# Service difficulty reports: Cessna U206F

A list on [Cessna U206F](https://openairdocs.org/model/cessna-u206f.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 5 · 227 reports

- [SDR 2026FA0000597](https://openairdocs.org/sdr/2026FA0000597.md): Engine · failed · Apr 16, 2026 · N93021 · Cessna U206F · Engine (Reciprocating)
  > COMPLETE LOSS OF POWER IN CRUISE FLIGHT, AIRCRAFT WAS DITCHED AND UNRECOVERABLE.
- [SDR 2020FA0000080](https://openairdocs.org/sdr/2020FA0000080.md): Lifter · spalled · Jan 22, 2020 · N710MH · Cessna U206F · Reciprocating Engine Power Section
  > PILOT REPORTED LOW OIL PRESSURE AT IDLE, REMOVED OIL PRESSURE REGULATOR AND FOUND SHARP METAL CHIP IN BOTTOM OF REGULATOR WHERE IT HAD ARRIVED AFTER FALLING OUT OF REGULATOR SEAT. PREVIOUS EXPERIENCE LED US TO BELIEVE THAT THE METAL WAS FROM A LIFTER, WE INSP
- [SDR CA190530008](https://openairdocs.org/sdr/CA190530008.md): Adapter · malfunctioned · May 26, 2019 · Cessna U206F · Engine Cranking
  > (CAN) DEFECT: PROP FAILED TO TURN ON START. RECTIFICATION: STARTER ADAPTER ASSEMBLY REMOVED AND REPLACED WITH OVERHAULED ASSEMBLY AND GASKET AS PER TCM MM X30039 SECT 4-21 AND SECT 7-8. AIRCRAFT GROUND RUN, FUNCTION AND LEAK CHECK FOUND SERVICEABLE. (TC# 20190
- [SDR CA180907015](https://openairdocs.org/sdr/CA180907015.md): Alternator · failed · Sep 7, 2018 · Cessna U206F · AC Generator-Alternator
  > (CAN) FAILED DURING FLIGHT, BATTERY RUN DOWN AS A RESULT. (TC# 20180907015)
- [SDR 2017FA0000512](https://openairdocs.org/sdr/2017FA0000512.md): Intake Valve · chipped · Oct 13, 2017 · N123TM · Cessna U206F · Reciprocating Engine Cylinder Section
  > LOW COMPRESSION DURING A 100 HOUR INSPECTION, IN ONE CYLINDER (20/80) WAS OBSERVED. BORESCOPE INSPECTION SHOWED AN INTAKE VALVE THAT HAD LOST PART OF THE LIP THAT SEALS AGAINST THE VALVE SEAT.
- [SDR 2017FA0000506](https://openairdocs.org/sdr/2017FA0000506.md): Rocker · brinelled · Oct 3, 2017 · N123TM · Cessna U206F · Reciprocating Engine Cylinder Section
  > DURING AN ENGINE REPAIR, ONE ROCKER ARM WAS FOUND TO HAVE SEVERELY WORN AREA WHERE THE ROCKER ARM PUSHES ON THE VALVE STEM.
- [SDR NXY2016F00000](https://openairdocs.org/sdr/NXY2016F00000.md): Engine · seized · Jul 14, 2016 · N8345Q · Cessna U206F · Engine (Reciprocating)
  > SHORTLY AFTER START, THE ENGINE STOPPED DURING GROUND OPERATION. ENGINE SEEMS TO BE SEIZED, HOWEVER FURTHER EVALUATION IS NEEDED TO ASCERTAIN CAUSE. THERE WAS NO INDICATION OF ANY PROBLEMS PRIOR TO THIS. WILL SUBMIT A FOLLOW UP REPORT AFTER TEARDOWN.
- [SDR P9KA2015091401](https://openairdocs.org/sdr/P9KA2015091401.md): Thru Bolt · broken · Sep 8, 2015 · N8419Q · Cessna U206F · Reciprocating Engine Power Section
  > WHILE PERFORMING A ROUTINE OIL & FILTER CHANGE, MECHANIC SAW LARGE AMOUNTS OF LEAKED OIL & A CRANKCASE THROUGH BOLT NUT IN THE COWLING. FURTHER INVESTIGATION REVEALED THAT THE LOWER FWD THROUGH BOLT HAD BROKEN AT THE NR 6 CYLINDER. UPON REMOVING THE REMAINS
- [SDR XDKC20140304001](https://openairdocs.org/sdr/XDKC20140304001.md): Attach Bracket · corroded · Mar 4, 2014 · N9515G · Cessna U206F · Fuselage Main, Attach Fittings
  > DISCOVERED HEAVY CORROSION AT BS 112 SEAT BELT ATTACH BRACKET.
