Cessna 206H

Service difficulty reports · 86

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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 = '206H'
  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 2003FA0000237Indicator · inoperativeNEW AIRCRAFT, NEW HSI 345 HRS TTAF. GLIDESLOPE INOPERATIVE, FOUND GLIDESLOPE NEEDLE RESTRAINT (FROM TRANSPORT) STILL IN PLACE.Feb 28, 2003 · N3535T · Cessna 206H · Glide Slope SystemSDR CYM2002F00000Pin · corrodedRETAINING PIN FAILED CAUSING THE SPACER SUPPORTS, AND SHOCK STRUT ASSEMBLIES (RUBBER DONUTS) TO FALL OFF OF THE YOKE ASSEMBLY AS A RESULT OF THE RETAINING PIN FAILURE THE WHEEL WAS PERMITTED TO ENTER THE WHEEL WELL BEYOND ALLOWABLE LIMITS RESULTING IN THE FLOAOct 10, 2002 · N7270C · Cessna 206H · Main Landing GearSDR 2002FA0000551Gasket · failedDURING CRUISE FLIGHT LOST OIL PRESSURE INDICATION, MADE A PRECAUTIONARY LANDING ON A SNOW COVERED REMOTE RUNWAY, AIRCRAFT NOSED DOWN AND HAD A PROP STRIKE, BENDING BLADES. THE MECHANIC REMOVED THE ENGINE, DISCOVERED THE LOWER VACUUM PUMP GASKET WAS BLOWN OUT.Apr 1, 2002 · N7254H · Cessna 206H · Reciprocating Engine Oil SystemSDR 2002FA0000593Indicator · malfunctionedON AN ILS FREQUENCY, WITH A VALID SIGNAL THE UNIT WILL PULL THE FLAG BUT GIVE THE FLY DOWN COMMAND ALL THE TIME, EVEN WHEN IT SHULD BE CENTERED.Mar 8, 2002 · N2448Z · Cessna 206H · Directional Gyro and Indicating SystemSDR 20010418CW007Sprocket · maladjustmentEXCESSIVE LEFT RUDDER PETAL PRESSURE REQUIRED TO MAINTAIN STRAIGHT AND LEVEL FLIGHT. FOUND TRIM CHAIN TENSION ADJUSTMENT IDLER SPROCKET SLIPPED IN ADJUSTMENT SLOT. TRIM CHAIN JUMPED POSITION ON STEERING BUNGEE GEAR, CAMPING LIMITED LEFT RUDDER TRIM. RUDDER Apr 2, 2001 · N2446X · Cessna 206H · Rudder Control SystemSDR 20001222SH012Gear · spalledDURING INSP C/W AD 91-14-22 AND LYC SB 475 REV A, NO DAMAGE FOUND TO CRANKSHAFT COUNTERBORE RECESS, ALIGNMENT DOWEL, RETAINING BOLTS AND THREADS. UPON INSP OF CRANKSHAFT GEAR TEETH, SEVERAL WERE FOUND TO HAVE LINEAR PTTING WHICH APPEARED TO BE CAUSED BY PLATIDec 22, 2000 · N7273Q · Cessna 206H · Reciprocating Engine Power SectionSDR 20001129SH022Light · inoperativeOIL PRESSURE LIGHT IN ANNUNCIATOR PANEL IS OUT. SUBMITTER SUSPECTED BAD BULB. REMOVED AND REPLACED ANNUNCIATOR PANEL IAW CESSNA MM. OPERATIONAL TEST GOOD. (X)Sep 27, 2000 · N7266Y · Cessna 206H · Central WarningSDR 20001026SH007Cable Guard · inaccurateDURING THE INITIAL INSPECTION OF THE AILERON INTERCONNECT CABLE QUADRANT (RT AND LT) IAW CESSNA SB SB00-27-02, IT WAS DETERMINED THE REQUIRED RADIUS AROUND THE EDGE OF THE HOLE WHERE THE INTERCONNECT CABLE PASSES WAS NOT PRESENT. SUBSEQUENT INSPECTION OF THE Sep 25, 2000 · N7273Q · Cessna 206H · Aileron Control SystemSDR 20001026SH006Cable Guard · inadequateDURING INITIAL INSPECTION OF THE AILERON INTERCONNECT CABLE QUADRANTS (RT AND LT) IAW CESSNA SB SB00-27-02, IT WAS DETERMINED THE REQUIRED RADIUS AROUND THE