# Service difficulty reports: Cessna 206H

A list on [Cessna 206H](https://openairdocs.org/model/cessna-206h.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 86 reports

- [SDR 2024FA0000575](https://openairdocs.org/sdr/2024FA0000575.md): Magneto · failed · Aug 7, 2024 · N246N · Cessna 206H · Magneto/Distributor
  > MAGNETO FAILED
- [SDR 2024FA0000573](https://openairdocs.org/sdr/2024FA0000573.md): Magneto · failed · Aug 6, 2024 · N246N · Cessna 206H · Magneto/Distributor
  > MAGNETO FAILED
- [SDR 2024FA0000578](https://openairdocs.org/sdr/2024FA0000578.md): Magneto · failed · May 20, 2024 · N6188Q · Cessna 206H · Magneto/Distributor
  > MAGNETO FAILED
- [SDR 2024FA0000577](https://openairdocs.org/sdr/2024FA0000577.md): Magneto · failed · Mar 14, 2024 · N234U · Cessna 206H · Magneto/Distributor
  > MAGNETO FAILED
- [SDR 2024FA0000576](https://openairdocs.org/sdr/2024FA0000576.md): Magneto · failed · Mar 6, 2024 · N234U · Cessna 206H · Magneto/Distributor
  > MAGNETO FAILED
- [SDR 2024FA0000572](https://openairdocs.org/sdr/2024FA0000572.md): Magneto · failed · Jan 29, 2024 · N6188Q · Cessna 206H · Magneto/Distributor
  > MAGNETO FAILED
- [SDR 2024FA0000078](https://openairdocs.org/sdr/2024FA0000078.md): Blade · loose · Jan 29, 2024 · N809HW · Cessna 206H · Propeller Blade Section
  > AFTER A FLIGHT A MECHANIC NOTICED THE SNAP RING AT THE BASE OF ONE OF THE PROPELLER BLADES WAS NOT IN ITS GROOVE AT THE BLADE ROOT BUT WAS DISLODGED AND WEDGED AGAINST THE SPINNER. THE BLADE WAS FOUND TO BE LOOSE IN THE HUB AND COULD BE MOVED AT THE BLADE TIP
- [SDR 2024FA0000571](https://openairdocs.org/sdr/2024FA0000571.md): Magneto · failed · Jan 24, 2024 · N246U · Cessna 206H · Magneto/Distributor
  > MAGNETO FAILED
- [SDR 2024FA0000570](https://openairdocs.org/sdr/2024FA0000570.md): Magneto · failed · Dec 27, 2023 · N234U · Cessna 206H · Magneto/Distributor
  > MAGNETO FAILED
- [SDR 2018FA0000345](https://openairdocs.org/sdr/2018FA0000345.md): Intake Valve · broken · Aug 3, 2018 · N9536F · Cessna 206H · Reciprocating Engine Power Section
  > ENGINE LOST POWER IN FLIGHT, RESULTING IN AN EMERGENCY LANDING. INSPECTION REVEALED THAT THE NUMBER 1 CYLINDER INTAKE VALVE FAILED, DAMAGING THE PISTON.
- [SDR XGKR20171030](https://openairdocs.org/sdr/XGKR20171030.md): Display · intermittent · Oct 30, 2017 · N5229C · Cessna 206H · Global Positioning System
  > INTERMITTENT HEADING FAILURE IN FLIGHT.
- [SDR 2017FA0000289](https://openairdocs.org/sdr/2017FA0000289.md): Pump · sheared · Jul 18, 2017 · N809Q · Cessna 206H · Vacuum System
  > VACUUM PUMP FAILED IN FLIGHT. CAUSED INSTRUMENT OPERATIONAL FAILURE OF SEVERAL INSTRUMENTS. OVERHAULED.
