Lycoming O-360-A1G6D

Service difficulty reports · 29

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 engine_model_key = 'O360A1G6D'
  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 2016FA0000371Accumulator · failedWHILE INSTRUCTOR PILOT PERFORMED EMERGENCY PROCEDURE TRAINING, SHUT DOWN AND SECURED THE LEFT ENGINE. UPON ATTEMPTING TO RESTART THE ENGINE, THE LEFT PROPELLER WOULD NOT UN-FEATHER. LANDED WITHOUT INCIDENT. MAINTENANCE CREWS DISCOVERED THE LEFT PROPELLER UNFEAAug 15, 2016 · N2007E · Beech 76 · Propeller Feathering/ReversingSDR CA150327019Seal · worn(CAN) DURING FLIGHT, PILOT REPORTED LANDING GEAR NOT EXTENDING, EMERGENCY EXTENSION CARRIED OUT SATISFACTORY. UPON INSPECTION FOUND HYDRAULIC LEAK AT NLG ACTUATOR, ACTUATOR INSPECTED AND FOUND O-RING UNSERVICEABLE, ACTUATOR SERVICED AND INSTALLED, GEAR SWING Mar 27, 2015 · Beech 76 · Landing Gear ActuatorSDR 2012FA0000463Accumulator · emptyTHE RT PROPELLER ACCUMULATOR WAS AT ZERO PSI AFTER LANDING. THE RT PROPELLER WAS UNABLE TO COME OUT OF FEATHERED POSITION IN FLIGHT.Jul 6, 2012 · N6704X · Beech 76 · Propeller Feathering/ReversingSDR 2012FA0000138Landing Gear · failedACFT SUFFERED 2 NOSE GEAR FAILURES IN JUST OVER A ONE YEAR PERIOD. FIRST FAILURE OCCURED 6/2/2010 AND SECOND OCCURED ON 1/19/2012.Jan 19, 2012 · N6045M · Beech 76 · Nose/Tail Landing GearSDR 2010FA0001067Muffler · unserviceableBAFFLE PLATE IN LT MUFFLER APPEARED TO BE OUT OF POSITION WHEN INSPECTED BY SHINING A FLASHLIGHT UP THE TAILPIPE. ON REMOVAL, IT WAS FOUND THAT THE BAFFLE PLATE WAS CRACKED AND WARPING IN A MANNER THAT COULD HAVE CREATED A SIGNIFICANT BLOCKAGE IN THE FLOW OF Sep 8, 2010 · N6011U · Beech 76 · Engine Noise SuppressorSDR CA071214011Bolt · missing(CAN) PILOT NOTICED ON PRE-FLIGHT, ABNORMAL ANGLE OF GEAR DOOR. IT WAS DISCOVERED THAT THE BOLT SECURING THE DOOR WAS MISSING. THIS STRESSED THE AFT BRACKET TO THE POINT OF CRACKING WHICH ALSO CAUSED THE DOOR TO CRACK ALONG THE BOLT HOLES. (TC NR 20071214011)Dec 14, 2007 · Beech 76 · Landing Gear DoorsSDR CA070621003Frame · separated(CAN) DURING TAXI PILOTS FELT THE RT WING DROP SUDDENLY AND HEARD A TIRE SKIDDING SOUND. THEY IMMEDIATELY STOPPED THE AIRCRAFT. MECHANICS FOUND THE LANDING GEAR A-FRAME HAD BROKEN FREE FROM THE MAIN LANDING GEAR TRUNNION. THE LANDING GEAR DID NOT COLLAPSE BUTJun 20, 2007 · Beech 76 · Wing SparSDR CA070621002Motor · contaminated(CAN) DURING APPROACH, PILOTS SELECTED LANDING GEAR DOWN, GEAR MOTOR CIRCUIT BREAKER POPPED AND GEAR WOULD NOT EXTEND. AN EMERGENCY EXTENSION WAS CARRIED OUT SATISFACTORILY. AFTER RETURN TO BASE MECHANICS FOUND THAT THE HYDRAULIC MOTOR WAS CONTAMINATED WITH HJun 16, 2007 · Beech 76 · Hydraulic System, MainSDR CA070522006Control Cable · frayed(CAN) AIRCRAFT WAS IN THE HANGER FOR INSPECTION. AN INSPECTION WAS BEING STARTED IN THE AFT TAIL AREA. THE AME APPRENTICE NOTICED THE