- [SDR XDKC2014F00093](https://openairdocs.org/sdr/XDKC2014F00093.md): Fitting · cracked · Mar 3, 2014 · N9515G · Cessna U206F · Fuselage, Landing Gear Attach Fittings
  > DISCOVERED CRACKS IN THE LT MLG FITTING.
- [SDR CA131118015](https://openairdocs.org/sdr/CA131118015.md): Sensor · failed · Nov 9, 2013 · Cessna U206F · AC Regulator
  > (CAN) THE ACFT EXPERIENCED AN OVER VOLTAGE LIGHT SHORTLY AFTER ENGINE START DURING A MAINTENANCE GROUND RUN. THE OVER VOLTAGE SENSOR WAS FOUND TO HAVE FAILED. THE UNIT WAS REPLACED AND THE SYSTEM WAS GROUND FUNCTION CHECKED SERVICEABLE.
- [SDR CA131103001](https://openairdocs.org/sdr/CA131103001.md): Alternator · failed · Jul 30, 2013 · Cessna U206F · AC Generator-Alternator
  > (CAN) ON ENGINE START UP THE CREW NOTICED THE ALTERNATOR AMP GAUGE WAS SHOWING A DISCHARGE, THE ACFT SHUTDOWN AND MAINTENANCE REPLACED THE ALTERNATOR WITH NEW. THE SYSTEM GROUND FUNCTION CHECKED SERVICEABLE.
- [SDR CA121031003](https://openairdocs.org/sdr/CA121031003.md): Alternator · failed · Oct 30, 2012 · Cessna U206F · AC Generator-Alternator
  > (CAN) ALTERNATOR FAILED, CASE BOLTS SHEARED ALTERNATOR FAILED AFTER 48 HRS SINCE NEW.
- [SDR CA121025004](https://openairdocs.org/sdr/CA121025004.md): Switch · faulted · Oct 16, 2012 · Cessna U206F · Magneto/Distributor
  > (CAN) ON SHUTDOWN, THE PILOT CONDUCTED A LIVE MAG CHECK AND FOUND THE MAGS WHERE BOTH LIVE. THE SWITCH WAS FOUND FAULTLY AND WAS REPLACED.
- [SDR CA121025002](https://openairdocs.org/sdr/CA121025002.md): Alternator · failed · Sep 12, 2012 · Cessna U206F · AC Generator-Alternator
  > (CAN) ON A ROUTINE FLIGHT THE PILOT NOTICED THE AMMETER SHOWING A DISCHARGE, THE FLIGHT ENDED WITHOUT INCIDENT AT THE INTENDED DESTINATION. MAINTENANCE DISCOVERED THAT ONCE AGAIN THE CASE HALF BOLTS HAD SHEARED ON THE ALTERNATOR CASING THE ALTERNATOR TO SPLIT
- [SDR UVVR2012081500024](https://openairdocs.org/sdr/UVVR2012081500024.md): Arm · corroded · Aug 15, 2012 · N334W · Cessna U206F · Rudder Control System
  > WHILE PERFORMING AN ANNUAL INSPECTION ON THIS ACFT EVIDENCE OF RUST WAS OBSERVED ON THE OPENING IN THE TOP OF THE PILOTS LEFT RUDDER PEDAL MECHANISM TUBE BEHIND THE RUDDER PEDAL. THE RUDDER PEDAL ATTACHES TO AND PIVOTS (FOR BRAKING PURPOSES) ON THIS TUBE. DIS
- [SDR 2012FA0000639](https://openairdocs.org/sdr/2012FA0000639.md): Connecting Rod · failed · Aug 9, 2012 · N345TW · Cessna U206F · Reciprocating Engine Power Section
  > INFLIGHT LOSS OF POWER AND LOSS OF OIL DURING CLIMB CAUSING AIRCRAFT UNSCHEDULED LANDING. VISUALLY INSPECTED ENGINE AND FOUND CRANKCASE WAS PUNCTURED BY A CONNECTING ROD CAUSING OIL TO LEAK.