- [SDR 2017FA0000242](https://openairdocs.org/sdr/2017FA0000242.md): Connector · burned · Jun 12, 2017 · N332SC · Cessna 206H · Navigation System Wiring
  > SECONDARY FLIGHT DISPLAY INOPERATIVE. PRELIMINARY INSPECTION FOUND THE NR 2 ELECTRICAL BUSS INOPERATIVE, INCLUDING THE DISPLAY, PITOT HEAT, NAV LIGHTS, RECOG/TAXI LIGHTS, STROBE LIGHTS, PANEL LIGHTS, AVN 2, SKYNODE, AND AIRBORNE IMAGING SYSTEM. FOUND THE NR
- [SDR 2017FA0000080](https://openairdocs.org/sdr/2017FA0000080.md): Pump · failed · Feb 14, 2017 · N229E · Cessna 206H · Reciprocating Engine Oil System
  > PILOT REPORTED MINOR ENGINE SURGING DURING FLIGHT. AFTER TROUBLESHOOTING AND REPAIRS, FOUND TO BE THE ENGINE DRIVEN FUEL PUMP INTERMITTENTLY DROPPING FUEL PRESSURE. ON INVESTIGATION THE OIL SEAL IN THE DIAPHRAGM PUMP WAS FOUND TO BE LEAKING AND OIL WAS IN TH
- [SDR 2016FA0000592](https://openairdocs.org/sdr/2016FA0000592.md): Pushrod · scored · Dec 6, 2016 · N249DB · Cessna 206H · Reciprocating Engine Cylinder Section
  > ONE ROCKER ARM IS SHOWING SIGNS OF SCORING ALONG WITH A PUSHROD, AND A HYDRAULIC LIFTER CAP. REPLACED IAW SA-167A.
- [SDR 2016FA0000544](https://openairdocs.org/sdr/2016FA0000544.md): Transponder · failed · Oct 26, 2016 · N565SA · Cessna 206H · Navigation System
  > TRANSPONDER FAILED WITH A PUFF OF SMOKE. FOLLOWED BY A FAIL MESSAGE. UNIT SECURED AND LANDED.
- [SDR 2P9A3229](https://openairdocs.org/sdr/2P9A3229.md): Spark Plug · broken · Oct 1, 2016 · N267MC · Cessna 206H · Spark Plug/Igniter
  > DURING CRUISE FLIGHT, THE PILOT EXPERIENCED A SUDDEN RISE IN EGT AND CHT FOR NR 4 CYLINDER AND THEN EXPERIENCED A ROUGH RUNNING ENGINE. PILOT MADE A PRECAUTIONARY LANDING TO GET THE PLANE INSPECTED. FOUND THE SPARK PLUG BROKEN.
- [SDR 2016FA0000457](https://openairdocs.org/sdr/2016FA0000457.md): Transponder · smoke · Sep 27, 2016 · N3518 · Cessna 206H · ATC Transponder System
  > SMOKE FROM TRANSPONDER ON APPROACH FOLLOWED BY FAILED MASSAGE. SHORTLY AFTER SCREEN WENT BLACK.
- [SDR 2016FA0000374](https://openairdocs.org/sdr/2016FA0000374.md): Actuator · failed · Jul 27, 2016 · N590MM · Cessna 206H · Elevator Tab Control System
  > FROM SAFETY REPORT, AIRCRAFT ELEVATOR TRIM WHEEL FAILURE ON DEPARTURE. ATTEMPTED ELEVATOR TRIM INPUT, NOSE UP, USING THE YOKE TRIM SWITCH AND NOTICED NOTHING HAPPENED. CHECKED AUTOPILOT CB AND IT WAS STILL IN. USED THE ELEVATOR TRIM WHEEL AND IT WOULD SPIN
- [SDR 2016FA0000325](https://openairdocs.org/sdr/2016FA0000325.md): Alternator · broken · Jul 6, 2016 · N590MM · Cessna 206H · AC Generator-Alternator
  > OIL LEAKING ONTO RIGHT SIDE OF AIRCRAFT UNDERBELLY OBSERVED IN POSTFLIGHT. INSPECTED ENGINE FOR OIL LEAK. INSPECTED NR 2 ALTERNATOR. FOUND MOUNTING BASE OF ALTERNATOR IS CRACKED AND SOME OIL LEAKING OUT OF ALTERNATOR.
