUMP FUEL ANMay 25, 2000 · Cessna U206F · Electrical Power System WiringSDR CA000614024Handle · damaged(CAN) PILOT CLOSED DOOR WITH HANDLE SELECTED TO THE CLOSED POSITION, HOWEVER, HANDLE WAS PARTIAL STRIP ON INSIDE GEARING, AND DOOR WAS NOT FULLY LOCKED. MAINTENANCE REPLACED DOOR HANDLE WITH SERVICEABLE HANDLE AND RETURNED THE AIRCRAFT TO SERVICE.May 5, 2000 · Cessna U206F · Passenger/Crew DoorsSDR AU000356Bulkhead · cracked(AUS) FORWARD DOORPOST BULKHEAD CRACKED IN RELIEF HOLE. CRACK LENGTH 12.7 MM (0.5 INCH). FOUND DURING INSPECTION IAW AD/C206/48.Apr 1, 2000 · Cessna U206F · Fuselage Main, BulkheadSDR CA000306020Cylinder · cracked(CAN) CYLINDER CRACKED AT INTAKE PORT NR 5 CYLINDER.Mar 6, 2000 · Cessna U206F · Reciprocating Engine Cylinder SectionSDR CA000306012Cylinder · cracked(CAN) EXHAUST PORT CRACK VISIBLE ON OUTSIDE OF CYLINDER.Mar 6, 2000 · Cessna U206F · Reciprocating Engine Cylinder SectionSDR 2000ZZZX831Impulse Coupling · failedTHE IMPULSE COUPLING ENGAGES ONLY 1 OUT OF 5 TIMES WHEN PROPELLER IS TURNED BY HAND. THE SPRING WHICH HOLDS THE PAWL OUT TO ENGAGE IMPULSE COUPLING HAS NOT BROKEN BUT HAS TOTALY LOST ITS SPRING EFFECT.Feb 26, 2000 · N123TM · Cessna U206F · Magneto/DistributorSDR CA991230012Plug · missing(CAN) TWO LOCKING EXPANSION PLUGS FOR EACH BLADE ALL WERE FOUND NOT INSTALLED. LOCKING EXPANSION PLUGS ARE USED TO LOCK THE BLADES TO THE HUB . THIS IS AN O/H OVERSIGHT AND A MAINTENANCE ISSUE.Dec 10, 1999 · Cessna U206F · Propeller Hub SectionSDR CA991230009Hub · cracked(CAN) FOUND CRACK IN DICATION USING EDDY CURRENT ON HUB SOCKET. NR 1 AND NR 2 HUB REPLACED.Dec 10, 1999 · Cessna U206F · Propeller Hub SectionSDR CA991230008Pin · corroded(CAN) DEEP CORROSION PITS, ACTUATING PINS REPLACED.Dec 10, 1999 · Cessna U206F · Propeller Blade SectionSDR 99ZZZX4546Camshaft · making metalFERROUS MATERIAL FOUND IN OIL FILTER. ENGINE DISASSEMBLED, PROBLEM FOUND TO BE FAILED CAMSHAFT AND LIFTER BODIES.Nov 22, 1999 · N7318Q · Cessna U206F · Reciprocating Engine Power SectionSDR CA991208079Impulse Coupling · worn(CAN) IMPULSE COUPLING WORN PAST LIMITS. DISTRIBUTOR DRIVE GEAR BUSHES WEAR WAS EXCESSIVE.Nov 10, 1999 · Cessna U206F · Magneto/DistributorSDR AU990933Seat Track · worn(AUS) LEFT SEAT RAIL WORN BEYOND LIMITS.Aug 3, 1999 · Cessna U206F · Fuselage, Seat/Cargo Attach Fittings
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