Cessna U206B

Service difficulty reports · 25

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 = 'U206B'
  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 CA100601001Bungee · failed(CAN) STEERING BUNGEE FOUND VERY WEAK WHEN A/C NEW TO COMPANY BEING INSPECTED FOR ACCEPTANCE ONTO MSA. STEERING BUNGEE REPLACED BECAUSE OF PROBLEMS REPORTED LAST YEAR. IT IS BELEIVED THAT THE WEAK STEERING BUNGEE LEAD TO THE RUDDER CONTACTING THE AFT BULK HEMay 31, 2010 · Cessna U206B · Landing Gear Steering SystemSDR 2007FA0000155Cylinder · crackedCRACKED CYLINDER HEAD BETWEEN 4TH AND 5TH FIN IB OF TOP SPARK PLUG. CRACKS HEADED TOWARD VALVE SEAT. (K)Feb 12, 2007 · N4988F · Cessna U206B · Reciprocating Engine Cylinder SectionSDR CA060808006Fitting · cracked(CAN) DURING A 100 HOUR INSPECTION LOOSE RIVETS WERE NOTICED AROUND THE LT MAIN GEAR. ONCE THE FLOOR WAS LIFTED TO PERFORM THE REPAIRS, THE LT MAIN GEAR OB FITTING WAS FOUND TO BE CRACKED PROPOGATING FROM THE AFT END OF THE GEAR LEG OPENING TOWARDS THE AFT ENAug 4, 2006 · Cessna U206B · Fuselage, Landing Gear Attach FittingsSDR CA060710003Throttle Control · separated(CAN) DURING A SCHEDULED 50 HOUR INSPECTION THE THROTTLE CONTROL WAS FOUND TO BE SEPARATED AT THE SWAGE AREA JUST AFTER THE CLAMP AREA ON THE ROD END END ALLOWING THE CONTROL GUIDE TO MOVE ALONG WITH THE CONTROL END POSSIBLY RESULTING IN CONTROL JAMMING. (TC NJul 7, 2006 · Cessna U206B · Fuel Control/Reciprocating EnginesSDR CA060526004Impulse Coupling · brokenDURING FLT, PILOT NOTICED A VERY SLIGHT RPM DROP AND SLIGHT ROUGHNESS. UPON LANDING A GROUND RUN WAS PERFORMED AND WHEN THE IGNITION SWITCH WAS SELECTED TO RT MAG, ENGINE DIED OFF BEFORE SELECTING BACK TO LT OR BOTH. WHEN COWLS WERE REMOVED IT WAS EVIDENT THMay 19, 2006 · Cessna U206B · Magneto/DistributorSDR CA050712002Bearing · unserviceableWHILE FUNCTION CHECKING THE AILERON CONTROL SYSTEM PRIOR TO FLIGHT THEY BECAME HARD TO OPERATE. THE CO-PILOT'S CONTROL COLUMN BEARING ON OUTER SURFACE OF FIREWALL WAS FOUND TO BE UNSERVICEABLE. THE NEEDLE BEARINGS HAD DEPARTED THE CAGE. THE BEARING WAS REPLJul 7, 2005 · Cessna U206B · Control Column SectionSDR CA050616002Oil Cooler · cracked(CAN) DURING INSPECTION OIL WAS NOTICED TO BE LEAKING, THE SOURCE OF WHICH WAS DETERMINED TO BE THE OIL COOLER AS THERE WAS A CRACK ON THE WELD ALONG THE UPPER OUTER CORNER OF THE OIL COOLER. THE OIL COOLER WAS REPLACED WITH AN OVERHAULED UNIT.May 13, 2005 · Cessna U206B · Engine Oil CoolerSDR CA050413004Alternator · unserviceable(CAN) UPON CLIMB-OUT AFTER DEPARTURE NOTICED WHITE SMOKE COMING FROM THE LT SIDE OF THE AIRCRAFT AND THE SMELL OF BURNING IN THE COCKPIT. NOTIFIED THE TOWER OF THE EVIDENCE OF SMOKE AND RETURNED TO LAND UNEVENTFULLY. UPON INVESTIGATION IT WAS REVEALED THE ALApr 8, 2005 · Cessna U206B · Alternator-Generator DriveSDR CA040823BBFitting · cracked(CAN) DURING THE 100 HOUR INSPECTION THE RH MAIN GEAR OUTBOARD FITTING WAS FOUND CRACKED AT THE UPPER AFT RADIUS OF THE FITTING OPENING.THE FITTING WAS REPLACED IN ACCORDANCE WITH CESSNA'S RECOMMENDATIONS (OBTAINED FROM CESSNA) WITH A USED SERVICEABLE CUSTOMERAug 20, 2004 · Cessna U206B · Fuselage, Landing Gear Attach FittingsSDR CA031015014Doubler · cracked(CAN) HORIZONTAL ATTACHMENT POINT DOUBLER FORWARD RT CRACKED AT TOP NUTPLATE RIVET. DOUBLER REPLACED WITH NEW. AREA INSPECTED. NO OTHER FAULTS FOUND. CAUSE IMPROPER GROUND HANDLING (SPECULATION).Oct 2, 2003 · Cessna U206B · Horizontal Stabilizer, Plate/SkinSDR CA030731002Cable · broken(CAN) DURING TAXI OF AIRCRAFT ADVANCING THROTTLE WOULD