EDGE OF THE HOLE WHERE THE INTERCONNECT CABLE PASSES WAS NOT PRESENT. SUBSEQUENT INSPECTION OF THE INTSep 25, 2000 · N7273Q · Cessna 206H · Aileron Control SystemSDR 20001026SH005Cable Guard · inadequateDURING INITIAL INSPECTION OF THE AILERON INTERCONNECT CABLE QUADRANTS (RT AND LT) IAW CESSNA SB SB00-27-02, IT WAS DETERMINED THE REQUIRED RADIUS AROUND THE EDGE OF THE HOLE WHERE THE INTERCONNECT CABLE PASSES WAS NOT PRESENT. SUBSEQUENT INSPECTION OF THE INTSep 20, 2000 · N7281M · Cessna 206H · Aileron Control SystemSDR 20001026SH004Cable Housing · inadequateDURING INITIAL INSPECTION OF THE AILERON INTERCONNECT CABLE QUADRANTS (RT AND LT) IAW CESSNA SB SB00-27-02, IT WAS DETERMINED THE REQUIRED RADIUS AROUND THE EDGE OF THE HOLE WHERE THE INTERCONNECT CABLE PASSES WAS NOT PRESENT. SUBSEQUENT INSPECTION OF THE INTSep 20, 2000 · N7281M · Cessna 206H · Aileron Control SystemSDR 20001129SH023Terminal · brokenOIL TEMPERATURE BULB CENTER WIRE TERMINAL POST SPINS IN HOUSING. SUBMITTER SUSPECTED FAULTY UNIT. REPLACED WITH SERVICEABLE UNIT FROM CESSNA, GROUND RAN ENGINE. OPERATION AND LEAK CHECKS GOOD. (X)Sep 15, 2000 · N7266Y · Cessna 206H · Engine Oil TemperatureSDR 20000913SH015Indicator · malfunctionedPILOT REPORTED CONTINUOUS TRIM INDICATOR MALFUNCTION. AFTER NUMEROUS ATTEMPTS TO RESET INDICATOR, A NEW PART WAS RECEIVED. THE TANG WHICH RIDES IN THE TRIM WHEEL WAS FOUND TO BE SHORT BY 50 PERCENT. NEW INDICATOR INSTALLED WITH NO FURTHER PROBLEMS. (X)Aug 27, 2000 · N631AF · Cessna 206H · Stabilizer Position IndicatingSDR 20001017SH035Pump · shearedRIGHT VACUUM PUMP FAILED, DRIVESHAFT SHEARED. (X)Aug 19, 2000 · N7273Q · Cessna 206H · Vacuum Distribution SystemSDR 20001013SH023Pump · shearedRIGHT VACUUM PUMP FAILED, DRIVESHAFT SHEARED. (X)Aug 14, 2000 · N2312V · Cessna 206H · Vacuum Distribution SystemSDR 20000809SH027Support Bracket · incorrectDURING ROUTINE INSPECTION, FOUND THE ALTERNATOR BELT DRIVE SUPPORT MISALIGNED WITH THE ALTERNATOR PULLEY CAUSING THE BELT TO SLIP PARTIALLY OFF OF THE ALTERNATOR PULLEY. FURTHER INVESTIGATION DETERMINED THE INCORRECT STARTER RING GEAR SUPPORT, PN 31M22045, WAJul 14, 2000 · N7254H · Cessna 206H · Alternator-Generator DriveSDR 20000720SH019Engine · failedPILOT REPORTED ENGINE SURGING ON TAKEOFF WITH SIGNIFICANT FUEL FLOW FLUCTUATION WHICH WAS CORRECTED WITH A DECREASE IN ENGINE POWER BY ADJUSTMENT OF THE PROP CONTROL AND ACTIVATION OF THE STANDBY ELECTRIC FUEL PUMP. POST-GROUND RUNS DUPLICATED THE PROBLEM, BUJun 5, 2000 · N7281M · Cessna 206H · Engine (Reciprocating)SDR 20000510SH002Line · defectiveDURING A 100-HOUR INSPECTION, THE FUEL LINE BETWEEN THE LEFT HEADER TANK AND THE FUEL SELECTOR WAS FOUND LEAKING AT THE FITTING. UPON REMOVAL, IT WAS DETERMINED THE FLARE WAS DEFECTIVE. (X)May 10, 2000 · N7273Q · Cessna 206H · Aircraft Fuel Distribution SystemSDR 20000720SH016Fuel Line · contaminatedPILOT REPORTED ENGINE SURGING ON TAKEOFF WITH