- [SDR 2015FA0000431](https://openairdocs.org/sdr/2015FA0000431.md): Actuator · broken · Sep 2, 2015 · N7276Z · Cessna 206H · Flight Control System
  > UPON REACHING CRUISE FLIGHT WITH THE AUTOPILOT ENGAGED, THE CREW BEGAN TO TRIM OUT THE AIRPLANE FOR LEVEL FLIGHT AND AS THE TRIM WHEEL WAS TURNING THEY GOT A TRIM IN MOTION WARNING. IT REPEATED MULTIPLE TIMES AND EVENTUALLY SAID CHECK PITCH TRIM. THE CREW DI
- [SDR 2015FA0000219](https://openairdocs.org/sdr/2015FA0000219.md): Connector · melted · May 20, 2015 · N250E · Cessna 206H · Electrical Power System Wiring
  > ALL AIRCRAFT SYSTEMS POWERED BY ESSENTIAL BUS 2 FAILED DURING TAKEOFF WITHOUT TURNING THE SWITCH OFF. ITEMS ON BUS 2 INCLUDE: THE TURN COORDINATOR, NAV LIGHTS, INTERIOR LIGHTS, STROBE LIGHTS, TAXI LIGHT, PITOT HEAT, TRANSPONDER, AND AUTOPILOT ALL FAILED. THE
- [SDR 2015FA0000175](https://openairdocs.org/sdr/2015FA0000175.md): Valve · broken · Apr 30, 2015 · N940H · Cessna 206H · Tire Tube
  > UPON LANDING THE PILOT NOTICED THAT THE WAS PULLING TO THE LEFT. THE TIRE WAS REMOVED AND FOUND THAT THE VALVE STEM HAD FRACTURED AND DEPARTED APPROXIMATELY.2500 DOWN FROM THE END. THE SUBSEQUENT LOSS OF AIR FROM THE TIRE CAUSED THE TIRE TO GO FLAT WHICH IN
- [SDR 2015FA0000126](https://openairdocs.org/sdr/2015FA0000126.md): Connector · melted · Apr 2, 2015 · N238D · Cessna 206H · Electrical Power System Wiring
  > ALL APPLIANCES AND SYSTEMS ON ACFT ESSENTIAL BUS 2 POWERED OFF WITH THE SWITCH ON. ITEMS ON BUS 2 INCLUDE: THE TURN COORDINATOR, NAV LIGHTS, INTERIOR LIGHTS, STROBE LIGHTS, TAXI LIGHT, PITOT HEAT, TRANSPONDER, AND AUTOPILOT ALL FAILED. THE 40 AMP. BUS 2 CIRCU
- [SDR 2015FA0000125](https://openairdocs.org/sdr/2015FA0000125.md): Connector · melted · Apr 2, 2015 · N8211P · Cessna 206H · Electrical Power System Wiring
  > ALL APPLIANCES AND SYSTEMS ON ACFT ESSENTIAL BUS 2 POWERED OFF WITH THE BUS 2 SWITCH ON. ITEMS ON BUS 2 INCLUDE: THE TURN COORDINATOR, NAV LIGHTS, INTERIOR LIGHTS, STROBE LIGHTS, TAXI LIGHT, PITOT HEAT, TRANSPONDER, AND AUTOPILOT ALL FAILED. THE 40 AMP BUS 2
- [SDR LC1R20140305001](https://openairdocs.org/sdr/LC1R20140305001.md): Pressure Switch · leaking · Mar 5, 2014 · N125MD · Cessna 206H · Engine Oil Pressure
  > AD 2013-11-11 HAD BEEN COMPLIED WITH BY IDENTIFYING THE PART NUMBER OF THE OIL PRESS SWITCH AS 83278 WHICH WOULD GIVE IT A 3000 HOUR SERVICE LIFE. DURING THE ANNUAL INSPECTION IT WAS DISCOVERED THAT THE SWITCH WAS LEAKING QUITE BADLY FROM THE CONNECTOR WELL A
- [SDR 2014FA0000027](https://openairdocs.org/sdr/2014FA0000027.md): Sprocket · sheared · Dec 12, 2013 · N181SA · Cessna 206H · Elevator Control System
  > DURING FLIGHT, ELEVATOR TRIM BECAME STIFF AND ELECTRIC TRIM WOULD NOT OPERATE. FOLLOWED BY COMPLETE LOSS OF ELEVATOR TRIM ABILITY. DURING INSPECTION FOUND CHAIN SPROCKET ON ELEVATOR TRIM HAD SHEARED FROM TRIM ACTUATOR ASSY.
