Cessna U206A

Service difficulty reports · 18

Newest first. General aviation reporting is voluntary.

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 = 'U206A'
  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 RTEA2013F00000Distributor Gear · dislodgedENGINE RAN ROUGH WHEN ON AFFECTED MAGNETO ONLY. DURING RUNUP FOR ROUTINE SCHEDULED INSPECTION. ON DISASSEMBLY OF MAGNETO, DISCOVERED THE DISTRIBUTOR FINGER HAD DISLODGE FROM THE DISTRIBUTOR GEAR, CAUSING ERRATIC TIMING. HAVE SEEN THESE FINGERS COME SLIGHTLApr 1, 2013 · N4879F · Cessna U206A · Magneto/DistributorSDR CA120712008Pump · contaminated(CAN) PILOT FLYING IN CRUISE AND HEARD A LOUD BANG. ENGINE CONTINUED TO ROTATE FOR A SHORT PERIOD AND THEN SIEZED. UPON LANDING 2 LARGE HOLES WERE DISCOVERED IN THE CRANKCASE WHERE THE NR 3 & NR 4 CONNECTING RODS HAD COME THROUGH THE CRANKASE. UPON DISASSEMBLYJun 8, 2012 · Cessna U206A · Reciprocating Engine Oil SystemSDR 2010FA0001240Wire Harness · faultyENGINE MISFIRING AT ALL POWER SETTINGS. DIAGNOSED FAULT TO BE THE IGNITION HARNESS LEADS. UTILIZING AN EASTERN TECHNOLOGY IGNITION HARNESS TESTER. IT WAS DETERMINED ALL THE BOTTOM LEADS WERE EITHER INTERMITTENT OR NONFUNCTIONAL FOR BOTH MAGNETOS. INSTALLINDec 8, 2010 · N4879F · Cessna U206A · Ignition System WiringSDR RTE2010F00001Contact Breaker · inoperativeIT IS APPARENT THAT MFG MAGNETOS HAVE HAD THE CONTACT BREAKER ASSY REPLACED IAW SB2-06A, DATED 7/1/06 ARE EXPERIENCING RAPID INTERNAL TIMING CHANGES. THE CONDITION NOTED ON NUMEROUS ACFT EQUIPPED WITH 4300 AND 6300 SERIES MAGNETOS IS ALWAYS A TIMING ADVANCE OSep 1, 2010 · N4879F · Cessna U206A · Magneto/DistributorSDR CA040920002Spark Plug · broken(CAN) WHEN REMOVING NR 4 CYLINDER LOWER SPARK PLUG, BROKE COMPLETELY OFF, JUST ABOVE BASE AND BELOW HEX DRIVE PORTION.Sep 13, 2004 · Cessna U206A · Spark Plug/IgniterSDR AUS20040069Fitting · improper part(AUS) STATIC SYSTEM T FITTING UNAPPROVED PART. FITTING WAS A COMMERCIAL PRODUCT. PERSONNEL/MAINTENANCE ERROR. UNAPPROVED PART.Jan 13, 2004 · Cessna U206A · Pitot/Static SystemSDR 031311BClamp · crackedDURING PRE-PURCHASE INSPECTION FOUND RT EXHAUST PIPE CLAMP CRACKED AND BROKEN AWAY FROM SUPPORT.Nov 7, 2003 · N4879F · Cessna U206A · Engine Collector/Tailpipe/NozzleSDR 031311ABlock · crackedDURING PRE-PURCHASE EVALUATION FOUND VOR ANTENNA ON TOP OF VERTICAL STABILIZER LOOSE. FURTHER INVESTIGATION REVEALED ANTENNA MOUNT BLOCK P/N 0570026-1 CRACKED AND BROKEN IN 2 PIECES. PREVIOUS UNKNOWN PERSON HAD ATTEMPTED REPAIR OF PART WITH EPOXY.Nov 7, 2003 · N4879F · Cessna U206A · Visual Omnirange (VOR) SystemSDR 031311Pump · wrong