- [SDR 2012F00147](https://openairdocs.org/sdr/2012F00147.md): Cylinder · cracked · Jul 23, 2012 · N7138Q · Cessna U206F · Reciprocating Engine Cylinder Section
  > ON FIRST RUN UP OF THE DAY PILOT NOTED ACFT RAN ROUGH AND SOUNDED DIFFERENT. MX PERSONAL PERFORMED A VISUAL INSPECTION OF CYLINDERS AND FOUND NR 5 CYLINDER MISSING SEVERAL COOLING FINS AND A HOLE THE SIZE OF A PENCIL IN THE AREA OF THE EXHAUST PORT ON THE TOP
- [SDR CA120726011](https://openairdocs.org/sdr/CA120726011.md): Alternator · malfunctioned · Jul 20, 2012 · Cessna U206F · AC Generator-Alternator
  > (CAN) DURING A ROUTINE FLIGHT THE PILOT NOTED A LOW VOLTAGE LIGHT FOLLOWED BY A DISCHARGE RESULTING IN A TOTAL LOSS OF POWER. MAINTENANCE DISCOVERED THE ALTERNATOR CASE HALF BOLTS SHEARED AS A RESULT OF AN INTERNAL BEARING FAILURE. MAINTENANCE REPLACED THE AL
- [SDR CA120709005](https://openairdocs.org/sdr/CA120709005.md): Line · leaking · Jul 9, 2012 · Cessna U206F · Turbine Engine Oil System
  > (CAN) EVIDENCE OF OIL FOUND ON CO-PILOT`S FLOOR. OIL PRESSURE LINE BETWEEN FIREWALL AND OIL PRESSURE GAUGE WAS FOUND LEAKING.
- [SDR CA120709010](https://openairdocs.org/sdr/CA120709010.md): Gyro · failed · Jul 5, 2012 · Cessna U206F · Attitude Gyro and Indicating System
  > (CAN) DURING TAXI AND RUN-UP IT WAS OBSERVED THAT THE ATTITUDE GYRO DID NOT BECOME ERECT, THE ATTITUDE GYRO WAS REPLACED AND GROUND FUNCTION CHECKED SERVICABLE.
- [SDR CA120513001](https://openairdocs.org/sdr/CA120513001.md): Cylinder Head · cracked · May 11, 2012 · Cessna U206F · Reciprocating Engine Cylinder Section
  > (CAN) CYLINDER HEAD FOUND CRACKED BOTTOM SIDE SPARK PLUG HOLE TO SPARK PLUG HOLE.
- [SDR CA120716025](https://openairdocs.org/sdr/CA120716025.md): Crankshaft · broken · May 8, 2012 · Cessna U206F · Reciprocating Engine Power Section
  > (CAN) CRANKSHAFT FAILED IN FLIGHT WHICH CAUSED THE ENGINE TO STOP. AIRPLANE HAD EMERGENCY LANDING WHICH CAUSED EXTENSIVE DAMAGE TO THE AIRPLANE. CRANKSHAFT FAILED IN SAME AREA THAT IS TO BE INSPECTED AS PER CONTINENTAL SB. 96-10A.
- [SDR CA120326014](https://openairdocs.org/sdr/CA120326014.md): Float · stuck · Mar 26, 2012 · Cessna U206F · Fuel Indicating System
  > (CAN) ON START UP TAXI AFTER TAKING ON FUEL, THE PILOT NOTICED THE RT FUEL GAUGE STILL INDICATED EMPTY. MAINTENANCE INSPECTED THE SYS AND FOUND THE FLOAT ARM WAS "STUCK" AT THE EMPTY POSITION. THE FLOAT ARM WAS KINETICALLY ADJUSTED WITH OUT FURTHER INCIDENT
- [SDR CA120203011](https://openairdocs.org/sdr/CA120203011.md): Wire · loose · Jan 31, 2012 · Cessna U206F · Fuel System Wiring
  > (CAN) ON A FLIGHT, RT FUEL GAUGE BECAME U/S READING ZERO, THE PILOT LANDED WITHOUT INCIDENT. MAINTENANCE DISCOVERED A LOOSE WIRE ON THE FUEL SENDER UNIT. THE WIRE WAS REPAIRED AND THE SYS WAS GROUND FUNCTION CHECKED SERVICABLE.