- [SDR 2013FA0000231](https://openairdocs.org/sdr/2013FA0000231.md): Bulkhead · cracked · Feb 26, 2013 · N5235C · Cessna 206H · Wheel/Ski/Float
  > AIRCRAFT CAME INTO THE MX SHOP FOR AN ANNUAL INSPECTION. THE ACFT IS ON A SET OF AMPHIBIOUS FLOATS, MODEL 3450. AFTER REMOVING THE RIGHT FLOAT BUMPER, 2 CRACKS WERE DISCOVERED ON THE BULKHEAD NOSE ASSY. PN 30A01000-329. THE CRACK STARTED FROM EACH OF THE B
- [SDR 2012FA0000733](https://openairdocs.org/sdr/2012FA0000733.md): Intake Valve · separated · Jul 29, 2012 · N206BC · Cessna 206H · Reciprocating Engine Cylinder Section
  > AT CRUISE FLIGHT, PILOT EXPERIENCED A BANG AND LOSS OF ENGINE POWER. ACFT LANDED SAFELY AT NEARBY AIRPORT. DURING COMPRESSION CHECK IT WAS FOUND THAT NR 6 CYL HAD NO COMPRESSION. CYLINDER WAS REMOVED AND FOUND INTAKE VALVE HAD BROKEN AND WEDGED VALVE FACE I
- [SDR 2011FA0000593](https://openairdocs.org/sdr/2011FA0000593.md): Piston Pin · missing · Sep 7, 2011 · N109P · Cessna 206H · Reciprocating Engine Power Section
  > BOTH PISTON PIN PLUGS WERE OMITTED FROM A CYLINDER DURING ENGINE ASSEMBLY AT THE FACTORY. DURING AN ANNUAL INSPECTION, THE COMPRESSION TEST INDICATED NO PRESSURE BEING HELD IN NR 4 CYLINDER. WHEN THE CYLINDER WAS REMOVED FOR REPAIR, THE PISTON PIN PLUGS WERE
- [SDR 2011FA0000037](https://openairdocs.org/sdr/2011FA0000037.md): Capacitor · failed · Nov 1, 2010 · N950HP · Cessna 206H · Audio Integrating System
  > ON 10/30/2010 AT APPROX 1600 HRS, WHILE FLYING TRAFFIC SUPPORT. SMOKE OBSERVED COMING FROM BEHIND GPS & NR 1 RADIO FACE AREA. PILOT IMMEDIATELY LANDED & SHUTDOWN ACFT. MX CALLED & INSPECTED ACFT, IT WAS DETERMINED TO BE AIRWORTHY. AFTER FERRY PERMIT WAS IS
- [SDR 2010FA0000094](https://openairdocs.org/sdr/2010FA0000094.md): Connector · loose · Jan 8, 2010 · N236KS · Cessna 206H · Fuel System Wiring
  > PILOT REPORTED THAT FLAPS WOULD NOT EXTEND. CONNECTED EXTERNAL POWER AND FOUND THAT FLAPS WORKED PROPERLY. ON POST INSPECTION RUN UP FOUND THAT FUEL BOOST PUMP WOULD NOT OPERATE AND BEACON WOULD NOT FLASH. FOUND THAT THE ABOVE COMPONENTS WERE ON THE SAME EL
- [SDR 2010FA0000023](https://openairdocs.org/sdr/2010FA0000023.md): Duct · collapsed · Jan 6, 2010 · N10457 · Cessna 206H · Engine Air Intake System
  > DURING ANNUAL INSP, FOUND DUCT JUST AFT OF INDUCTION FILTER TO BE PARTIALLY COLLAPSED. AFTER REMOVING DUCT, FOUND THE INTERNAL WIRE FORMERS TO BE DISCONNECTED AND UNRAVELED CAUSING THE DUCT TO COLLAPSE.
- [SDR 2009FA0000476](https://openairdocs.org/sdr/2009FA0000476.md): Strut · failed · Jun 3, 2009 · N220DE · Cessna 206H · Main Landing Gear Strut/Axle/Truck
  > RT MAIN GEAR SPRING STRUT HAD A CATASTOPHIC FAILURE. THE STRUT BROKE IN HALF APPROX 2 INCHES ABOVE THE BRAKE LINE ATTACH BRACKET. THE ACFT WAS PARKED IN THE HANGAR AND NO PERSONNEL WERE AROUND OR PRESENT WHEN THIS OCCURED. THE RT WING TIP CONTACTED THE HANG
- [SDR 2008FA0000928](https://openairdocs.org/sdr/2008FA0000928.md): Magneto · damaged · Dec 30, 2008 · N5880K · Cessna 206H · Magneto/Distributor
  > RT MAGNETO INTERMITTENT, MAGNETO STAYED HOT AND SOME TIMES IT WILL NOT HAVE ANY CURRENT GOING THROUGH. IF PROPELLER WAS MOVE IT WILL FIRE RT UP, AFTER REMOVED RT MAGNETO AND OPENED FOUND THAT THAT COIL HAS MELTED MOST OF THE GEARS AND CASING.
