# Service difficulty reports: Cessna TU206G A list on [Cessna TU206G](https://openairdocs.org/model/cessna-tu206g.md). Newest first. General aviation reporting is voluntary. Page 1 of 3 · 123 reports - [SDR 2025FA0000673](https://openairdocs.org/sdr/2025FA0000673.md): Wire · damaged · Sep 30, 2025 · Cessna TU206G · Engine Fuel System Wiring > DURING FLIGHT, PILOT REPORTED FUEL FLOW DISCREPANCY AND ENGINE ROUGHNESS AND RETUNRED TO BASE FOR A PRECAUTIONARY, ALBEIT IF VERY STRESSFUL, LANDING. UPON INSPECTION OF THE FUEL FLOW SENSOR ( PART OF THE JPI 930 ENGINE INSTRUMENTAION - STC SA01435SA) IT WAS - [SDR 2023FA0000000](https://openairdocs.org/sdr/2023FA0000000.md): Contactor · failed · Jan 2, 2023 · Cessna TU206G · Magneto/Distributor > 0.0 TSMO OVH MAG INSTALLED ON 0.0 TSMO IO550F AT ENG CHANGE. TEST FLIGHTS AND GROUND RUNS ALL OK. 28.7 HOURS LATER MAG WAS REMOVED FOR MAJOR ROUGHNESS, INABILITY TO IDLE, AND MULTIPLE CYLINDERS WITH ERRANT TEMPERATURES. POINT CONTACTOR PAD IN STAMPED ARM WAS - [SDR CA190402009](https://openairdocs.org/sdr/CA190402009.md): Bearing Race · corroded · Mar 28, 2019 · Cessna TU206G · Propeller System > (CAN) ENGINE COULD NOT ATTAIN TAKE OFF RPM. PROPELLER WAS REMOVED AND BENCH TESTED. IT WAS FOUND THAT IT WOULD NOT CYCLE INTO FINE PITCH. UPON DISASSEMBLY IT WAS FOUND THAT THE BEARING RACES, RETAINERS AND BALLS WERE SEVERELY CORRODED. PROPELLER WAS REASSEMBLE - [SDR 2019FA0000168](https://openairdocs.org/sdr/2019FA0000168.md): Nut · defective · Mar 15, 2019 · N7PCMO · Cessna TU206G · Propeller Governor > ATTACHMENT NUTS SUPPLIED WITH ATTACHMENT KIT (P/N KPL2001) FAILED BEFORE REACHING RECOMMENDED TORQUE (180-220 IN LBS). THE NUTS SEEM VERY SOFT. - [SDR 4DSR2018081000002](https://openairdocs.org/sdr/4DSR2018081000002.md): Fitting · cracked · Aug 8, 2018 · N243DR · Cessna TU206G · Fuselage, Landing Gear Attach Fittings > DURING AN ANNUAL INSPECTION, AFTER REMOVAL OF THE RT MAIN GEAR TO FUSELAGE FAIRING FOR INSPECTION, FOUND THE GEAR ATTACHMENT OUTBOARD FITTING CRACKED. THE CRACK WAS IN THE WEB OR BODY OF THE PART AND NOT EMANATING FROM AN EDGE. REQUIRED MAGNIFICATION TO CONFIR - [SDR 4DSR2018081000001](https://openairdocs.org/sdr/4DSR2018081000001.md): Line · chafed · Aug 8, 2018 · N243DR · Cessna TU206G · Landing Gear Brake System > DURING ANNUAL INSPECTION, AFTER REMOVAL OF THE RIGHT MAIN GEAR TO FUSELAGE FAIRING, FOUND THE ALUMINUM BRAKE LINE SEVERELY GOUGED AND CHAFED. CHAFING ON THE FUSELAGE SKIN CUTOUT WHERE THE LEAF SPRING-TYPE GEAR PASSED THROUGH. THE BRAKE LINE WALL WAS OVER 90% - [SDR M2LA201806221001](https://openairdocs.org/sdr/M2LA201806221001.md): Cylinder · cracked · Jun 11, 2018 · N206WD · Cessna TU206G · Reciprocating Engine Cylinder Section > ACFT STARTED AND RUNNING FOR A TRAINING FLIGHT, PILOTS NOTICED A VIBRATION OF THE ENGINE AND NO CYLINDER HEAD TEMP OR EXHAUST TEMP ON NR 6 CYLINDER IAW THE ENGINE MONITOR. PILOTS