- [SDR CA120203010](https://openairdocs.org/sdr/CA120203010.md): Handle · broken · Jan 30, 2012 · Cessna U206F · Passenger/Crew Doors
  > (CAN) UPON ENTRY INTO THE ACFT THE PILOT WENT TO OPEN THE DOOR AND THE HANDLE BROKE OFF IN HIS HAND. THE HANDLE WAS REPLACED WITHOUT FUTHER INCIDENT.
- [SDR 2012FA0000024](https://openairdocs.org/sdr/2012FA0000024.md): Housing · galled · Jan 2, 2012 · N8368Q · Cessna U206F · Engine Fuel Pump
  > ENGINE DIED ON INITIAL RUN-UP DUE TO FUEL STARVATION. FOUND GALLING BETWEEN FUEL PUMP DRIVE GEAR AND HOUSING. CAUSE UNDETERMINED. SENT BOTH PARTS OUT FOR O/H.
- [SDR CA120105002](https://openairdocs.org/sdr/CA120105002.md): Alternator · malfunctioned · Dec 6, 2011 · Cessna U206F · AC Generator-Alternator
  > (CAN) AMMETER CHECK DURING RUN-UP SHOWED NO CHARGING. ALTERNATOR REPLACED.
- [SDR CA111121009](https://openairdocs.org/sdr/CA111121009.md): Indicator · failed · Nov 17, 2011 · Cessna U206F · Attitude Gyro and Indicating System
  > (CAN) DURING A ROUTINE FLIGHT IT WAS NOTED DURING THE CLIMBOUT THE PILOT ATTITUDE INDICATOR BECAME UNSERVICEABLE, THE FLIGHT AND LANDING CONTINUED WITHOUT COMPLICATIONS. THE ATTITUDE INDICATOR WAS R & R, THE SYS WAS GROUND FUNCTION CHECKED SERVICEABLE.
- [SDR 2011FA0000592](https://openairdocs.org/sdr/2011FA0000592.md): Attach Bracket · cracked · Sep 15, 2011 · N9575G · Cessna U206F · Horizontal Stabilizer, Attach Fittings
  > CRACKS WERE FOUND ON THE REAR HORIZ STABILIZER ATTACHMENT BRACKET ON THE FUSELAGE. 4 EXAMPLE PARTS WERE TURNED IN THE THE CERTIFICATION OFFICE AND ARE BEING FORWARDED TO THE ACO.
- [SDR CA110531008](https://openairdocs.org/sdr/CA110531008.md): Wire · burned · May 31, 2011 · Cessna U206F · Electrical Power System Wiring
  > ACFT LOST RADIO COMMUNICATIONS IN FLIGHT. RETURNED TO DEPARTURE AIRPORT. MX FOUND A BURNED WIRE ON THE ALTERNATOR AND REPAIRED. ALTERNATOR REPLACED.
- [SDR SVVA03082001](https://openairdocs.org/sdr/SVVA03082001.md): Main Bearing · failed · Feb 7, 2011 · N50159 · Cessna U206F · Reciprocating Engine Power Section
  > FOUND PARTICLES IN OIL FILTER. FURTHER SEARCHING FOR PROBLEM FOUND MAIN BEARING PARTS IN OIL PAN.
- [SDR CA110107007](https://openairdocs.org/sdr/CA110107007.md): Hub · cracked · Jan 6, 2011 · Cessna U206F · Propeller Hub Section
  > UPON LPI OF HUB, FOUND A CRACK 1 1/2 INCHES LONG RUNNING FROM ONE STUD HOLE TO ONE DOWEL HOLE ON THE MOUNTING FLANGE.
- [SDR CA110103007](https://openairdocs.org/sdr/CA110103007.md): Fitting · disconnected · Dec 20, 2010 · Cessna U206F · Fuel Storage
  > WHILE INSPECTING TANK FOR A SUSPECTED LEAK, IT WAS NOTED THAT THE FUEL FILLER FITTING ON THE INBOARD FILLER HAD BECOME DETACHED FROM THE TANK. A WHITE FLAKEY RESIDUE WAS OBSERVED INSIDE THE TANK AND IS SUSPECTED OF BEING THE GLUE USED TO BOND THE METAL FITTING
- [SDR 2010FA0001232](https://openairdocs.org/sdr/2010FA0001232.md): Cylinder · cracked · Dec 7, 2010 · Cessna U206F · Reciprocating Engine Cylinder Section
  > THE ENGINE HAS APPROX 300 HOURS SINCE MAJOR O/H, THE ENGINE HAD LOW COMPRESSION, UPON BOROSCOPE ALL 6 CYLINDERS WERE REPORTED CRACKED, VARIOUS HEAD CRACKING.
