Continental IO-360-G

Service difficulty reports · 53

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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 = 'IO360G'
  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 CA150810002Clamp · malfunctioned(CAN) ON LANDING PILOT REPORTED GEAR DOORS OPEN BUT GEAR DID NOT FULLY EXTEND. THERE WAS NO GREEN GEAR DOWN LIGHT AND GEAR WAS NOT VISIBLE. ELECTRIC GEAR POWER PAK MOTOR WAS RUNNING CONTINOUSLY. THE PILOT DID A LOW OVERHEAD AND IT WAS NOTED THAT THE GEAR WAS HAug 7, 2015 · Cessna 337G · Landing Gear Door Retract SectionSDR CA140506006Drive Gear · cracked(CAN) OIL PUMP DRIVE GEAR FOUND CRACKED AT RADIUS BETWEEN GEAR FACE AND SHAFT. CRACK LENGTH IS APPROXIMATELY 1/3 THE CIRCUMFERENCE OF SHAFT. NO PREVIOUS HISTORY OF PROP-STRIKE. SUSPECTED OVER-TORQUE OF THE OIL PUMP DRIVE GEAR NUT OF 23.3-25.0 FT LBS.May 6, 2014 · Reciprocating Engine Oil SystemSDR CA131002004Clamp · broken(CAN) DURING OPS CHECKS OF THE ENGINE AFTER ENGINE INSPECTION, IT WAS NOTED THAT THE FRONT ENGINE LT MAG HAD A DROP OF 250. THE MAGNETO WAS REMOVED AND DISASSEMBLED FOR INSPECTION. IT WAS THEN NOTICED THAT THE CLAMPS THAT BOTH OF THE CLAMPS THAT HOLD DOWN THOct 1, 2013 · Cessna 337G · Magneto/DistributorSDR CA120507018Cable · frayed(CAN) INSPECTED FLAP CABLES AND FOUND FLAP CABLES 1460100-7 AND 1460100-8. FRAYED AT LOCATIONS SHOWN IN ALERT. CABLES R & R WITH NEW.Mar 16, 2012 · Cessna 337G · Trailing Edge FlapsSDR CA110707004Line · crackedPILOT REPORTED REAR ENGINE RUNNING TO LEAN CONDITION. NO MIXTURE ADJUSTMENT AVAILABLE. FOUND A CRACK IN THE NR 6 CYLINDER FUEL SUPPLY LINE TO NR 6 CYLINDER. REPLACED LINE WITH NEW LINE PN 630662, LEAK TESTED AND TEST FLIGHT PERFORMED, SATISFACTORY.Jul 5, 2011 · Cessna 337G · Engine Fuel DistributionSDR CA101214008Piston Rod · mismanufactured(CAN) PISTON ROD PURCHASE (NEW) AND RECEIVED - VISUALLY ACCEPTABLE. PISTON ROD MACHINED INCORRECTLY FROM MCCAULEY - WHEN TRYING TO INSTALL BETA TUBE THREW THE PISTON ROD IT WILL NOT ALLOW THE TUBE ALL THE WAY IN. THE PISTON ROD INSIDE DIAMETER IS TOO SMALL ANDec 14, 2010 · Propeller AssemblySDR 2010FA0000005Stud · damagedDURING THE TORQUE SEQUENCE FOR THE ENG O/H FINAL ASSY, FASTENERS ON THE ENG CASE WERE BROUGHT TO HALF THEIR FINAL TORQUE VALUES WITHOUT ISSUE IAW THE CURRENT MM AND PERTINENT SB`S. THEN WHILE ATTEMPTING TO REACH FINAL TORQUE VALUES, NOTED THAT MANY OF THE STUDec 18, 2009 · N337LC · Cessna 337G · Reciprocating Engine Cylinder SectionSDR 2009FA0000782Control Cable · frayedFOUND BOTH OF THE RT WING FLAP EXTEND CABLES WITH BROKEN INTERNAL WIRES. CABLES HAD TO BE REMOVED AND TWISTED AGAINST THEIR NORMAL WIND TO FIND THE TROUBLE. BOTH WERE DAMAGED AT THE POINT WHERE THEY GO AROUND THE BELLCRANKS IN THE WING, ABOUT 2 INCHES FROM THSep 10, 2009 · N1873M · Cessna 337G · Trailing Edge Flap Control SystemSDR CA090712001Valve · failed(CAN) ON LANDING, THE PILOT NOTED THE ACFT PULLED TO THE LT. AFTER LANDING, IT WAS NOTED THAT THE LT TIRE HAD A FLAT SPOT THAT MIGHT HAVE BEEN DUE TO BRAKE