SHUT ENGINE DOWN AND NOTIFIED MAINTENANCE. AFTER INSPECTION OF CYLINDER NR 6, B - [SDR 2017FA0000401](https://openairdocs.org/sdr/2017FA0000401.md): Post · cracked · Feb 27, 2017 · N9438M · Cessna TU206G · Wing Main, Frame Structure > DURING LOWER FWD DOOR POST AND STRUT FITTING INSPECTION REQUIRED BY SERVICE BULLETIN SEB935R1, FOUND A CRACK IN RADIUS OF CORNER ADJACENT TO AND DISAPPEARING UNDER THE STRUT FITTING. - [SDR 2016FA0000539](https://openairdocs.org/sdr/2016FA0000539.md): Belt · sheared · Oct 26, 2016 · N602MB · Cessna TU206G · Electrical Power System > SQUEALING SOUND AT ENGINE START VOLTMETER SHOWING DISCHARGE. ALTERNATOR BELT WAS SHEARED. - [SDR 2015FA0000364](https://openairdocs.org/sdr/2015FA0000364.md): Master Cylinder · cracked · Aug 5, 2015 · N206PD · Cessna TU206G · Master Cylinder/Brake Valve > UPON LANDING, PILOT LOST RT BRAKE PEDAL ACTUATION AS WELL AS RT BRAKE CAPABILITIES. INITIAL GVI-VISUAL INVESTIGATION REVEALED RT BRAKE MASTER CYLINDER PISTON ROD PN 0541143, BROKEN AT BASE BELOW CLEVIS CHECK NUT PN 0541140. UPON DVI-VISUAL INSPECTION THE CL - [SDR CA140714002](https://openairdocs.org/sdr/CA140714002.md): Oil System · malfunctioned · Jul 11, 2014 · Cessna TU206G · Engine (Reciprocating) > (CAN) ENGINE REMOVED FOR TEARDOWN AND INSPECTION DUE PERSISTENT LOW OIL PRESSURE, HIGH OIL TEMPERATURE. AIRCRAFT REMOVED FROM SERVICE. - [SDR CA130930006](https://openairdocs.org/sdr/CA130930006.md): Cylinder · cracked · Sep 26, 2013 · Cessna TU206G · Reciprocating Engine Cylinder Section > (CAN) JUST AFTER TAKEOFF, PILOT HEARD A LOUD BANG. PARTIAL POWER LOSS WAS NOTED AND THE ACFT RETURNED TO DEPARTURE. VISUAL INSPECTION HAS SHOWN SUBSTANTIAL OIL LOSS. THE NR 5 CYLINDER WAS FOUND TO HAVE CRACKED AND SEPARATED. - [SDR WU52013F00000](https://openairdocs.org/sdr/WU52013F00000.md): Drag Link · broken · Aug 22, 2013 · N206GA · Cessna TU206G · Nose/Tail Landing Gear Strut/Axle > LINK-DRAG BROKEN AT WELDED JOINT. - [SDR CA130809002](https://openairdocs.org/sdr/CA130809002.md): Spar · cracked · Aug 9, 2013 · Cessna TU206G · Elevator, Spar/Rib > (CAN) WHILE COMPLYING WITH SB SEB85-7, REV 3, TO REPLACE RT ELEVATOR TRIM TAB AND LT & RT T/E WEDGES DUE TO THE FOAM CORES WERE SATURATED, IT WAS DISCOVERED THAT THE AFT SPAR OF THE ELEVATOR, ITSELF, WAS CRACKED. - [SDR YN8R201301240001](https://openairdocs.org/sdr/YN8R201301240001.md): Cover · cracked · Jan 24, 2013 · N778CW · Cessna TU206G · Wheel/Ski/Float > DURING INSPECTION OF FLOATS, FOUND NUMEROUS CRACKS IN COVER REINFORCEMENTS ON FLOAT. CRACKS WERE AT THE OUTER ATTACHMENT THROUGH THE RIVET HOLES. UNKNOWN TIME ON FLOATS, AT LEAST 1200 HRS. THIS FLOAT HAD FOUR TOTAL CRACKED REINFORCEMENTS, BOTH LARGE AND SMA - [SDR YN8R01242013RHBH](https://openairdocs.org/sdr/YN8R01242013RHBH.md): Reinforcement · cracked · Jan 24, 2013 · N778CW · Cessna TU206G · Wheel/Ski/Float > DURING INSPECTION OF FLOATS, FOUND NUMEROUS CRACKS