Lycoming HIO-360-D1A

Service difficulty reports · 78

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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 engine_model_key = 'HIO360D1A'
  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 2026F00166Support Frame · crackedLEFT AFT AIRFRAME CLUSTER FITTING THAT ATTACHES TO REAR CROSSMEMBER, LANDING GEAR, AND TAIL-BOOM SUPPORT STRUT WAS FOUND CRACKED DURING A VISUAL PREFLIGHT INSPECTION. AIRCRAFT IS GROUNDED AND HAS NOT BEEN RETURNED TO SERVICE. FRAME REPLACEMENT IS REQUIRED. AIRJul 28, 2026 · N776LH · Hughes 269C · Fuselage Main, StructureSDR 2014FA0000546Magneto · failedCOMPLETE RT MAGNETO IGNITION FAILURE WITH NO OUTPUT. MAGNETO FAILED PRIOR TO SCHEDULED INSPECTION.Sep 13, 2014 · N645KA · Hughes 269C · Magneto/DistributorSDR BY8S2014092600566Magneto · failedCOMPLETE RT MAGNETO IGNITION FAILURE/NO OUTPUT. MAGNETO FAILED PRIOR TO SCHEDULED HOUR INSPECTION.Sep 13, 2014 · N645KA · Hughes 269C · Magneto/DistributorSDR FAA20140910000001Sensor · detachedTHE ENGINE STOPPED DUE TO LACK OF OIL. THE OIL TEMPERATURE SENSOR, AND CRUSH WASHER WERE FOUND HANGING BY ITS ELECTRICAL CONNECTOR INSIDE THE ENGINE COMPARTMENT. A REMOTE FILTER SYSTEM WAS INSTALLED ON THE ACFT 1298 HOURS PRIOR TO THE INCIDENT.Aug 23, 2014 · N34LB · Hughes 269C · Turbine Engine Oil SystemSDR 2011FA0000183Tail Rotor · damagedODOR OF BURNING LUBRICANT, EXCESSIVE VIBRATION, FORCED A SUCCESSFUL OFF AIRPORT LANDING. FOUND AFT "H" FRAME BEARING, PN 269A5050-56, SEIZED, OVERHEATED, DRIVESHAFT JAMMED FWD AGAINST BEARING, AFT BEARING SUPPORT BROKEN OFF FRAME, PN 269A5573-13, AND MISSING. Mar 18, 2011 · N958CP · Hughes 269C · Tail Rotor Drive SystemSDR 2010FA0001006Pin · wornDURING 200 HR INSP WEAR MARKS WERE FOUND ON THE BOTTOM OF BOTH FUEL TANKS, CAUSED BY ATTACH PIN PN MS20392-2C47 USED ON STRAP ASSY. PN 269A8329-23. DETAILED INSP FOUND WEAR TO BE CAUSED BY INSUFFICIENT PAD MATERIAL INSTALLED ON STRAP ALLOWING CONTACT BETWEEN TSep 17, 2010 · N8363C · Hughes 269C · Fuel StorageSDR NDF2009F00001Alternator · failedALTERNATOR FAILED IN FLIGHT. ALTERNATOR WAS INSTALLED DURING ENGINE O/H BY MFG.Aug 31, 2009 · N7511A · Scwzer 269D · DC Generator-AlternatorSDR CA090126006Bolt · brokenOPERATING A SCHWEIZER 269 C MODEL SERIAL NUMBER S1575 TSN 6449.5 THE CONICAL BRGS WERE REPLACE WITH NEW AT 6338.8 AND A NEW BOLT WAS INSTALLED AT THIS TIME P/N 269A6092-3 WHICH WAS PURCHASE NEW FROM SCHWEIZER ON. THE RETORQUE WAS CARRIED OUT AT 6416.1 TSN NO Jan 26, 2009 · Hughes 269C · Tail Rotor HeadSDR CA080212005Link · disconnected(CAN) THE COTTER PIN SECURING THE IDLE MIXTURE LINK BLOCK TO THE MIXTURE CONTROL ARM BECAME DISLODGED. THIS ALLOWED THE MIXTURE LINK BLOCK TO BECOME DISCONNECTED FROM THE MIXTURE CONTROL ARM. RESULTING A LOSS OF CONTROL OVER FUEL FLOW TO THE ENGINE AND THE ENGFeb 8, 2008 · Hughes 269C · Fuel Controlling SystemSDR 2007FA0000697Condenser · disconnectedSPRING CLIP ON TERMINAL WIRE CAME OFF ALLOWING WIRE TO DISCONNECT. (K)Jul 11, 2007 · N7508H · Hughes 269C · Magneto/DistributorSDR 