Textron T206H

Service difficulty reports · 157

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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 = 'T206H'
  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 2015FA0000241Cylinder Head · crackedACFT LOST POWER AND MADE EMERGENCY LANDING WITHOUT DAMAGED TO ACFT. INSPECTION REVEALED NR 5 CYLINDER CRACKED AND SEPARATED AT HEAD. REPLACED WITH NEW CYLINDER, O5K22680.Apr 20, 2015 · N72768 · Cessna T206H · Reciprocating Engine Cylinder SectionSDR 2015FA0000145Pump · faultyREMOVED DEFECTIVE ENGINE DRIVEN FUEL PUMP RG9080J9A/M, SN E3394 AND INSTALLED "DEFECTIVE" NEWLY O/H FUEL PUMP, PN RG9080J8A/M, SN E-1186 THE FUEL PUMP WOULD NOT MAINTAIN PROPER FUEL PUMP AT IDLE RPM. WE OBTAINED ANOTHER NEWLY O/H FUEL PUMP RG9080J8A/M, SN D-1Apr 13, 2015 · N630KS · Cessna T206H · Engine Fuel PumpSDR CA141114005Oil Filter · cracked(CAN) AFTER LANDING FOR FUEL PILOT NOTED A LARGE AMOUNT OF OIL WAS VISIBLE LONG THE ENTIRE LENGTH OF THE BOTTOM OF THE FUSELAGE. AN INVESTIGATION LED MAINTENANCE TO THE COOLING SHROUD ASSEMBLY FOR VACUUM PUMP. THE SHROUD HAD LOOSENED AND ROTATED COMING IN CONTNov 3, 2014 · Cessna T206H · Reciprocating Engine Oil SystemSDR 2014FA0000481Sending Unit · malfunctionedRECURRING PROBLEMS WITH FUEL QTY SENDING UNITS OF THE LT AND RT WING FUEL TANKS. 5 OCCURRENCE'S THIS FISCAL YEAR OF FAILED UNITS. FLOAT TYPE, ALL WORK PERFORMED IN REF TO 28-40-00, REV 18. THE FLEET OF 8 AIRCRAFT ACROSS THE COUNTRY HAVE FREQUENT PROBLEMS WITAug 14, 2014 · N51216 · Cessna T206H · Fuel Quantity IndicatorSDR A8XR2014081300479Indicator · malfunctionedRECURRING PROBLEMS WITH FUEL QUANTITY INDICATION. 3 FAILURES THIS FISCAL YEAR. 2 ADDITIONAL FAILURES OF ANOTHER ACFT AT THIS FACILITY. ALL WORK PERFORMED RE: 28-40-00, REV 15. THE FLEET OF 8 ACFT ACROSS THE COUNTRY HAVE FREQUENT PROBLEMS WITH FUEL QUANTITYAug 13, 2014 · N51824 · Cessna T206H · Fuel Quantity IndicatorSDR CA140130014Pump · erratic(CAN) FUEL PUMP OUTPUT PRESSURE ERRATIC CAUSING A ROUGH ENGINE IDLE BETWEEN 700-1000 RPM.Jan 29, 2014 · Cessna T206H · Fuel Boost PumpSDR CA140123004Timer · failed(CAN) PROP DE-ICE TIMER UNSERVICABLE. CUSTOMER HAS RARELY USED THIS SYSTEM ON THE ACFT SINCE NEW.Jan 22, 2014 · Cessna T206H · Propeller/Rotor Anti-Ice/De-Ice SystemSDR CA140124003Pump · malfunctioned(CAN) ENGINE DRIVEN FUEL PUMP HAS INCONSISTENT OUTPUT PRESSURE CAUSING A ROUGH IDLE.Jan 20, 2014 · Cessna T206H · Engine Fuel PumpSDR CA131205005Control Cable · worn(CAN) AILERON CARRY THROUGH CABLES 1260505-154 AND -160, WORN OR CHAFED TO BETWEEN 40 AND 50 PERCENT OF THE OUTER WIRES. THE AILERON CABLES WERE