IN COVER REINFORCEMENTS ON FLOAT. CRACKS WERE AT THE OUTER ATTACHMENT THROUGH THE RIVET HOLES. UNKNOWN TIME ON FLOATS, AT LEAST 1200 HRS. THIS FLOAT HAD 6 TOTAL CRACKED REINFORCEMENTS, BOTH LARGE AND SMALL - [SDR 2012FA0000522](https://openairdocs.org/sdr/2012FA0000522.md): Attach Fitting · cracked · Aug 1, 2012 · N602MB · Cessna TU206G · Fuselage, Landing Gear Attach Fittings > DURING AN ANNNUAL INSPECTION, FOUND A.7500" CRACK IN THE LT MAIN LANDING GEAR OUTBOARD ATTACH FITTING AS VIEWED THROUGH A FLOOR ACCESS PANEL. THE CRACK IS IN THE RADIUS OF THE FITTING AFT AND BELOW THE MLG SPRING. FOUND NO HISTORY OF A HARD LANDING. - [SDR 2012FA0000375](https://openairdocs.org/sdr/2012FA0000375.md): Wire · burned · Jun 6, 2012 · N136Z · Cessna TU206G · Electrical Power System Wiring > PILOT REPORTED SMOKE IN COCKPIT AND TERMINATED FLIGHT. FOUND WIRE PB7 FROM FIELD CIRCUT BREAKER TO ALTERNATOR SWITCH BURNED AND MELTED INTO WIRE BUNDLE. MELTING AND HEAT DAMAGED APPROX 10-12 WIRES IN THE BUNDLE. VOLTAGE REGULATOR FAILURE CAUSED THE 24 GA W - [SDR 2012FA0000157](https://openairdocs.org/sdr/2012FA0000157.md): Bolt · loose · Feb 16, 2012 · N232MT · Cessna TU206G · DC Generator-Alternator > DURING TROUBLESHOOTING FOR ALTERNATOR NOISE, INSPECTED ALTERNATOR AND FOUND BOLT LOOSE INSIDE ALTERNATOR CASE. REMOVED ALTERNATOR AND DISASSEMBLED, FOUND DIODE RECTIFIER BRIDGE BOLT HAD BACKED OUT AND HAD CONTACTED THE ROTOR, BENDING THE BOLT AND ELONGATING T - [SDR 2012FA0000068](https://openairdocs.org/sdr/2012FA0000068.md): Governor · disintegrated · Jan 25, 2012 · Cessna TU206G · Propeller Governor > PROP GOVERNOR BEARING IN THE IDLER PART OF THE OIL PUMP DISINTEGRATED. - [SDR 2011FA0000270](https://openairdocs.org/sdr/2011FA0000270.md): Nut · loose · Apr 11, 2011 · Cessna TU206G · Reciprocating Engine Oil System > SHORTLY AFTER INSTALLATION, THE ENG BEGAN AN OIL LEAK, UP FRONT ON THE RT SIDE NEAR THE OIL COOLER. OIL COOLER WAS REMOVED, FOUND THAT THE NUTS THAT HOLD THE OIL COOLER ADAPTER WERE LOOSE AND COULD BE REMOVED BY HAND. THIS ENGINE HAD 39.1 HOURS TSN ON IT WHE - [SDR 2010FA0001222](https://openairdocs.org/sdr/2010FA0001222.md): Magneto · failed · Nov 4, 2010 · N7347N · Cessna TU206G · Magneto/Distributor > THIS O/H MAGNETO WAS INSTALLED ON THE ACFT IAW MM AND STANDARD PRACTICES, TIMED TO ENG IAW MM. THE ENGINE WAS RUNUP IAW POH AND THE MAG CHECK WAS SATISFACTORY. THE ENGINE WAS SHUTDOWN AND COWLING INSTALLED. AT THE NEXT ENGINE STARE, THE LT MAGNETO FAILED TO - [SDR 2011FA0000153](https://openairdocs.org/sdr/2011FA0000153.md): Throttle Control · loose · Feb 10, 2010 · Cessna TU206G · Power Lever > THROTTLE CONTROL ASSEMBLY - ON AFT END OF THE CONTROL, THE PILOT END OF THE PUSH/PULL CONTROL - THE THREADED ALUMINUM ATTACH FITTING IS LOOSE ON THE STEEL SLEEVE, NORMALLY A TIGHT FIT. ON THE FWD END OF THE CONTROL - THE ENGINE ATTACHMENT END, THE SLEEVE IS - [SDR