2007FA0000688Bracket · looseALTERNATOR BRACKET LOOSE AT ENGINE BOSS. BOLT CAUSES DAMAGE TO ENGINE CRANKCASE WHEN LOOSE. FRETTING OF ARM AND ENGINE CRANKCASE OCCURS. (K)Jul 10, 2007 · N9988F · Hughes 269C · Electrical Power SystemSDR 2007FA0000561Bushing · wornENGINE MOUNTED THROTTLE LINKAGE BUSHINGS WORN. FOUND ON INSPECTION WITH EXCESSIVE PLAY. PROBABLY OCCURRED DUE TO EXCESSIVE VIBRATION OR LACK OF SUBRICATION. RECOMMENDATION TO PREVENT WOULD BE TO LUBRICATE MORE FREQUENTLY OR DIFFERENT DESIGN OF LINKAGE. (K)May 25, 2007 · N1666S · Hughes 269C · Engine ControlsSDR BS2R2120003Pulley Bracket · brokenONE OF THE TWO BELT DRIVE CLUTCH ACTUATOR CABLE PULLEY BRACKETS BROKE CLEAN ACROSS BETWEEN THE FRAME MOUNT HOLE AND THE PULLEY MOUNT HOLE DURING ENGAGEMENT OF THE ROTOR SYSTEM. DURING THE SUBSEQUENT TAKE OFF ATTEMPT THE ROTOR RPM WOULD BLEED OFF RAPIDLY DUE TONov 17, 2006 · N11047 · Hughes 269C · Engine/Transmission CouplingSDR CA060306008Fuel Control · malfunctioned(CAN) CANNOT UNJUST IDLE MIXTURE. REPLACED FUEL CONTROL. (TC NR 20060306008)Jan 12, 2006 · Scwzer 269D · Fuel Control/Reciprocating EnginesSDR CA060303016Valve · incorrectFUEL SYSTEM SENDER INCORRECT VALVE. REPLACED SENDER.Nov 25, 2005 · Hughes 269C · Fuel Quantity SensorSDR CA050825001Ring · failed(CAN) HEAVY OIL CONSUMPTION CYLINDER NR 3. OIL RING NOT PERFORMING ITS WORK. REMOVED AND SENT FOR REPAIR. REINSTALLED CYLINDER.Aug 17, 2005 · Hughes 269C · Reciprocating Engine Cylinder SectionSDR CA041124003Rotor Shaft · broken(CAN) ON RUN UP MAGNETO CHECK, FOUND LT MAG INOP. LT MAG REMOVED AND INSPECTED, ROTOR GEAR WAS FOUND SEPARATED FROM ROTOR SHAFT. RT MAGNETO WAS INSPECTED IN THE SAME AREA OF LT MAG FAILURE NO DEFECT FOUND. A NEW MAGNETO WAS INSTALLED IN LT POSITION RT MAGNENov 22, 2004 · Hughes 269C · Magneto/DistributorSDR CA060303015Indicator · failedOIL PRESSURE UNSERVICEABLE. REPLACED CLUSTER ASSEMBLY.May 30, 2004 · Hughes 269C · Engine Oil PressureSDR AUS20040413Bolt · separated(AUS) GOVERNOR LINKAGE BOLT SEPARATED. LOSS OF ENGINE CONTROL RESULTED IN AUTO ROTATION AND HEAVY LANDING WITH SOME MINOR DAMAGE TO THE AIRCRAFT.May 14, 2004 · Hughes 269C · FastenersSDR H592004F00000Spline · slippedLEVEL FLIGHT, THE TAIL ROTOR DRIVESHAFT STARTED SLIPPING. TAIL ROTOR DRIVESHAFT SPLINES STRIPED. ON FRONT HALF OF SHAFT, STUDENT ENTERED AN AUTOROTATION AND AIRCRAFT LANDED HARD AND RECEIVED SUBSTANTIAL DAMAGE.Feb 28, 2004 · N75070 · Hughes 269C · Tail Rotor Drive ShaftSDR AUS20040136Fuel Control · faulty(AUS) ENGINE FUEL CONTROL UNIT FAULTY. INVESTIGATION FOUND PRESSURE ON THE MIXTURE ARM CHANGED THE FUEL FLOW RATE CAUSING THE ENGINE TO STOP.Feb 27, 2004 · Hughes 269C · Fuel Control/Reciprocating EnginesSDR AUS20040085Seal · worn(AUS) ENGINE CRANKSHAFT SEAL LEAKING. INVESTIGATION FOUND SEAL HAD DISINTEGRATED AROUND THE SEALING LIP. THIS IS A REPLACEMENT SEAL AFTER THE SEAL FAILURE IN MDR 04/0084.Feb 8, 2004 · Hughes 269C · Reciprocating Engine Power SectionSDR CA031212006Drive Assy · corroded(CAN) PILOT REPORTED LOST ROTOR TACH