ELEVATOR TRIM CABLE SEVERELY FRAYED WHERE IT WRAPPED AROUND THE TRIM SERVO. THE CABLE WAS REMOVED AND REPLACED WITH A NEW PARTMay 20, 2007 · Beech 76 · Elevator Tab Control SystemSDR CA070129006Connector · disconnected(CAN) ADF INTERMITTENT NDB AND HEADING. AFTER SWAPPING RECEIVERS, ANTENNA, REPLACING ANTENNA TRAY AND CONNECTOR, REPLACING PINS IN RECEIVER TRAY, FOUND CO-AX CONNECTOR INNNER CORE TOUCHING SHIELDING AT RECEIVER TRAY. SNAG ONLY APPREARED WHEN WIRING HARNESS WASDec 21, 2006 · Beech 76 · Navigation System WiringSDR 2007FA0000033Starter · intermittentREPEATED TRYS, BENDIX FAILED TO ENGAGE. LUBRICATED AND INSPECTED BENDIX, FAILS TO ENGAGE EVERY OTHER TIME. IT STARTS (1) TIME THEN FAILS. (K)Dec 19, 2006 · N60156 · Beech 76 · Engine StarterSDR CA061108006Connector · contaminated(CAN) DURING TRAINING IN IMC CONDITIONS, ATC REPORTED TO STUDENT THAT HE WAS WAY OFF TRACK, PILOT CONFIRMED THAT HSI SYSTEM HAD FAILED. AIRCRAFT RETURNED TO BASE WITH HELP FROM ATC WITH NO OTHER INCIDENCE. MAINTENANCE DUPLICATED DEFECT, HSI SYSTEM INSPECTED ANNov 5, 2006 · Beech 76 · Navigation System WiringSDR CA060410009Channel · crackedDISCOVERED DURING INSPECTION. NLG ACTUATOR ATTACH BRACKET WAS FOUND CRACKED FROM THE EDGE OF THE BRACKET, THROUGH A LIGHTENING HOLE AND OUT THE OTHER SIDE. THE AREA IS DIFFICULT TO INSPECT. THIS IS THE SUPPORT CHANNEL THAT THE UPPER END OF THE NLG ACTUATOR Apr 1, 2006 · Beech 76 · Fuselage Miscellaneous StructureSDR AU510001756Piston Ring · deteriorated(AUS) ENGINE OIL FOUND TO BE VERY BLACK. INSPECTION FOUND THE PLASMA COATING ON THE TOP PISTON RINGS ON ALL FOUR CYLINDERS FRACTURED. (CASA NR 510001756)Dec 12, 2005 · Beech 76 · Reciprocating Engine Cylinder SectionSDR AU510001792Piston Ring · delaminated(AUS) ENGINE PISTON TOP COMPRESSION RINGS EXHIBITED SLIGHT SIGNS OF DELAMINATION. ENGINE OIL VERY DIRTY. PREMATURE WEAR ALSO FOUND ON EXHAUST VALVE ROTATING CAPS. (CASA NR 510001792)Dec 12, 2005 · Beech 76 · Reciprocating Engine Power SectionSDR AU510002202Plug · cracked(AUS) NOSE LANDING GEAR ACTUATOR END PLUG CRACKED IN AREA OF SPANNER FLATS. LOSS OF HYDRAULIC FLUID. (CASA NR 510002202)Dec 12, 2005 · Beech 76 · Landing Gear ActuatorSDR CA060509005Powerpack · failed(CAN) LANDING GEAR FAILED TO EXTEND. CREW ACTIVATED EMERGENCY EXTENSION. STILL NO INDICATION ON RT GEAR POSITION. SWITCHED BULBS ON GEAR INDICATOR AND DISCOVERED ONE BULB U/S. LANDING CARRIED OUT NORMALLY. FOUND HYDRAULIC POWER PUMP MOTOR BRUSHES WORN. RMay 17, 2005 · Beech 76 · Hydraulic System, MainSDR AUS20040056Damper · faulty(AUS) NOSE WHEEL SHIMMY DAMPER END CAP RETAINING CIRCLIP MISSING.Jan 23, 2004 · Beech 76 · Shimmy DamperSDR AUS20040033Motor · faulty(AUS) LANDING GEAR HYDRAULIC PUMP ELECTRIC MOTOR FAULTY. INVESTIGATIONFOUND BROKEN WIRE IN THE MOTOR WINDINGS.Jan 20, 2004 · Beech 76 · Landing Gear Retraction/Extension SystemSDR AUS20030937Hub · unserviceable(AUS) PROPELLER HUB DAMAGED IN AREA OF PRELOAD PLATE SHELF. PROPELLER HAD BEEN REMOVED AND DISMANTLED FOLLOWING GROUND STRIKE.Sep 15, 2003 · Beech 76 · Propeller Hub SectionSDR AUS20030881Hinge · corroded(AUS) RUDDER HINGE BRACKET CORRODED (RUSTED).Sep 1, 2003 · Beech 76 · Rudder/Tab, Attach FittingsSDR AUS20030783Actuator · cracked(AUS) NOSE LANDING GEAR ACTUATOR CRACKED AND LEAKING. INVESTIGATION FOUND A CRACK IN THE CYLINDER BODY END CAP THREAD ROOT LOCATED APPROXIMATELY THREE THREADS FROM THE SEALING CHAMFER.Jul 21, 2003 · Beech 76 · Landing Gear ActuatorSDR 2002FA0000981Rod End Bearing · separatedMETAL CONTAMINATION FOUND IN SUCTION SCREEN AND FILTER. DISASSEMBLY OF ENGINE NOTED BABBIT SEPERATION FROM NR 1 ROD CAP BEARING SHELL. THE REMAINDER OF THE OTHER ROD BEARINGS SHOWED SIGNS OF STARTING TO SEPARATE.Aug 13, 2002 · N66340 · Beech 76 · Reciprocating Engine Power SectionSDR AUS20020303Current Limiter · failed(AUS) PILOT EXPERIENCED COMPLETE LOSS OF ELECTRICAL POWER WHEN THE UNDERCARRIAGE WAS RETRACTED AFTER TAKE-OFF. INVESTIGATION FOUND THE BUS 1 AND 2 CURRENT LIMITERS BLOWN. FURTHER INVESTIGATION FOUND THE ALTERNATOR BLOCKING DIODE HAD AN UNSERVICEABLEINSULATOR TMar 28, 2002 · Beech 76 · DC Power Distribution SystemSDR CA020313003Brushes · worn(CAN) LANDING GEAR HYDRAULIC POWER PACK MOTOR DID NOT RUN. AIRCRAFT PUT ON JACKS & GEAR SELECTED UP, WITH A LIGHT TAP ON MOTOR GEAR RETRACTED NORMALLY WITHIN ALLOWABLE TIME LIMITS. SAME PROBLEM OCCURRED WHEN GEAR SELECTED BACK DOWN. INVESTIGATION REVEALED BRUSMar 2, 2002 · Beech 76 · Hydraulic Pump (Electric/Engine), MainSDR 2001FA0000392Bearing · departedIN STARTER DRIVE END CASTING, THE (FORWARD) BUSHING DEPARTED FROM THE CASTING THIS IS THE FORWARD PIVOT BUSHING/BEARING FOR THE BENDIX DRIVE SHAFT. 432.24 HOURS OF FLIGHT TRAINING, OVERHAULED BY MFG.Aug 16, 2001 · N6013M · Beech 76 · Engine StarterSDR CA010313017Spark Plug · damaged(CAN) IN CRUISE PILOT REPORT RT ENGINE SURGING, THEN COMPLETELY ROUGH RUNNING. ENGINE SHUTDOWN, AIRCRAFT LANDED SAFELY. COMPRESSION TEST REVEALED ONE WEAK CYLINDER 50/80 PSI. BOTH SPARK PLUGS IN THAT CYLINDER SHORTED DUE TO BEING PEENED OVER BY FOREIGN OBJECT Feb 15, 2001 · Beech 76 · Cylinder Head Temperature (CHT) Indicating SystemSDR CA010208012Circuit Breaker · intermittent(CAN) LANDING GEAR FAILED TO EXTEND WHEN GEAR SELECTED DOWN. GEAR WAS EXTENDED USING EMERGENCY PROCEDURES. AIRCRAFT WAS PUT ON JACKS HYDRAULIC POWER WOULD NOT RUN UNTIL CIRCUIT BREAKER WAS CYCLED.Jan 17, 2001 · Beech 76 · Landing Gear Retraction/Extension SystemSDR AU000727Carburetor · corroded(AUS) CARBURETOR FAULTY. INVESTIGATION FOUND STICKY NEEDLE AND SEAT ASSEMBLY, PLUNGER O''-RING FAULTY AND CORROSION ON THE INSIDE OF THE CARBURETOR COVER. (X)Sep 1, 2000 · Beech 76 · Fuel Control/Reciprocating Engines
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