NOT INCREASE ENGINE RPM. - INVESTIGATION SHOWED THROTTLE CABLE BROKEN IN ENGINE COMPARTMENT BETWEEN WIRE CABLE AT BASE OF SOLID PUSH ROD ON CONTROL ASSEMBLY (THROTTLE).Jul 13, 2003 · Cessna U206B · Power LeverSDR CA030528001Pump · failed(CAN) FAILURE OF VACUUM AIR PUMP ON DESCENT DURING UFR OPERATIONS. VANE FAILURE, DRIVE SHEARED.May 21, 2003 · Cessna U206B · Vacuum Distribution SystemSDR 2003FA0000015Bolt · looseINSPECTION IAW AD AND FOUND LOOSE BOLT HOLES FOR VERTICAL STABILIZER ATTACH. INSTALLED OVERSIZE BOLTS AND DYE CHECK, NO CRACKS FOUND, RETORQUED BOLTS DYE PENETRANT INSPECTION ITEMS.Sep 30, 2002 · N4994F · Cessna U206B · FastenersSDR AUS20021008Fitting · cracked(AUS) FORWARD FIN ATTACHMENT FITTING CRACKED IN AREA ADJACENT TO THE LH BOLT HOLE. FOUND DURING INSPECTION IAW AD/C206/7A4.Aug 30, 2002 · Cessna U206B · Fuselage, Stabilizer Attach FittingsSDR CA020530010Hinge Bracket · cracked(CAN) AILERON BRACKETS WERE LOOSE ON SPAR AND IN SKIN ATTACH. UPON EXAMINATION FOUND BOTH BRACKETS CRACKED AT REAR AND BOTTOM FLANGES. IT APPEARS THAT THE BRACKETS HAD BEEN LOOSE PREVIOUSLY AND REPAIRED BY SUBSTITUING CHERRY MAX THROUGH BOTTOM SKIN WHICH DID NMay 17, 2002 · Cessna U206B · AileronsSDR AU000847Angle · corroded(AUS) LEFT AND RIGHT WING FORWARD ATTACHMENT FITTING ANGLES CONTAINED INTERGRANNULAR CORROSION. (X)Sep 13, 2000 · Cessna U206B · Wing, Fuselage Attach FittingsSDR AU000815Angle · corroded(AUS) LEFT WING UPPER SPAR CAP ANGLE CONTAINED EXFOLIATION CORROSION. (X)Sep 12, 2000 · Cessna U206B · Wing SparSDR AU000814Angle · corroded(AUS) RIGHT WING LOWER SPAR CAP ANGLE CONTAINED INTERGRANNULAR CORROSION. (X)Sep 12, 2000 · Cessna U206B · Wing SparSDR AU000813Bulkhead · cracked(AUS) FORWARD DOORPOST BULKHEAD CRACKED ON LEFT AND RIGHT SIDES. (X)Sep 12, 2000 · Cessna U206B · Fuselage Main, BulkheadSDR 20000828SH029Nut · damagedDURING LANDING TOUCHDOWN, THE AIRCRAFT''S NOSE WHEEL DEPARTED AIRCRAFT. LOCAL PEOPLE, AT THE SITE, FOUND THE NOSE WHEEL AND ATTACHMENT BOLT ALONG WITH OTHER ATTACHMENT HARDWARE. (THE AN6-58A NOSE WHEEL BOLT REVEALS NO SIGNS TO THREAD DAMAGE. ADDITIONALLY, Jul 2, 2000 · N3488L · Cessna U206B · Nose/Tail Landing GearSDR CA990715032Rib · cracked(CAN) THE CENTER RIB AT WS 190.0 OF RT WING FOUND CRACKED AT TRAILING END THAT IS RIVETED TO WING REAR SPAR. ALSO, FOUND SEVERAL LOOSE AND SMOKING RIVETS IN THIS AREA.Jul 5, 1999 · Cessna U206B · Wing, Rib/BulkheadSDR AU990086Static System · contaminated(AUS) STATIC SYSTEM CONTAMINATED WITH WATER. AIRCRAFT HAD BEEN PARKED IN THE OPEN DURING A RAIN STORM.Jan 28, 1999 · Cessna U206B · Pitot/Static SystemSDR 97ZZZX4728Cylinder · crackedNR 5 CYLINDER ASSY CRACKED ONE-THIRD AROUND STEEL BARREL APPROXIMATELY 1 INCH BELOW CYLINDER HEAD.Oct 11, 1997 · N3435L · Cessna U206B · Reciprocating Engine Cylinder SectionSDR 96ZZZX952Bulkhead · crackedANNUAL INSPECTION REVEALED BOTH LEFT AND RIGHT SIDES OF LOWER FORWARD DOORPOST BULKHEAD (PN 1213407-2) CRACKED AS SHOWN IN CESSNA SEB 93-5R1. ALTHOUGH ACFT IS BELOW THE 4,000-HOUR TOTAL TIME SHOWN IN SERVICE BULLETIN, EXTENSIVE FLOAT OPERATION AND PRIOR DAMAGFeb 15, 1996 · N3870G · Cessna U206B · Fuselage Main, BulkheadSDR 95ZZZX813Bolt · failedON LANDING ROLL-OUT, NORMALLY FIXED NOSE LANDING GEAR DRAG BRACE AFT ATTACH BOLT FAILED ALLOWING LANDING GEAR TO PARTIALLY RETRACT IN FORWARD DIRECTION. INSPECTION OF BOLT INDICATED THAT A PREVIOUS FRACTURE IN THE THREADED AREA EXISTED. PREVIOUS NLG MAINTENAJan 29, 1995 · N3817G · Cessna U206B · Main Landing Gear
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