INDICATION. ROTOR DRIVE CABLE WAS REMOVED FROM ITS OUTER SHEATH FOR INSPECTION AND WAS FOUND SNAPPED IN TWO JUST BEFORE IT ENTERS INTO THE TRANSMISSION. IT WAS REMOVED PREVIOUSLY DUE TO REPORT THAT ROTOR NEEDLE WAS BOUNCINGDec 10, 2003 · Scwzer 269D · Main Rotor Indicating SystemSDR CA030703013Engine · flamed out(CAN) SUDDEN ENGINE FLAMES AND A CONTINUOUS LOSS OF SUBSTANTIAL POWER. EMERGENCY LANDING CARRIED OUT. THE ENGINE IS UNDER INVESTIGATION BY TSB. ADDITIONAL REPORT TO FOLLOW.Jun 18, 2003 · Hughes 269C · Engine (Reciprocating)SDR AUS20030615Pinion Gear · failed(AUS) MAIN TRANSMISSION TAIL ROTOR DRIVESHAFT PINION FAILED IN AREA LOCATED JUST IN FRONT OF THE THREADED AREA ALLOWING THE TAIL ROTOR DRIVE TO SEPARATE. AIRCRAFT STRUCK THE GROUND CAUSING EXTENSIVE DAMAGE TO THE LANDING GEAR.Jun 9, 2003 · Hughes 269C · Main Rotor GearboxSDR 2003FA0000694Magneto · failedMAGNETO WAS REPLACED ON 5-27-03 WITH THIS MAGNETO. ON 5-28-03, WHILE PERFORMING MAGNETO CHECK, LEFT MAGNETO WAS DEAD. VERIFIED BY REMOING PRIMARY LEAD. CHECKED NEXT DAY AND STILL WAS NOT FUNCTION ING. REMOVED AND REPLACED MAGNETO.May 29, 2003 · N103WP · Scwzer 269D · Magneto/DistributorSDR AUS20030521Frame · cracked(AUS) FUSELAGE FRAME RT CLUSTER CRACKED.May 17, 2003 · Hughes 269C · Fuselage Main, FrameSDR CA030425007Shaft · undersize(CAN) FORWARD BEARING INNER RACE TURNING ON SHAFT.Apr 19, 2003 · Scwzer 269D · Main Rotor HeadSDR CA030425008Bearing · failed(CAN) BEARING INNER RACE TURNING ON PULLEY SHAFT.Apr 7, 2003 · Scwzer 269D · Main Rotor HeadSDR AUS20030482Coupling · worn(AUS) ENGINE TO TRANSMISSION DRIVE LOWER COUPLING WORN. COUPLING HAS A DIFFERENT SERIAL NUMBER TO THE LOGBOOK ENTRY. SUSPECT UNAPPROVED PART. PERSONNEL/MAINTENANCE ERROR.Mar 27, 2003 · Hughes 269B · Engine/Transmission CouplingSDR CA030311005Control Cable · stiff(CAN) FUEL CONTROL CABLE STIFF TO OPERATE. REPLACED CONTROL WITH NEW PART.Mar 5, 2003 · Scwzer 269D · Fuel Control/Reciprocating EnginesSDR CA030311006Belt · cracked(CAN) BELTS CRACKED TO FABRIC. BELT SET REPLACED.Mar 5, 2003 · Scwzer 269D · Passenger Compartment EquipmentSDR CA021031012Fuel Control · failed(CAN) FUEL INJECTOR WOULD NOT CUT OFF. ENGINE WOULD CONTINUE RUNNING. REPLACED FUEL CONTROL.Sep 6, 2002 · Scwzer 269D · Fuel Controlling SystemSDR AUS20020649Bearing · failed(AUS) MAIN ROTOR TRANSMISSION OUTPUT SHAFT BEARING DISINTEGRATED. TAILROTOR DRIVESHAFT TWISTED UP AT TRANSMISSION END.Jun 17, 2002 · Hughes 269C · Main Rotor GearboxSDR AUS20020610Bolt · broken(AUS) TAIL ROTOR FORK BOLT BROKEN IN HALF.Jun 15, 2002 · Hughes 269C · Tail Rotor HeadSDR CA021004005Bolt · broken(CAN) NOISE OF STARTER AT ATTEMPTED START. FOUND TWO MISSING AND TWO BROKEN BOLTS THAT HOLD MOTOR HOUSING TO DRIVE HOUSING. INDUSTRIAL GRADE HARDWARE WITH ONLY SHAKE PROOF WASHERS FOUND ON SERVICEABLE UNIT BEING INSTALLED. HARDWARE REPLACED WITH DRILLED HEAD BJun 12, 2002 · Scwzer 269D · Engine StarterSDR CA021003008Nut · loose(CAN) DAILY INSPECTION REVEALED CLUTCH OIL ON BELT DRIVE ASSEMBLY, STATIC LEAK. INVESTIGATION REVEALED