BEING ON. INSP OF THE PARKING BRAKE REVEALED THAT WHEN THE PARK BRAKE WAS PUT ON AND THEN TURNED OFF SJul 12, 2009 · Cessna 337G · Landing Gear Brake SystemSDR CA080918003Alternator · damaged(CAN) THE ACFT, A CESSNA 337G WAS ON A RETURN FLIGHT TO MAIN BASE WHEN THE PILOT NOTICED A INDICATION OF A FAILED FRONT ENGINE ALTERNATOR. THE ACFT LANDED WITHOUT INCIDENT AND MX INVESTIGATED THE PROBLEM. DURING REMOVAL OF THE FRONT ALTERNATOR, IT WAS DISCOVSep 17, 2008 · Cessna 337G · DC Generator-AlternatorSDR CA070823009Engine · failed(CAN) REAR ENGINE EXPERIENCED A LOSS OF OIL PRESSURE DURING FLIGHT. ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO BASE. ENGINE WAS REPLACED. UNABLE TO DETERMINE OIL PRESSURE PROBLEM WITH FAILED OIL PRESSURE ON ENGINE. ENGINE WAS SHIPPED TO ENGINE SHOP. (TC NRJul 24, 2007 · Cessna 337G · Engine Oil PressureSDR CA060508001Fuel Line · brokenSHORTLY AFTER TAKEOFF, THE PILOT OF A CESSNA 337 NOTICED THAT FUEL PRESSURE ON THE REAR ENGINE BEGAN TO DROP OFF AND THE ENGINE BEGAN TO RUN ROUGH. TURNED ON THE ELECTRIC BOOST PUMP AND THE ENGINE CONTINUED TO RUN NORMALLY. ELECTED TO RETURN TO THE AIRPORT ANMay 4, 2006 · Cessna 337G · Engine Fuel DistributionSDR SDR2006001Unknown · unknownWHILE HOLDING FOR TAKEOFF, NR 1 ENGINE FIRE WARNING INDICATION ACTIVATED. CREW DISCHARGED FIRE BOTTLE AS A PRECAUTIONARY PROCEDURE. PERFORMED FIRE DETECTION TEST AND FOUND OPERATING PROPERLY. (K)Jan 2, 2006 · N4AE · Aerosp ATR72212 · Fire DetectionSDR AU510001955Shaft · loose(AUS) LATERAL CYCLIC CONTROL BELLCRANK LOOSE. DISASSEMBLY AND INVESTIGATION OF THE TRANSMISSION FOUND THAT THE BELLCRANK MOUNTING SHAFT ATTACHED TO THE TRANSMISSION HAD NO SPLIT PIN WHICH ALLOWED THE NUT TO WORK LOOSE AND COME OFF THE SHAFT. THE NUT AND WASHERDec 9, 2005 · Hughes 269C · Main Rotor GearboxSDR CA051108010Circuit Breaker · arced(CAN) DURING APPROACH FLIGHT, PILOT SELECTED LANDING GEAR DOWN. LANDING GEAR CONTROL CIRCUIT BREAKER POPPED AND WOULD NOT RESET. PILOT WAS INSTRUCTED TO CARRY OUT AN EMERGENCY GEAR EXTENSION AND FOLLOW LANDING PROCEDURES IN PILOT'S OPERATING HANDBOOK. UPON Oct 28, 2005 · Cessna 337C · Landing Gear System WiringSDR CA051027005Ignition Lead · deteriorated(CAN) ON GROUND RUN, LT MAGNETO ON FRONT ENGINE HAD A 200 RPM DROP. DURING TROUBLESHOOTING FOUND NR 4 CYLINDER TOP LEAD SHORTING FROM INNER COIL THROUGH INSULATOR TO CAP. LEAD REPAIRED, AIRCRAFT RELEASED INTO SERVICE. AFTER A FEW HOURS OF FLIGHT, THE PROBLEM ROct 14, 2005 · Cessna 337G · Ignition Harness (Distribution)SDR CA050404009Crankcase · cracked(CAN) THE INITIAL PROBLEM WAS AN OIL LEAK FOUND DURING INSPECTION, AFTER SEVERAL ENGINE GROUND RUN-UPS, CRACK OF 2 INCHES FOUND FWD OF CYLINDER NR 5 ON CRANKCASE UPPER SECTION, ENGINE REMOVED AND SEND TO REPAIR SHOP.Apr 4, 2005 · Cessna 337G · Reciprocating Engine Power SectionSDR CA040130007Housing · cracked(CAN) ON INSPECTION OF ALTERNATOR HOUSING 2 RIBS WERE FOUND CRACKED COMPLETELY THROUGH. THERE HAVE BEEN TWO OTHER SIMILAR ALTERNATORS FOUND WITH CRACKED RIBS.Jan 6, 2004 · Cessna 