SIGNIFICANT FUEL FLOW FLUCTUATION WHICH WAS CORRECTED WITH A DECREASE IN ENGINE POWER BY ADJUSTMENT OF THE PROP CONTROL AND ACTIVATION OF THE STANDBY ELECTRIC FUEL PUMP. POST-GROUND RUNS COULD NOT DUPLICATE THE PRMay 3, 2000 · N7254H · Cessna 206H · Aircraft Fuel SystemSDR 20000720SH018Engine · failedPILOT REPORTED ENGINE SURGING ON TAKEOFF WITH SIGNIFICANT FUEL FLOW FLUCTUATION WHICH WAS CORRECTED WITH A DECREASE IN ENGINE POWER BY ADJUSTMENT OF THE PROP CONTROL AND ACTIVATION OF THE STANDBY ELECTRIC FUEL PUMP. POST-GROUND RUNS COULD NOT DUPLICATE THE PRApr 25, 2000 · N7281M · Cessna 206H · Engine (Reciprocating)SDR 20000510SH004Propeller · leakingDURING A PRE-FLIGHT INSPECTION OF THE AIRCRAFT IN A HANGAR, THE PILOT FOUND A LARGE POOL OF RED OIL ON THE FLOOR BENEATH THE PROPELLER. UPON REMOVAL OF THE SPINNER, DETERMINED THE FLUID WAS LEAKING FROM UNDER A PROPELLER BLADE ROOT. THE PROP WAS REMOVED AND Apr 8, 2000 · N2312V · Cessna 206H · Propeller AssemblySDR 20000510SH006Line · defectiveDURING A 100-HOUR INSPECTION, THE FUEL LINE BETWEEN THE RIGHT HEADER TANK AND THE FUEL SELECTOR WAS FOUND LEAKING AT THE FITTING. UPON REMOVAL, DETERMINED THE FLARE WAS DEFECTIVE. (X)Apr 7, 2000 · N7273Q · Cessna 206H · Fuel StorageSDR 20000510SH003Nut · defectiveDURING A 100-HOUR INSPECTION, THE FUEL INJECTION LINE CLAMPS WERE FOUND SECURED WITH FIBER LOCK NUTS, OF WHICH THE FIBER LOCK WAS MELTED FROM THE HEAT OF THE ENGINE DURING OPERATION. ALL NUTS WERE REPLACED WITH ALL-STEEL LOCK NUTS, P/N MS21045. (X)Apr 7, 2000 · N7273Q · Cessna 206H · Engine Fuel DistributionSDR 20000626SH026Seal · leakingDURING PRE-FLIGHT INSPECTION OF THE AIRCRAFT IN A HANGAR, PILOT FOUND A LARGE POOL OF RED OIL ON THE FLOOR BENEATH THE PROPELLER. UPON REMOVAL OF THE SPINNER, DETERMINED THE FLUID WAS LEAKING FROM UNDER A PROPELLER BLADE ROOT. THE PROPELLER WAS REMOVED AND SApr 6, 2000 · N2312V · Cessna 206H · Propeller AssemblySDR 20000802SH010Governor · leakingDURING 100-HOUR INSPECTION, DISCOVERED PROPELLER GOVERNOR LEAKING FROM PLUG LOCATED ON THE TOP OF THE GOVERNOR. (X)Mar 22, 2000 · N2312V · Cessna 206H · Propeller GovernorSDR 20000802SH009Tank · leakingDURING 100-HOUR INSPECTION, DISCOVERED THE RT AUXILIARY FUEL TANK LEAKING FROM A JOINT WELD LOCATED ON THE TOP LEFT SIDE, AND LEAKING FROM THE AFT SIDE OF THE TANK WHERE THERE WAS EVIDENCE OF THE ELECTRODE TOUCHING THE TANK DURING ITS PRODUCTION, AND BURNING AMar 22, 2000 · N2312V · Cessna 206H · Fuel StorageSDR 20000802SH008Rib · crackedDURING 100-HOUR INSPECTION, DISCOVERED THE RT WING LEADING EDGE NOSE RIB LOCATED AT STA 136.00 CRACKED AT THE LIGHTENING HOLE. SUBMITTER SUSPECTED PART WAS DAMAGED DURING INITIAL INSTALL AT THE FACTORY ASSY LINE. (X)Mar 22, 2000 · N2312V · Cessna 206H · Wing, Rib/BulkheadSDR 20000620SH016Line · chafed**ISAAC, NADA, PART NAME, ETC.