CA100114004](https://openairdocs.org/sdr/CA100114004.md): Alternator · failed · Jan 13, 2010 · Cessna TU206G · DC Generator-Alternator > (CAN) ALTERNATOR FAILED DURING FLIGHT. ELECTRICAL POWER LOSS INDICATED TO CREW. CREW RETURNED FOR LANDING AT CYTZ. (TC NR 20100114004) - [SDR 2009FA0000761](https://openairdocs.org/sdr/2009FA0000761.md): Ignition Switch · failed · Sep 4, 2009 · N602MB · Cessna TU206G · Ignition Switching > IGNITION SWITCH FAILED TO SHUT-OFF MAGENTO DURING A PRE-FLIGHT MAGNETO CHECK AND FAILED AT 1201.1 HOURS SINCE NEW. THE REQUIRED DIODE ON THE STARTER SOLENOID WAS INSTALLED PER THE AD/SERVICE BULLETIN SO THIS SWITCH SHOULD NOT HAVE FAILED AT 1201.1 HOURS. - [SDR 2009FA0000712](https://openairdocs.org/sdr/2009FA0000712.md): Cylinder · peeling · Jul 13, 2009 · N756MR · Cessna TU206G · Reciprocating Engine Cylinder Section > CYLINDER BARREL PEELING FOUND AFTER A LOW COMPRESSION TEST. THE BARREL PEELED IN AN AREA APPROX 2 INCHES WIDE. THE METAL CONTAMINATED THE ENG LUBRICATION SYS REQUIRING A COMPLETE TEARDOWN OF THE ENG. THIS CYL WAS INSTALLED AT ENG O/H ON 5/30/2009. (K) - [SDR CA090707002](https://openairdocs.org/sdr/CA090707002.md): Aneroid · failed · Jun 10, 2009 · Cessna TU206G · Engine Fuel Pump > (CAN) FUEL PUMP ANEROID FAILED CAUSING ERRATIC FUEL FLOWS. - [SDR M2L2009F00000](https://openairdocs.org/sdr/M2L2009F00000.md): Hinge Bracket · broken · May 11, 2009 · N7520N · Cessna TU206G · Ailerons > THIS PART HAS 2 SMALL 90 DEGREE ANGLES AT EITHER SIDE BOTTOM. THEY HAVE LITTLE OR NO ACTUAL STRENGTH OTHER THAN TO PREVENT THE LOWER WING SKIN FROM NOT BEING SECURED. RT AILERON OTBD HINGE BRACKET. (K) - [SDR M2L2009F00001](https://openairdocs.org/sdr/M2L2009F00001.md): Hinge Bracket · broken · May 7, 2009 · N7520N · Cessna TU206G · Wing, Control Surface Attach Fittings > THIS PART HAD 1 OR 2, 90 DEGREE ANGLES ON THE BOTTOM SIDE, CRACKED. THIS WAS CAUSED MOST LIKELY FROM YEARS OF FATIGUE. DON`T THINK THIS WOULD HAVE CAUSED AN AIRWORTHINESS CONCERN AS IT DOES NOT APPEAR TO HAVE WEAKENED THE ATTACHMENT OF THE HINGE BRACKET. TH - [SDR 2009FA0000198](https://openairdocs.org/sdr/2009FA0000198.md): Cylinder · cracked · Mar 10, 2009 · N899RC · Cessna TU206G · Reciprocating Engine Cylinder Section > NR 4 CYLINDER BARREL CRACKED APPROX. 1INCH FROM THE TOP OF THE BARREL AND ALMOST.7500 INCH OF THE WAY AROUND THE INSIDE CIRCUMFERENCE. THIS WAS A NEW ECI FREEDOM STEEL BARREL CYLINDER. THE CYLINDER HAS TEST CELL AND GROUND RUN TIME ONLY, WHEN THE MECHANIC N - [SDR 2008FA0000565](https://openairdocs.org/sdr/2008FA0000565.md): Intake Duct · cracked · Aug 13, 2008 · N602MB · Cessna TU206G · Engine Air Intake System > MFG SUPPLIED ENGINE INTAKE DUCT BEFORE THE AIR FILTER IS SUBJECT TO CRACKING IN MULTIPLE LOCATIONS. THIS PARTICULAR AC AND ANOTHER IDENTICAL MODEL AC THIS FACILITY MAINTAINS, HAVE BEEN CONVERTED TO ANOTHER ENGINE AFTER THE STC CONVERSION. CRACKING PROBLEM HA - [SDR 