- [SDR 2009FA0000024](https://openairdocs.org/sdr/2009FA0000024.md): Servo · leaking · Dec 4, 2008 · N137P · Cessna 206H · Fuel Control/Reciprocating Engines
  > FUEL SERVO LEAKED WHILE ACFT WAS PARKED OVERNIGHT. THE MIXTURE WAS IN CUT OFF POSITION. FLIGHT MANUAL, SEC 4, NORMAL PROCEDURES PAGE 4-23 SECURING ACFT NR 10 STATES: FUEL SELECTOR VALVE RT OR LT TO PREVENT CROSS FEEDING. IF THE FUEL SELECTOR VALVE WAS TURNE
- [SDR 2008FA0000212](https://openairdocs.org/sdr/2008FA0000212.md): Gasket · unknown · Mar 19, 2008 · N2446X · Cessna 206H · Fuel Control/Reciprocating Engines
  > INSPECTED FUEL SERVO PLUG IAW SBPRS-107, REVISION 1, DATED MARCH 6, 2008. NO DAMAGE FOUND ON THE THREADS OF THE PLUG OF THE SERVO UNIT. INSTALLED PLUG AND SAFETIED IAW INSTRUCTIONS.
- [SDR 2007FA0000451](https://openairdocs.org/sdr/2007FA0000451.md): Cylinder · scratched · Mar 28, 2007 · Cessna 206H · Reciprocating Engine Cylinder Section
  > SET OF 6 CYLINDERS CAME IN WITH 2 BROKEN CONTROL RINGS. CYLINDERS HAD RING STEPS ON TOP AND BOTTOM OF CYLINDER BARRELS. CORROSION WAS PRESENT IN BARRELS FROM THE MIDDLE UP TO THE HEAD OF THE CYLINDERS. EXHAUST GUIDES WERE FAR OUT OF LIMITS AND DIFFICULT TO REM
- [SDR 2007FA0000450](https://openairdocs.org/sdr/2007FA0000450.md): Cylinder · scratched · Mar 28, 2007 · Cessna 206H · Reciprocating Engine Cylinder Section
  > SET OF 6 CYLINDERS CAME IN WITH 2 BROKEN CONTROL RINGS. CYLINDERS HAD RING STEPS ON TOP AND BOTTOM OF CYLINDER BARRELS. CORROSION WAS PRESENT IN BARRELS FROM THE MIDDLE UP TO THE HEAD OF THE CYLINDERS. EXHAUST GUIDES WERE FAR OUT OF LIMITS AND DIFFICULT TO REM
- [SDR 2006FA0000357](https://openairdocs.org/sdr/2006FA0000357.md): Servo · inoperative · Mar 13, 2006 · N236KS · Cessna 206H · Fuel Controlling System
  > AIRCRAFT LANDED AND ENGINE QUIT. TO RESTART ENGINE MIXTURE HAD TO PULL MIXTURE BACK TO.5 INCH OF IDLE CUT TO KEEP ENGINE RUNNING. TRIED TO ADJUST IDLE MIXTURE WITHOUT SUCCESS. AT THE ADJUSTMENT LEANEST SETTING THERE WAS STILL A 600 RPM RAISE WHEN MIXTURE P
- [SDR 2006FA0000275](https://openairdocs.org/sdr/2006FA0000275.md): Alternator · burned · Mar 7, 2006 · Cessna 206H · AC Generation System
  > BATTERY TERMINAL LUG BURNT OFF DUE TO SHORT CAUSED BY TERMINAL ON WIRE HARNESS BREAKING OFF. THIS CAUSED THE ALTERNATOR CONTROL UNIT TO FAIL (SMOKE) AND HEAVY ARCING AT TERMINAL LUG. THERE WAS AN INDICATION OF NOT CHARGING ON G-1000 MFD AND PFD SCREENS. THI
- [SDR CA060105004](https://openairdocs.org/sdr/CA060105004.md): Control Cable · frayed · Jan 5, 2006 · Cessna 206H · Wheel/Ski/Float
  > WATER RUDDER STEERING CABLES ARE FRAYED WHERE IT ENTERS THE SIDE OF THE FLOAT. THE MAIN CAUSE OF THIS IS A MISALIGNMENT OF THE HOLE ON THE SIDE OF THE FLOAT TO THE ACTUAL POSITIONING OF THE RUN. IN SOME CASES, THE CABLE HAD CUT A 1/4" SLOT ON THE FLOAT SIDE
- [SDR 2005FA0001009](https://openairdocs.org/sdr/2005FA0001009.md): Bellcrank · binding · Jul 1, 2005 · N239LF · Cessna 206H · Trailing Edge Flap Control System