***FOUND FUEL PRESSURE LINE, PN 1250990-16, AND OIL PRESSURE LINE, PN 1250990-15, RUBBING IN ENGINE COMPARTMENT. THESE LINES RUN FROM FUEL DISTRIBUTOR MANIFOLD TO RT REAR BAFFLE AND RT FRONT OIL PASSAGE TO RT REAR BAFFLE. OIL PREMar 17, 2000 · N950HP · Cessna 206H · Engine Fuel DistributionSDR 20000802SH011Line · damagedDURING A 100-HOUR INSPECTION, FOUND FUEL LINE FROM FUEL BOOST PUMP TO LT HEADER TANK LEAKING AT THE HEADER TANK FITTING. UPON REMOVAL OF LINE, DISCOVERED DAMAGED FLARE. AIRCRAFT TT 288.7 HOURS. (X)Mar 13, 2000 · N7254H · Cessna 206H · Aircraft Fuel Distribution SystemSDR 20000802SH012Pump · inoperativePILOT REPORTED RIGHT VACUUM PUMP INOPERATIVE, ANNUNCIATOR LIGHT ILLUMINATED DURING FLIGHT. UPON REMOVAL OF THE VACUUM PUMP, DISCOVERED THE DRIVE COUPLING SHAFT SHEARED. (X)Mar 6, 2000 · N7273Q · Cessna 206H · Vacuum Distribution SystemSDR 20000802SH013Line · damagedDURING THE AIRCRAFT''S FIRST 100-HOUR INSPECTION, DISCOVERED FUEL LEAK AT FUEL SELECTOR VALVE AROUND FITTING ON FUEL LINE FROM SELECTOR TO LT HEADER TANK. UPON REMOVAL OF LINE, DISCOVERED DAMAGED FLARE. TOTAL AIRCRAFT TIME: 98.6 HRS. (X)Feb 23, 2000 · N7281M · Cessna 206H · Fuel Selector/Shut-Off ValveSDR 20000413SH048Seal · leakingDURING INITIAL 100-HOUR INSPECTION ON A NEW CESSNA 206H, FUEL WS FOUND LEAKING FROM THE RIGHT SIDE FUEL SENDER SCREWS. INSPECTION REVEALED LEAK EMANATING FROM IMPROPERLY SEALED NUT RING. AFTER REMOVAL, INSPECTION REVEALED TWO VOIDS BETWEEN NUT RING AND RIB. Feb 18, 2000 · N7264D · Cessna 206H · Aircraft Fuel Distribution SystemSDR 20000518SH013Circuit Breaker · failedDURING TROUBLESHOOTING OF KING KAP-140 AUTOPILOT SYSTEM, FOUND AUTOPILOT CIRCUIT BREAKER TO BE THE ''NON-PULLABLE'' TYPE CONTRARY TO THE PILOT OPERATING HANDBOOK EMERGENCY PROCEDURES FOR AUTOPILOT RUNAWAY **TONY, ISAAC PUT ENG IN SYS**TRIM INDICATION. UPON FLFeb 15, 2000 · N7273Q · Cessna 206H · Autopilot SystemSDR 20000518SH015Wire · shortedPILOT REPORTED SPARKS COMING FROM UNDER THE INSTRUMENT PANEL UPON ENERGIZING THE IGNITION SWITCH. UPON FURTHER INVESTIGATION, FOUND THE WIRE BUNDLE FOR THE CIRCUIT BREAKERS ADJACENT TO THE IGNITION SWITCH WAS TOO LONG AND A WIRE IN THE BUNDLE HAD CHAFED ON ANFeb 11, 2000 · N2312V · Cessna 206H · Ignition System WiringSDR 20000518SH014Shroud · crackedDISCOVERED OIL LEAK IN ENGINE COMPARTMENT COMING FROM RIGHT SIDE PUSH ROD TUBE SHROUD ON NR 5 CYLINDER ASSEMBLY. ON FURTHER INSPECTION, TUBE WAS FOUND CRACKED APPROXIMATELY ONE INCH DIAGONALLY THEN EXTENDING AROUND THE CIRCUMFERENCE OF THE TUBE (APPROX HALF WFeb 1, 2000 · N7281M · Cessna 206H · Reciprocating Engine Cylinder SectionSDR 99ZZZX2348Bolt · looseON PRE-FLIGHT, PILOT COULD NOT MOVE AILERONS TO LEFT. UPON INVESTIGATION, FOUND LT AILERON UPSTOP BOLT BACKED OUT LEAVING ONLY A 4 DEGREE TRAVEL. FOUND STOP NUT LOOSE, BUT HELD IN PLACE BY TORQUE PUTTY. RE-ADJUSTED STOP TO OBTAIN PROPER TRAVEL PER SM AND CApr 26, 1999 · N14122 · Cessna 206H · Aileron Control System
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