WORN AT THE PULLEYS AT WS94 IN BOTH LT AND RT WINGS,Dec 2, 2013 · Cessna T206H · Aileron Control SystemSDR CA131204004Selector Valve · leaking(CAN) PILOTS REPORTED THAT FUEL TRANSFERS BETWEEN FUEL TANKS WITH THE FUEL SELECTOR IN OFF POSITION. DISCOVERED WHEN LOOKING FOR A FUEL LOAD THAT SOMETIMES ONE TANK HAD MORE FUEL THAN OTHER. SEALS BYPASSING FUEL INTERNALLY. FUEL SELECTOR REPLACED WITH NEW.Nov 26, 2013 · Cessna T206H · Fuel Selector/Shut-Off ValveSDR 2013FA0000502Magneto · malfunctionedLT AND RT MAGNETOS EXPERIENCING REPEATED INTERNAL TIMING DRIFT DURING SHORT PERIODS OF OPERATION. ACFT ARE ON A 50 HOUR PHASE INSPECTION CYCLE. PILOTS REPORT DIFFICULTY STARTING ACFT, INSP RESULTS DETERMINE THAT MAGNETOS ARE CAUSE. REMOVAL OF MAGNETOS, DISASep 4, 2013 · N511HP · Cessna T206H · Magneto/DistributorSDR M2LA201309160001Clamp · brokenPILOT HAD DEPARTED AND SHORTLY AFTER TAKEOFF EXPERIENCED SMOKE IN THE CABIN. LANDED. INSTALLED NEW EXHAUST TAILPIPE ASSEMBLY V-BAND CLAMP.Aug 28, 2013 · N376ME · Cessna T206H · Engine Collector/Tailpipe/NozzleSDR M2LA2013F00169Clamp · brokenSHORTLY AFTER TAKEOFF, EXPERIENCED SMOKE IN THE CABIN. LANDED. INSTALLED NEW EXHAUST TAILPIPE ASSEMBLY V-BAND CLAMP, WHICH HAD BROKEN.Aug 28, 2013 · N376ME · Cessna T206H · Engine Collector/Tailpipe/NozzleSDR 2013FA0000457Magneto · failedMAGNETO INSTALLED. 337.4 HRS LATER, ENGINE HARD TO START, TIMING TO ENGINE OK. REMOVED AND SENT FOR EVALUATION AND FOUND INTERNAL TIMING OUT OF SPEC.Aug 9, 2013 · N551HP · Cessna T206H · Magneto/DistributorSDR 2013FA0000456Magneto · inoperative8540.2 HRS. MAGNETO INSTALLED. 8597.3 HRS ENGINE HARD TO START, FOUND MAGNETO INTERNAL TIMING INCORRECT.Aug 9, 2013 · N551HP · Cessna T206H · Magneto/DistributorSDR 2013FA0000455Magneto · inoperativeMAGNETO INSTALLED 337.4 HRS LATER BECAME ENGINE HARD TO START. TIMING TO ENGINE OK. REMOVED AND SENT FOR EVALUATION AND FOUND INTERNAL TIMING OUT OF SPEC.Aug 9, 2013 · N551HP · Cessna T206H · Magneto/DistributorSDR 2013FA0000454Magneto · inoperative8372.5 HRS MAGNETO INSTALLED. 8509.9 HRS ENGINE BECAME HARD TO START. RESET MAGNETO TO ENGINE TIMING AND REPLACED SPARK PLUGS. 8540.2 HRS ENGINE STILL HARD TO START. REMOVED MAGNETO AND SENT FOR EVALUATION. INTERNAL TIMING FOUND TO BE INCORRECT.Aug 9, 2013 · N551HP · Cessna T206H · Magneto/DistributorSDR 2013FA0000453Magneto · inoperative8372.5 HRS, MAGENTO INSTALLED. ENGINE BECAME HARD TO START. RESET MAGNETO TO ENGINE TIMING AND REPLACED SPARK PLUGS. ENGINE STILL HARD TO START. REMOVED MAGNETO AND SENT FOR EVALUATION. INTERNAL TIMING FOUND TO BE INCORRECT.Aug 9, 2013 · N551HP · Cessna T206H · Magneto/DistributorSDR 2013FA0000452Magneto · inoperative8540.2 HOURS, MAGNETO INSTALLED. 