  > BINDING IN FLAP DR SYS AT BELLCRANKS WHERE ROD ENDS ATTACH. FLAP DR RODENDS WERE FOUND DIGGING INTO BELLCRANK ARMS AS THEY OPERATED, NML TRAVEL AS SHOWN BY RUB MARKS ON RODENDS. BELLCRANK ARMS, EXCESS CLAMPED BY RODEND ATTACH BOLTS, SOME BOLTS NOT TIGHTENED
- [SDR 2005FA0000687](https://openairdocs.org/sdr/2005FA0000687.md): Indication Sys · inoperative · Jan 4, 2005 · N962AC · Cessna 206H · Turn and Bank/Rate of Turn Indicator
  > UNIT WAS INSTALLED IN AIRCRAFT ON 12/20/2004. AFTER APPROX.5 HOURS, PILOT OBSERVED TURN COORDINATOR OFF FLAG, MOMENTS LATER AUTOPILOT DISENGAGED. THIS UNIT REPLACED AN EARLIER INSTALLED OVERHAULED UNIT INSTALLED 7/04. (K)
- [SDR 2004FA0000861](https://openairdocs.org/sdr/2004FA0000861.md): Wire · burned · Oct 31, 2004 · N21076 · Cessna 206H · Electrical Power System Wiring
  > PILOT REPORTED AN ALTERNATOR FAILURE. REMOVED ENGINE COWLING AND FOUND THE POWER WIRE AND THE GROUND WIRE FOR THE ALTERNATOR WERE BROKEN IN HALF ABOUT 3 INCHES FROM THE TERMINALS ON THE ALTERNATOR. THE ENDS OF BOTH WIRES WERE MELTED, SUSPECTED FROM ARCING.
- [SDR 2004FA0000649](https://openairdocs.org/sdr/2004FA0000649.md): Sump · cracked · Aug 19, 2004 · N242ME · Cessna 206H · Reciprocating Engine Oil System
  > DURING AN ANNUAL INSPECTION THE ENGINE OIL SUMP WAS FOUND CRACKED IN THE LT REAR STUD BOSS WHERE THE STUD US THREADED INTO THE SUMP.
- [SDR LU42004F00000](https://openairdocs.org/sdr/LU42004F00000.md): Flyweight · broken · Jun 30, 2004 · N7270C · Cessna 206H · Propeller Governor
  > GOVERNOR FAILED TO PRODUCE PRESSURE, UPON DISASSEMBLY FOUND BROKEN FLYWEIGHT DISC PN D20880, SPRING DRIVE PN C20886 DAMAGED, PN B208821, SPRING BROKEN. NOTE: NO IMPACT KNOWN PARTS SENT TO MFG FOR INSPECTION.
- [SDR 2004FA0000652](https://openairdocs.org/sdr/2004FA0000652.md): Reservoir · leaking · May 10, 2004 · N72635 · Cessna 206H · Fuel Storage
  > RESERVOIR FUEL TANKS BELOW FUEL SELECTOR WAS LEAKING FUEL FROM A SEEM WELD THAT HAD CRACKED. FOUND DURING ROUTINE WALK AROUND INSPECTION. THE LEAK WHEN FIRST NOTICED WILL INDICATE THE FUEL PEDCOK IS LEAKING UNDER THE BELLY OF THE AIRCRAFT FURTHER INSPECTION
- [SDR CMR2003F00000](https://openairdocs.org/sdr/CMR2003F00000.md): Rod · broken · Nov 17, 2003 · N35561 · Cessna 206H · Aileron Control System
  > IMMEDIATELY AFTER TAKE OFF, THE PILOT NOTICED MINIMAL REACTION FROM AILERON CONTROL INPUTS. PILOT LANDED SAFELY. INVESTIGATION REVEALED LT AILERON DISCONNECTED FROM CONTROL ROD. FOUND THAT CONTROL ROD HAD BROKEN IN THREADED AREA JUST FORWARD OF AILERON CONT
- [SDR 2003FA0001061](https://openairdocs.org/sdr/2003FA0001061.md): Distributor Blk · burned · Jul 25, 2003 · N3530E · Cessna 206H · Magneto/Distributor
  > DISTRIBUTOR BLOCK AND GEAR ASSEMBLY BURNED UP.

Next page: https://openairdocs.org/model/cessna-206h/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 = '206H'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/cessna-206h/reports

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