2008FA0000554](https://openairdocs.org/sdr/2008FA0000554.md): Intake Duct · cracked · Aug 13, 2008 · N602MB · Cessna TU206G · Engine Air Intake System > MANUFACTURER SUPPLIED ENG INTAKE DUCT BEFORE THE AIR FILTER IS SUBJECT TO CRACKING IN MULTIPLE LOCATIONS. THIS PARTICULAR ACFT AND ANOTHER IDENTICAL MODEL ACFT THIS FACILITY MAINTAINS HAVE BEEN CONVERTED TO AN IO-550-F ENG. AFTER THE STC CONVERSION, THE CRAC - [SDR 243DR1](https://openairdocs.org/sdr/243DR1.md): Servo · misinstalled · Nov 21, 2007 · N243DR · Cessna TU206G · Autopilot Trim Servo > WHILE UNDERGOING A SCHEDULED INSPECTION, MECHANIC FOUND ELEVATOR TRIM SYS WAS MISRIGGED. TRAVEL LIMITS WERE NOT CORRECT AND WERE ACTUALLY RIGGED OPPOSITE WITH REGARDS TO MAX TRAVEL UP/DOWN. TRAVEL LIMITS IN MM NR D2070-3-13 FIGURE 1-1 WERE MISINTERPRETED, MFG - [SDR CA070119010](https://openairdocs.org/sdr/CA070119010.md): Spar · failed · Jan 16, 2007 · Cessna TU206G · Wing Spar > (CAN) DURING REPLACEMENT OF LOWER OB SKIN, EDGE DISTANCE OF RIVETS THROUGH LOWER FLANGE LESS THAN MINIMUM ALLOWED IN 32 PLACES FROM STAT. 100.0 TO STAT. 154.00 REPLACEMENT OF PARTS REQUIRED TO REPAIR PROBLEM. (TC NR 20070119010) - [SDR CA070119009](https://openairdocs.org/sdr/CA070119009.md): Spar · failed · Jan 16, 2007 · Cessna TU206G · Wing Spar > (CAN) EDGE DISTANCE OF RIVETS ON LOWER FLANGE LESS THAN MINIMUM ALLOWED. REPLACEMENT OF PART REQUIRED TO REPAIR PROBLEM. (TC NR 20070119009) - [SDR CA061218014](https://openairdocs.org/sdr/CA061218014.md): Seal · leaking · Dec 18, 2006 · Cessna TU206G · Propeller Blade Section > (CAN) BLADE GREASE SEAL FAILED. GREASE LEAVING HUB. PROP REMOVED AND SENT TO REPAIR FACILITY WHERE NEW SEALS WERE INSTALLED. PROP REINSTALLED AND A/C SERVICEABLE (TC NR 20061218014). - [SDR 2006ADP09001](https://openairdocs.org/sdr/2006ADP09001.md): Wire Harness · cracked · Sep 1, 2006 · Cessna TU206G · Ignition System Wiring > DURING INSPECTION ON A NEW, LOW TIME ENGINE, THE MT NOTICED A RATHER LARGE CRACK IN THE RT IGNITION HARNESS COVER, WHERE THE HARNESS ATTACHES TO THE MAGNETO. AFTER LOOKING A LITTLE CLOSER, IT IS CLEAR THAT THE CRACK WAS THERE PRIOR TO OVERHAUL AND PAINTING. - [SDR MPVMANIFOLD](https://openairdocs.org/sdr/MPVMANIFOLD.md): Fuel Divider · leaking · Mar 28, 2006 · Cessna TU206G · Fuel Divider > FUEL MANIFOLD VALVE IS LEAKING FROM THE VENT PORT. - [SDR 2006ADP001](https://openairdocs.org/sdr/2006ADP001.md): Cylinder · cracked · Feb 24, 2006 · Cessna TU206G · Reciprocating Engine Cylinder Section > ALL SIX CYLINDERS HAVE CRACKS IN THE SAME AREA JUST ABOVE THE TOP SPARK PLUG HOLE. - [SDR MAFALT4](https://openairdocs.org/sdr/MAFALT4.md): Rotor · failed · Sep 2, 2005 · Cessna TU206G · AC Generation System > ELECTROSYSTEM WOES CONTINUE, WITH ANOTHER ROTOR GOING BAD. DETAILS: M/N DOFF10300BR S/N B110413 WITH A TS0:1095.1 ON THE ALTERNATOR. THE ROTOR WAS CHANGED 3 DIFFERENT TIMES ON THIS ALTERNATOR AND IT RAN ON FOUR DIFFERENT A/C IN IT'S LIFE HERE. THIS LAST RO - [SDR GAJ2005F00001](https://openairdocs.org/sdr/GAJ2005F00001.md): Control Cable · frozen · Aug 15, 2005 · N7537N · Cessna TU206G · Mixture Control > 3/25/04, HOBBS 3218.1, TTAF 9745.1, REMOVED AND REINSTALLED ENGINE, THROTTLE, MISTURE AND PROP CONTROLS. 