8597.3 HOURS ENGINE HARD TO START, FOUND MAGNETO INTERNAL TIMING INCORRECT.Aug 9, 2013 · N551HP · Cessna T206H · Magneto/DistributorSDR 2013FA0000183Pump · defectiveENGINE WILL NOT PERFORM PROPERLY DURING ENGINE START AND IDLE OPERATION. INSTALLED (4 DEFECTIVE NEW ENGINE DRIVEN FUEL PUMPS (PN 200F-5006) BY THE DIRECTION OF FIELD TECH. FINALLY RECEIVED MFG APPROVAL TO INSTALL A DIFFERENT MFR ENGINE DRIVEN FUEL PUMP O/H PNMar 13, 2013 · N204JH · Cessna T206H · Engine Fuel PumpSDR 2012FA0000766Fuel Line · leakingDETECTED AN ODOR OF FUEL DURING AVIONICS INSTALLATION. FOUND LINE LEAKING AT B-NUT ON SELECTOR VALVE. LINE IS INSTALLED BETWEEN SELECTOR VALVE AND RT FUEL RESERVOIR. R &R LINE. FOUND LINE MADE FROM TUBING SHOWING AN INTERNAL SEAM. COULD FEEL SEAM AT FLARENov 19, 2012 · N437CP · Cessna T206H · Aircraft Fuel Distribution SystemSDR 2012FA0000820Injector · failedAFTER INSTALLATION OF FACTORY REBUILT ENGINE. PERFORMED GROUND RUN OF ACFT, AT ALL SETTINGS THE ENGINE RAN TOO RICH, AND ADJUSTMENTS HAD NO EFFECT. ACFT WAS NOT AIRWORTHY. REMOVED FUEL SERVO FROM ENGINE, SENT OUT FOR REPAIR. REINSTALLED FUEL SERVO AFTER RENov 12, 2012 · N661HP · Cessna T206H · Fuel Injector NozzleSDR 2012FA0000475Servo · inoperativeAFTER INSTALLATION OF FACTORY REBUILT ENGINE, ENGINE PERFORMED NORMALLY FOR 28 HRS. THEN IT BEGAN TO RUN EXCESSIVELY RICH WITH BLACK SMOKE AT LOW RPM AND AT FULL POWER. MIXTURE CONTROL HAS NO EFFECT, AFTER LANDING, BOOST PUMP MUST BE TURNED ON IN ORDER TO KEJul 3, 2012 · N773HP · Cessna T206H · Aircraft Fuel Distribution SystemSDR CA120515005Pump · leaking(CAN) DURING INSPECTION FOUND FUEL PUMP DRIVE SEAL LEAKING. THE DRIVE CAVITY DRAIN LINE IS ROUTED ABOVE THE HEIGHT OF FUEL PUMP CAVITY DRAIN OUTLET PREVENTING LEAKING FUEL FROM DRAINING FROM THE CAVITY AND CAUSING FLOODING OF THE PUMP MOTOR.May 15, 2012 · Cessna T206H · Engine Fuel PumpSDR CA120508002Clamp · cracked(CAN) DURING INSPECTION FOUND TURBOCHARGER TAILPIPE CLAMP CRACKED.May 7, 2012 · Cessna T206H · Exhaust TurbochargerSDR 2012FA0000182Brushes · disintegratedALTERNATOR FIELD CIRCUIT BREAKER TRIPPED INTERMITTENTLY OVER LAST 25 HRS WITH VARIOUS INSTANCES OF RADIO NOISE. ALTERNATOR REMAINED FUNCTIONAL. SUSPECT POSSIBLE BRUSH FAILURE AND ELECTED TO REPLACE THE ALTERNATOR DURING AN ANNUAL INSPECTION. ALTERNATOR WAS DIApr 5, 2012 · N2095S · Cessna T206H · DC Generator-AlternatorSDR T22R2012032858301Retainer · brokenENGINE STARTED TO RUN ROUGH WITH POWER LOSS ON TAKEOFF CLIMB. RETURNED TO AIRPORT AND LANDED SAFELY. UPPER VALVE SPRING RETAINER BROKE APART WHICH