LT THREAD NUT/SEAL RUNNER WAS LOOSE.May 1, 2002 · Scwzer 269D · Reciprocating Engine Rear SectionSDR AUS20011318Bracket · cracked(AUS) LOWER DRIVE PULLEY SUPPORT BRACKET CRACKED. ONE ATTACHMENT LUGSEPARATED.Dec 11, 2001 · Hughes 269C · Engine/Transmission CouplingSDR AUS20011251Damper · loose(AUS) LH REAR LANDING GEAR DAMPER UPPER CAP UNSCREWED AND SEPARATED FROM PISTON. SUSPECT CAUSED BY VIBRATION.Nov 19, 2001 · Hughes 269C · Main Landing Gear Strut/Axle/TruckSDR AUS20011055Frame · cracked(AUS) FUSELAGE FRAME CRACKED AT LT CLUSTER. FOUND VISUALLY AND CONFIRMED USING DYE PENETRANT INSPECTION. AIRCRAFT HAD OPERATED FOR 192.2 HOURS SINCE AD/HU269/57 AMDT2 WAS CARRIED OUT.AD/HU269/57 AMDT2 IS CARRIED OUT EVERY 200 HOURS.Sep 30, 2001 · Hughes 269C · Fuselage Main, FrameSDR 2001FA0000472Bearing · failedENGINE WAS REMOVED DUE TO METAL CONTAMINATION. FOUND NR 3 CONNECTING ROD BEARING FAILED. THE ENGINE DID NOT EXHIBIT SIGNS OF OIL STARVATION. CAUSE FOR THIS FAILURE COULD BE DELAMINATION OF THE ROD BEARING.Sep 12, 2001 · Reciprocating Engine Power SectionSDR CA010724034Blade · cracked(CAN) ON DAILY INSPECTION OUTBOARD PART OF BLADE SKIN WAS FOUND TO BE CRACKED. CRACK IS FORMED AROUND TIP BLOCK ON BLADE. THE CRACK IS APPROX. 3 INCHES LONG, STARTING FROM BEHIND ABRASION STRIP TO ABOUT MIDDLE OF BLADE.Jul 10, 2001 · Hughes 269C · Tail Rotor BladesSDR CA010724035Blade · damaged(CAN) ON INSPECTION OF OPPOSITE TAIL ROTOR BLADE, THIS TAIL ROTOR BLADE WAS FOUND TO HAVE NO ABRAISON STRIP ON LEADING EDGE OF BLADE. FURTHER INSPECTION REVEALED THAT FILLER WAS USED UNDER PAINT TO BUILD UP EDGE. BOTH BLADES WERE REMOVED AND SENT TO SCHWEIZER Jul 10, 2001 · Hughes 269C · Tail Rotor BladesSDR CA010727009Seal · leaking(CAN) OIL SEAL LEAKING IN RPM CABLE. REPLACE OIL SEAL PN CR 3687.Jul 7, 2001 · Scwzer 269D · Main Rotor GearboxSDR CA010727011Bearing · ratcheting(CAN) BEARING RACHET WHEN INSPECTION. REPLACE BEARING.Jul 7, 2001 · Scwzer 269D · Main Rotor HeadSDR CA010727014Bracket · cracked(CAN) BRACKET CRACK . REPLACE BRACKET.Jul 7, 2001 · Scwzer 269D · Heating SystemSDR CA010727008Shaft · broken(CAN) BROKEN TEETH ON SHAFT ON ENGINE ADAPTER SIDE. REPLACE SHAFT.Jun 7, 2001 · Scwzer 269D · Engine/Transmission CouplingSDR CA010727010Bearing · worn(CAN) BEARING WORN INSIDE. REPLACE ALL 3 GRIP BEAR IN SET.Jun 7, 2001 · Scwzer 269D · Main Rotor HeadSDR 20010420CW009Bearing · damagedAT 25 HOUR OIL CHANGE, FOUND METAL PARTICLES IN SUCTION SCREEN AND FILTER. ON INSPECTION, FOUND NR 2 MAIN BEARING HAD SPUN NEARLY CAUSING ENGINE FAILURE. CHECK SCREENS.Mar 16, 2001 · N7430F · Scwzer 269D · Reciprocating Engine Power SectionSDR AU001170Key · disintegrated(AUS) NO3 CYLINDER EXHAUST VALVE SPRING LOCKING KEYS SHATTERED BUT WERE STILL HOLDING THE SPRINGS IN PLACE. CAP PNO MS13998-3 ALSO HADSEVERAL CHIPS MISSING. THE VALVE SEAT WAS DAMAGED BEYOND LIMITS.FOUND DURING INSPECTION IAW LYCOMING SB 388B. NO EVIDENCE OFMEDec 8, 2000 · Hughes 269C · Reciprocating Engine Cylinder Section
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