- [SDR CA101230004](https://openairdocs.org/sdr/CA101230004.md): Indicator · failed · Oct 5, 2010 · Cessna U206F · Turn and Bank/Rate of Turn Indicator
  > ON A FLIGHT, IT WAS NOTICED THAT THE TURN COORDINATOR HAD FAILED. THE INSTRUMENT WAS REPLACED AND NO FURTHER INCIDENT PREVAILED.
- [SDR CA100913011](https://openairdocs.org/sdr/CA100913011.md): Air Box · cracked · Sep 13, 2010 · Cessna U206F · Engine Air Intake System
  > INDUCTION AIR BOX SENT IN FOR REPAIR. AD 85-10-02 APPLIES TO THIS UNIT. UNIT HAS.040" THICK SKIN AS OUTLINED IN AD AND IS STILL CRACKED WITH LARGE PIECES MISSING. UNIT WILL BE REPAIRED IAW AC 43.13-1A AND AC43.13-2A USING MATERIAL.050" THICK. AD 85-10-02 IN
- [SDR CA100924003](https://openairdocs.org/sdr/CA100924003.md): Bulkhead · cracked · Sep 8, 2010 · Cessna U206F · Wing, Rib/Bulkhead
  > DURING A ROUTINE 200 HR INSP, WHILE INSPECTING THE RT WING ROOT AREA, IT WAS NOTED THAT THE RT WING ROOT BULKHEAD ABOVE THE CO-PILOTS DOOR HAD SEVERAL CRACKS RUNNING IN ALL DIRECTIONS. WHEN THE RT WING TIP WAS MOVED UP OR DOWN OR FORE AND AFT, THIS CAUSED THE
- [SDR CA100622022](https://openairdocs.org/sdr/CA100622022.md): Brake Disc · cracked · May 31, 2010 · Cessna U206F · Landing Gear Brake System
  > (CAN) BRAKE DICS FOUND CRACKED AND RIPPED OUT AT BOLT HOLES BOTH WHEELS. SDR IS LATE BECAUSE UNKNOWN IF FLIGHT SAFTEY WAS AN ISSUE.
- [SDR CA101230005](https://openairdocs.org/sdr/CA101230005.md): Tachometer · failed · Mar 4, 2010 · Cessna U206F · Engine RPM Indicating System
  > (CAN) ON FLIGHT, THE PILOT REPORTED THE TACHOMETER HAD FAILED. THE TACHOMETER WAS REPLACED AND NO FURTHER INCIDENT PREVAILED.
- [SDR CA091202010](https://openairdocs.org/sdr/CA091202010.md): Shaft · broken · Nov 27, 2009 · Cessna U206F · Elevator Tab Control System
  > (CAN) IT APPEARS THE THREADED SHAFT OF THE ELEVATOR TRIM BROKE ON TAKEOFF OR IMMEDIATELY AFTER, CAUSING THE ELEVATOR TO JAM AND CREATING FLUTTER IN THE ELEVATOR CAUSING IT TO BREAK. THIS ALSO CAUSED THE OUTER PORTION OF THE RIGHT HORIZANTAL STABILZER TO FLUTT
- [SDR CA091203006](https://openairdocs.org/sdr/CA091203006.md): Spar · damaged · Nov 24, 2009 · Cessna U206F · Wing Spar
  > (CAN) UPON PULLING THE WINGS FOR A PAINT JOB, IT WAS NOTICED AT SOME POINT SOMEONE WHO WAS DRILLING A SCREW FROM THE WING ROOT FAIRING, DRILLED THROUGH THE WING ATTACH POINT FROM THE SPAR INTO THE WING BOLT.