partDURING PRE-PURCHASE EVALUATION FOUND DRY VACUUM PUMP INSTALLED AT ENGINE OVERHAUL APPROX 90 HOURS AGO. ORIGINAL PUMP WAS WET TYPE. ALL PLUMBING FOR WET PUMP WAS UTILIZED WITH DRY PUMP INSTALLED WITH NON STANDARD FITTINGS. NO APPROVAL FOR INSTALLATION OF DRY PUNov 7, 2003 · N4879F · Cessna U206A · Vacuum Distribution SystemSDR CA030915010Mount · cracked(CAN) CRACKS IN RADIUS OF ENGINE MOUNT SUPPORT.Sep 8, 2003 · Cessna U206A · Engine Mount SectionSDR T042003F00000Bulkhead · crackedTHIS BULKHEAD CRACKED BETWEEN THE MOUNTING HOLES OF THE RE-ENFORCEMENT AND OUTBOARD FLANGE. ONLY 2 CRACKS, PORT DID NOT FAIL FURTHER FOUND AT 100 HOUR INSPECTION.Nov 13, 2002 · N8091Z · Cessna U206A · Propeller Spinner SectionSDR WVBA2001031Control Cable · out of positionPILOT REPORTED UNCONTROLLABLE PITCH CONTROL AND LIMITED AILERON CONTROL. IN FLIGHT, AFTER TAKEOFF, WHICH RESULTED IN A CRASH LANDING. ON EXAMINATION OF THE AIRCRAFT IT WAS DISCOVERED THAT THE RIBBON CABLE ASSY FOR ELECTRICAL CONTROLS ON THE YOKE, HAD FOULED May 16, 2001 · N756DJ · Cessna U206A · Control Column SectionSDR AU001085Trim Tab · cracked(AUS) ELEVATOR TRIM TAB CRACKED AND FAILED IN THE AREA AROUND THE HORN. (X)Nov 9, 2000 · Cessna U206A · Elevator, Tab StructureSDR CA001027018Line · broken(CAN) AFTER LOADING PASSENGERS, AIRCRAFT STARTED TO TAXI. WHILE ON RUNWAY, PILOT HAD A FAILED BRAKE ON RT SIDE FOLLOWED BY A FAILURE ON THE LT SIDE. AIRCRAFT WAS PUSHED TO TAXIWAY. PASSENGERS HAD STEPPED ON BRAKELINES DURING BOARDING AND BROKEN THEM OFF. BOct 27, 2000 · Cessna U206A · Landing Gear Brake SystemSDR CA001027012Wheel · cracked(CAN) FLANGE ON INNER WHEEL HALF CRACKED CAUSING BRAKE TO JAM. AIRCRAFT HAD DIFFICULTY TAXIING. (X)Sep 29, 2000 · Cessna U206A · Wheel/Ski/FloatSDR 20000712SH012Housing · loosePILOT REPORTED ALTERNATOR INOPERABLE AT TAKEOFF POWER. AT IDLE, ALTERNATOR APPEARED TO OPERATE NORMALLY. UPON EXAMINATION, FOUND THE COARSE THREAD INTERNAL WRENCHING BOLTS HOLDING THE ALTERNATOR CASE HALVES WERE LOOSE, WHICH AT HIGH ENGINE RPM, CAUSED THE CJun 15, 2000 · N756DJ · Cessna U206A · DC Generator-AlternatorSDR AU970448Altimeter · error(AUS) ALTIMETER OT OF CALIBRATION - AT 5000FT THERE WAS A 500FT ERROR - AT 6000FT THERE WAS A 700FT ERROR - ALTIMETER IS OF CHINESE MANUFACTURE - FOUND DURING INSPECTION IAW AD/INST/8 AMDT3May 2, 1997 · Cessna U206A · Altimeter, Barometric/EncoderSDR 96ZZZX2150Cylinder · crackedNR 2, NR 6, NR 1, NR 3, AND NR 5 CYLINDERS WERE FOUND CRACKED AT INTAKE SEAT.Mar 20, 1996 · N4975U · Cessna U206A · Reciprocating Engine Cylinder Section
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