ALLOWED EXHAUST VALVE TO DROP INTO CYLINDER COMBUSTION CHAMBER ON A NEW CYLINDER WITH 8.0 HOURS ON IT. EXHAUSTMar 28, 2012 · N707VT · Cessna T206H · Reciprocating Engine Cylinder SectionSDR CA120227005Coupling · broken(CAN) TAIL PIPE COUPLING BROKE ON OUTERBAND AT APPROXIMATELY THE 1:30 POSITION CAUSING THE TAIL PIPE TO FALL OUT OF POSITION.Feb 17, 2012 · Cessna T206H · Engine Collector/Tailpipe/NozzleSDR CA120113013Sprocket · broken(CAN) ON RIGGING CHECK, THE ELEVATOR TRIM SYS WAS MOVED THOUGH RANGE OF MOTION. THE SYSTEM BECAME LOOSE AND IT WAS DISCOVERED THAT THE SPROCKET SHAFT HAD BROKEN AT THE INSTALLATION ROLL PIN LOCATION. IT IS OUR BELIEF IT BROKE AT A PRE-EXISTING CRACK FROM FACJan 12, 2012 · Cessna T206H · Elevator Tab Control SystemSDR 2012FA0000126Fuel Control · failedSINCE INSTALLATION OF RE-MFG ENGINE WHICH INCLUDE ACCESSORIES. FUEL INJECTION SERVO AND FUEL PUMP, ENGINE IS NOW PRODUCING EXCESSIVELY HIGH FUEL FLOW FOR ENGINE OPERATION WHEN COMPARED TO HISTORICAL OPERATION AND IAW POH FOR THIS ACFT. ENGINE OPERATION/ RUNSAug 16, 2011 · N513HP · Cessna T206H · Fuel Control/Reciprocating EnginesSDR 2011FA0000479Impulse Coupling · bentDURING 500 HR MAGNETO INSPECTION, FOUND IMPULSE COUPLINGS OUT OF SPEC. POSSIBLY PAWL INTERFERENCE WITH WOODRUFF KEY DURING DISASSEMBLY CAUSING PAWL TO BEND PAWL RIVET AND INCREASE PAWL BOSS CLEARANCE.Jul 22, 2011 · N839SA · Cessna T206H · Magneto/DistributorSDR 2011FA0000328Control Unit · intermittentTHE ALTERNATOR FIELD CB POPPED SHORTLY AFTER ENGINE START, THEN CB RESET RESULTING IN NORMAL ALTERNATOR OPERATION FOR THE REMAINDER OF THE FLIGHT. THE PROBLEM REOCCURRED ON A SUBSEQUENT FLIGHT. CAREFUL TROUBLESHOOTING REVEALED NO APPARENT FAULTS. SB04-24-01May 24, 2011 · N2095S · Cessna T206H · DC Generating SystemSDR CA101101002Piston · corrodedAFTER REMOVING AN ENGINE CYL TO REPLACE AN EXAUST STUD, IT WAS NOTICED THAT THE PISTON HAD CORROSION ON IT. ALL CYLINDERS WERE REMOVED AND PISTONS INSPECTED. CORROSION WAS FOUND ON ALL PISTONS. THE CYLINDERS WERE REPAIRED AND NEW PISTONS AND RINGS INSTALLED.Oct 22, 2010 · Cessna T206H · Reciprocating Engine Power SectionSDR 2010FA0001223Tire · failedDURING LANDING ROLL THE PILOT EXPERIENCED AN ABNORMAL DRAG TO THE LT, OBSERVED THE LT MAIN TIRE HAD GONE FLAT AND CAME TO A STOP ON THE RUNWAY. THE ACFT WAS THEN TOWED TO THE HANGAR AND THE INSP PROCESS BEGAN. UPON INSP, IT WAS DISCOVERED THAT THE RUBBER USEOct 22, 2010 · N5219E · Cessna T206H · TireSDR CA100920001Shroud · chafedWHILE CONDUCTING A PHASE 2 INSP, EXCESSIVE EXHAUST DUCT WAS NOTED AROUND THE NR 2 CYLINDER EXHAUST ATTACH STUDS. 