- [SDR CA091030001](https://openairdocs.org/sdr/CA091030001.md): Bolt · loose · Oct 29, 2009 · Cessna U206F · AC Generator-Alternator
  > (CAN) ALTERNATOR WAS RETURNED DUE TO FAILURE TO CHARGE BATTERY AND HAD BEEN O/H. UPON INSP THE THROUGH BOLTS WERE FOUND LOOSE. THE STATOR HAD BECOME LOOSE BETWEEN THE HSG AND HAD BEEN SPUN BY THE ROTOR, BREAKING THE STATOR WIRES. A PLACARD ON ALTERNATORS STAT
- [SDR CA090818002](https://openairdocs.org/sdr/CA090818002.md): Ground Stud · broken · Aug 15, 2009 · Cessna U206F · Electrical Power System Wiring
  > (CAN) THE GROUND POST WAS FOUND BROKE OFF, THE ALTERNATOR WAS NOT PRODUCING A CHARGE, BATTERY DIED.
- [SDR CA090806010](https://openairdocs.org/sdr/CA090806010.md): Bolt · bent · Jul 12, 2009 · Cessna U206F · Nose/Tail Landing Gear
  > WE WERE IN CONTRACT WITH TC CONCERNING THIS INCIDENT AND THIS SEEMS TO BE THE ONLY WAY OF DEALING WITH THIS PROBLEM. AFTER THE INCIDENT REPORTED SDR 2009 0707010 THE SCISSORS LINK WAS INSPECTED AND BOLT P/N AN 4 -31 WAS FOUND BENT. BOLT PN NAS 6203-22D WAS FO
- [SDR CA090806008](https://openairdocs.org/sdr/CA090806008.md): Bolt · bent · Jul 12, 2009 · Cessna U206F · Main Landing Gear Strut/Axle/Truck
  > SORRY FOR THE DELAY BUT WE CONTACTED T.C. AND IT SEEMS THIS IS THE ONLY WAY TO ADDRESS THE PROBLEM. WHILE CHANGING TIRES, THE WHEEL BOLT P/N NAS 145-41 WAS FOUND LOOSE. WHEN REMOVED BOLT P/N NAS 146-43 WAS FOUND BENT. ALL BOLTS WERE REPLACED. THE DISTURBING
- [SDR CA090707010](https://openairdocs.org/sdr/CA090707010.md): Lock · failed · Jul 4, 2009 · Cessna U206F · Main Landing Gear
  > (CAN) LANDING, ACFT VEERED TO THE RT UNCONTROLLABLY. ACFT ENDED UP BEYOND APPROACH LIGHTS IN THE GRAVEL. NO DAMAGE TO ACFT AND ACFT LANDING GEAR IS BEING INSPECTED TO DETERMINE THE CAUSE. LOCKING DEVICE OR OLEO OVER INFLATED MAY BE CAUSE.
- [SDR CA090622010](https://openairdocs.org/sdr/CA090622010.md): Adapter · misrepaired · Jun 19, 2009 · Cessna U206F · Engine Starter
  > UPON INSP OF THE STARTER ADAPTER, WE FOUND THE WRONG MAIN SPRING AND STARTER SHAFT GEAR HAD BEEN INSTALLED. THE PN FOR THE SPRING USED WAS CAM539568 ALSO MEANT FOR USE IN THE "OLD STYLE" ADAPTER. THE COMPLETE ASSY, PN FOR THE "OLD STYLE" IS 635050A4 AND THIS
- [SDR CA090622012](https://openairdocs.org/sdr/CA090622012.md): Cylinder · cracked · Jun 18, 2009 · Cessna U206F · Reciprocating Engine Cylinder Section
  > (CAN) DURING INSP, IT WAS DISCOVERED THAT NR 2 CYL HAD LOW COMPRESSION, VALVE COVER WAS REMOVED AND IT APPEARED LEAK WAS COMING FROM EXHAUST VALVE SPRING. CYL WAS REMOVED ALONG WITH VALVES, FURTHER INSP REVEALED THAT EXHAUST PORT HSG WAS CRACKED. CYL ASSY W
- [SDR 2009FA0000327](https://openairdocs.org/sdr/2009FA0000327.md): Hinge Bracket · broken · Apr 15, 2009 · N206KL · Cessna U206F · Ailerons
  > LOWER SUPPORTING ANGLE CRACKED FROM MANY YEARS AND HOURS OF FATIGUE. THIS ACFT HAS BEEN OPERATED ON UNIMPROVED BACK COUNTRY DIRT LANDING STRIPS WHICH POUND AND SHAKE THESE ACFT EXTREMLY. THIS TYPE OF PART FAILURE IS TO BE EXPECTED UNDER THE CONDITIONS THIS A

Next page: https://openairdocs.org/model/cessna-u206f/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 = 'U206F'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/cessna-u206f/reports

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