7/22/04, HOBBS 3417.7, TTAF 9944.0, VERNIER CONTROL RELEASE BUTTON FROZE IN PUSHED POSITION, REMOVED MIXTURE CONTROL CABLE AND REPLACED WITH NEW. 8/12/05 - [SDR DUKESPUMPMPG](https://openairdocs.org/sdr/DUKESPUMPMPG.md): Pump · leaking · Apr 5, 2005 · Cessna TU206G · Engine Fuel Pump > PUMP IS LEAKING AT THE SEAL AT THE BASE OF THE PUMP, NEAR DRAIN PIPE. - [SDR DUKESPUMPPKMP](https://openairdocs.org/sdr/DUKESPUMPPKMP.md): Pump · leaking · Apr 5, 2005 · Cessna TU206G · Engine Fuel Pump > PUMP IS LEAKING AT THE SEAL AT THE BASE OF THE PUMP-NEAR/AT DRAIN PIPE. - [SDR MAFALT3](https://openairdocs.org/sdr/MAFALT3.md): Wire · open · Apr 4, 2005 · Cessna TU206G · Electrical Power System Wiring > OPEN FIELD WINDING AT SLIP RING (WIRE BROKEN AT SOLDER JOINT). - [SDR MAFALT2](https://openairdocs.org/sdr/MAFALT2.md): Alternator · open · Apr 4, 2005 · Cessna TU206G · DC Generating System > OPEN FIELD WINDING AT SLIP RING (WIRE BROKEN AT SOLDER JOINT). - [SDR MAFALT1](https://openairdocs.org/sdr/MAFALT1.md): Alternator · open · Apr 4, 2005 · Cessna TU206G · DC Generating System > OPEN FIELD WINDING. - [SDR CA050324006](https://openairdocs.org/sdr/CA050324006.md): Counterweight · failed · Mar 15, 2005 · Cessna TU206G · Reciprocating Engine Power Section > (CAN) ROLLER RETAINER AND SNAP RING CAME OUT OF CLUT, RELEASING ROLLER IN 5TH ORDER CWT. (NO DAMAGE TO PARTS, POSSIBILITY WAS NOT INSTALLED CORRECTLY.) ROLLER MIGRATED TO REAR OF ENGINE AND JAMMED BETWEEN 6TH ORDER CWT AND ENGINE CASE STOPPING ENGINE. CRANKSH - [SDR TCMMAQ2](https://openairdocs.org/sdr/TCMMAQ2.md): Magneto · deformed · Jan 25, 2005 · Cessna TU206G · Magneto/Distributor > COIL WEDGES OVERDRIVEN TO THE POINT OF CONTACT WITH COIL, CRACKING THE INSULATION. - [SDR TCMMAQ1](https://openairdocs.org/sdr/TCMMAQ1.md): Magneto · deformed · Jan 25, 2005 · Cessna TU206G · Magneto/Distributor > COIL WEDGES OVERDRIVEN TO THE POINT OF CONTACT WITH COIL, CRACKING THE INSULATION. - [SDR M2L2005F00000](https://openairdocs.org/sdr/M2L2005F00000.md): Fitting · cracked · Sep 15, 2004 · N7520N · Cessna TU206G · Main Landing Gear > THIS IS A RESULT OF HARD USE FOR MANY YEAR IN BACK COUNTRY. THE CRACKS WERE FOUND AT A PHASE II INSPECTION. THESE PARTS HAVE SERVED THEIR USEFUL LIFE AND SHOULD BE CHANGED WITH THIS MUCH TIME AND HARD USE. LANDING GEAR FITTINGS, LT AND RT, OB. (NM1120040361 Next page: https://openairdocs.org/model/cessna-tu206g/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = 'TU206G' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/cessna-tu206g/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.