2 STUDS WERE PULLED LOOSE FROM THE CYLINDER. EXHAUST GASES WERE LEAKING INTO THE UNDER COWL AREA WITH BURN MARKS ON THE CYL COOLING FINS. THE CYLSep 19, 2010 · Cessna T206H · Reciprocating Engine Cylinder SectionSDR CA100812017Seal · leakingFOUND FUEL PUMP DRIVE SEAL LEAKING. THE FUEL PUMP DRIVE CAVITY DRAIN LINE IS ROUTED ABOVE THE HEIGHT OF THE FUEL PUMP PREVENTING LEAKING FUEL FROM DRAINING FROM THE CAVITY AND FLOODING THE PUMP MOTOR.Aug 12, 2010 · Cessna T206H · Engine Fuel PumpSDR 2010FA0000589Housing · failedHAD FAILURES OF THE HOUSING THAT CONTAINS THE STARTER DRIVE GEAR WITHIN A PERIOD OF 4 DAYS ON 2 SEPAATE ACFT. THE HOUSING THAT SURRROUNDS THE DRIVE GEAR CRACKED AND CAUSED THE DRIVE GEAR TO SHIFT AWAY FROM THE RING GEAR ON THE PROP TO WHERE THE GEARS WERE UNAJun 4, 2010 · N2383L · Cessna T206H · Engine StarterSDR 2010FA0000587Housing · crackedHAD FAILURES OF THE HOUSING THAT CONTAINS THE STARTER DRIVE GEAR WITHIN A PERIOD OF 4 DAYS ON 2 SEPARATE ACFT. THE HOUSING THAT SURROUNDS THE DRIVE GEAR CRACKED AND CAUSED THE DRIVE GEAR TO SHIFT AWAY FROM THE RING GEAR ON THE PROP TO WHERE THE GEARS WHERE UNJun 4, 2010 · N1746L · Cessna T206H · Engine StarterSDR CA091221005Case · broken(CAN) ON FIRST START OF THE DAY, STARTER WOULD ENGAGE BUT UNABLE TO CRANK ENGINE, GEAR GRINDING SOUND HEARD. VISUAL INSPECTION REVEALED SIGNIFICANT STARTER CASING RUPTURE (TC NR 20091221005)Dec 21, 2009 · Cessna T206H · Starter-GeneratorSDR 2009FA0001075Bellcrank · obstructedFLAP POSITION ARM BELLCRANK ASSY PN 1262060-1 HITS BRACKET ASSY PN 1262045-8 WHERE THE BRACKET ASSY ATTACHES TO SUPPORT PN 1260448-4. THE SUPPORT FLEXES WHEN HIT AND AREA HAS METAL SHAVINGS FROM THE EXCESSIVE CONTACT. SHAVINGS COULD CONTACT WIRING AND SWITCHESDec 21, 2009 · N541TC · Cessna T206H · Trailing Flap Position Indicating SystemSDR 2009FA0001074Bellcrank · obstructedFLAP POSITION ARM BELLCRANK ASSY. PN 1262060-1 HITS BRACKET ASSY. P/N 1262045-8, WHERE THE BRACKET ATTACHES TO SUPPORT PN 1260448-4. THE SUPPORT FLEXES WHEN HIT, AND AREA HAS METAL SHAVINGS FROM THE EXCESSIVE CONTACT. THERE IS NOT ENOUGH RIVET EDGE DISTANCE TODec 21, 2009 · N1739L · Cessna T206H · Trailing Edge FlapsSDR CA091216004Alternator · low(CAN) DURING INITIAL CLIMB-OUT "LOW VOLTAGE" ANNUNCIATOR ILLUMINATED, PILOT NOTED A DISCHARGE INDICATION ON THE AMMETER. UNEVENTFUL RETURN TO AIRPORT FOR LANDING. ALTERNATOR FOUND AT FAULT. (TC NR 20091216004)Dec 15, 2009 · Cessna T206H · AC Generator-AlternatorSDR CA091216006Fuel Nozzle · obstructed(CAN) ON APPROACH FOR LANDING PILOT REPORTED "ROUGHNESS" FROM THE ENGINE AT THE LOWER POWER SETTINGS. GROUND RUNNING CONFIRMED ROUGHNESS WITH BLACK SMOKE COMING FROM TAILPIPE. ONE OF THE FUEL NOZZLE ASSEMBLIES WAS FOUND TO HAVE FUEL DYE RESIDUE, "GUMMY DIRT"Dec 12, 2009 · Cessna T206H · Fuel Injector NozzleSDR 2009FA0000718Seat Track · misinstalledDURING 100 HR/ANNUAL INSP THE PILOTS OTBD SEAT TRACK (PN1210816-6) WAS FOUND TO HAVE BEEN INSTALLED INCORRECTLY (180 DEGREES OUT FROM THE INBD TRACK) THIS INSTALLATION WOULD NOT ALLOW THE PILOTS SEAT LOCKING PINS TO ENGAGE AND LOCK THE SEAT IN POSITION. (K)Aug 14, 2009 · N154HR · Cessna T206H · Fuselage, Seat/Cargo Attach FittingsSDR CA090506006Clamp · failed(CAN) TURBO TURBINE FLANGE EXHAUST V-BAND CLAMP FAILED AT T-BOLT CLAMPING SUPPORT. (CLAMP FAILED) FOUND ON WALKAROUND - PREFLIGHT INSPECTION A/C TTSN 2537.2 CLAMP SUSPECTED TTSN 2537.2Apr 24, 2009 · Cessna T206H · Exhaust Turbine System (Reciprocating)SDR CA090430004Control Cable · frayed(CAN) STRAIGHT FLIGHT STC NR SA00515DE RT RUDDER, ELEVATOR UP AND DOWN CONTROL CABLES FOUND TO BE WORN AND FRAYED AT DEFLECTION PULLEY CLUSTER - BETWEEN STA. 100.0 AND 112.0. CONDITION FOUND TO BE DUE TO CONTACT WITH FWD INBD GUIDE PIN. NEW CABLES WERE SUPPLMar 23, 2009 · Cessna T206H · Elevator Control SystemSDR 2009FA0000218Bracket · brokenDURING A 100 HR/ ANNUAL INSP THE AUTOPILOT PITCH TRIM SERVO BRACKET WAS FOUND TO HAVE BROKEN FREE FROM THE 90 DEGREE SUPPORT BRACKET THAT IT ATTACHES TO. THIS BRACKET IS A FACTORY INSTALLED PART FOR THE AUTOPILOT SYS AND IS RIVETED TO THE EXISTING AIRFRAME. Feb 16, 2009 · N923SD · Cessna T206H · Autopilot Trim ServoSDR 2009FA0000083Structure · crackedREMOVED CRACKED LT AND RT WING TIPS AND REPLACED WITH NEW PN`S 0723205-1 AND 0723205-20. REMOVED CRACKED ELEVATOR RT AND LT TIPS AND REPLACED WITH NEW PN`S 1234640-4 AND 1234640-3. REMOVED CRACKED HORIZONTAL STAB PLASTIC TIP ON RT SIDE & REPLACED WITH NEW. Feb 2, 2009 · N2457M · Cessna T206H · Wing Main, Frame StructureSDR 2009FA0000082Structure · crackedREMOVED CRACKED LT AND RT WING TIPS AND REPLACED WITH NEW PN`S 0723205-1 AND 0723205-20. REMOVED CRACKED ELEVATOR RT AND LT TIPS AND REPLACED WITH NEW PN`S 1234640-4 AND 1234640-3. REMOVED CRACKED HORIZONTAL STAB PLASTIC TIP ON RT SIDE & REPLACED WITH NEW. Feb 2, 2009 · N2457M · Cessna T206H · Wing Main, Frame StructureSDR OMKR2008-0002Unknown · unknownNEW AIRCRAFT FROM FACTORY. PERFORMED AD SEARCH DUE TO EXPORT REQUIREMENT DURING ANNUAL. FOUND CESSNA SUPPLIED AD LIST DID NOT MATCH LYCOMING SUPPLIED LIST, AND CESSNA HAD CHANGED 8 AD SIGN-OFFS FROM LYCOMING. CESSNA CONTACTED, AND SAID THEY HAD TO CHANGE LYNov 24, 2008 · N6197S · Cessna T206H · Standard Practices/Structures
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