337G · DC Generator-AlternatorSDR AUS20031296Hose · deteriorated(AUS) REAR ENGINE FUEL PRESSURE HOSE LOCATED BETWEEN FIREWALL AND FUEL MANIFOLD DETERIORATED AND LEAKING ONTO LT EXHAUST STACK.Nov 28, 2003 · Cessna 337G · Aircraft Fuel Distribution SystemSDR AUS20031318Control Cable · frayed(AUS) IB FLAP CABLE CONTAINED BROKEN WIRES LOCATED AT TIGHT BEND AROUND THE BELLCRANK. APPROXIMATELY 50 PERCENT OF THE WIRES WERE BROKEN. INSPECTION CARRIED OUT IN RESPONSE TO MFG ALERT.Nov 28, 2003 · Cessna 337H · Trailing Edge Flap Control SystemSDR CA031001009Control Cable · damaged(CAN) A SPECIAL INSPECTION WAS INITIATED TO COMPLY WITH REMOVAL AND INSPECTION OF FLAP CONTROL CABLES THAT ARE CONNECTED TO THE INBOARD FLAP BELLCRANK. CABLE P/N 1460 100-7 AND 1460100-8 WERE BOTH FOUND TO HAVE SEVERAL BROKEN STRANDS AND REQUIRED REPLACEMENT. Sep 23, 2003 · Cessna 337G · Trailing Edge Flap Control SystemSDR AUS20030912Structure · corroded(AUS) LT TAILBOOM LOWER STRUCTURE CORRODED IN AREA OF ATTACHMENT TO WING STRUCTURE. CORROSION IS BOTH INTERNAL AND EXTERNAL. RT TAILBOOM CONTAINED INTERNAL CORROSION ONLY.Sep 8, 2003 · Cessna 337G · Fuselage Main, StructureSDR CA030602001Control Cable · damaged(CAN) AFTER RECEIVING SDR ALERT AL-2003-05 AN INSPECTION WAS CARRIED OUT ON OUR 337G. TWO CABLES ON BOTH SIDES WERE FOUND DAMAGED. THE DAMAGE WAS LOCATED EXACTLY IN THE SAME LOCATION AS MENTION IN THE ALERT IE AROUND THE SHARP BEND OF THE BELLCRANK. ALL CABLESMay 30, 2003 · Cessna 337G · Trailing Edge Flap ActuatorSDR CA020611006Bevel Gear · failed(CAN) - VACUUM PUMP DRIVE NOT TURNING.- INSPECTION REVEALS NO TEETH ON DRIVE BEVEL GEAR.- METAL CONTAMINANTS CONTAINED INSIDE STARTER ADAPTER.- TCM SB 01-5 ADDRESSES PROBLEM.- TCM WARRANTS FULL REPLACEMENT.Jun 3, 2002 · Cessna 337G · Reciprocating Engine Rear SectionSDR LU42001F00002Bearing · failedRELEVANT INDICATION.Oct 17, 2001 · N11FT · Cessna 337G · Propeller AssemblySDR CA010627062Piston · broken(CAN) ON A GROUND RUN-UP PRIOR TO A SCHEDULED INSPECTION A PARTIAL POWER LOSS WAS DETECTED. A MOTO-STAT WAS CARRIED OUT AND #6 CYL. HAD VERY LOW COMPRESSION. A FILTER CHECK WAS CARRIED OUT AND SUBSTANIAL METAL PARTS, ALM, CHROME AND STEEL WERE FOUND THAT ARE CJun 18, 2001 · Cessna 337G · Reciprocating Engine Cylinder SectionSDR 20010605CW017Alternator · failedOWNER OF THIS AIRCRAFT EXPERIENCED FWD ENGINE ALTERNATOR FAILURE (AS INDICATOR BY FAILURE LIGHT) DURING FLIGHT. TECHNICIAN AND OWNER REMOVED ALTERNATOR FROM ENGINE AND DISCOVERED THE DRIVE SHAFT SHEARED. THE GEAR RETAINING BOLT HAD RUBBED INTERNALLY AND BUSMay 16, 2001 · N297DC · Cessna 337G · DC Generator-AlternatorSDR CA010504017Support Bracket · cracked(CAN) DURING A 100 HOUR INSPECTION IT WAS OBSERVED THERE WA A CRACK IN THE ABOVE MENTIONED BRACKET. A NEW BRACKET WAS INSTALLED AND AIRCRAFT RELEASED FOR RETURN TO SERVICE.Apr 16, 2001 · Cessna 337C · Rudder Control SystemSDR AU001098Gear · failed(AUS) VACUUM PUMP DRIVE GEAR FAILED. (X)Nov 21, 2000 · Cessna 337G · Reciprocating Engine Rear SectionSDR CA001228030Fuel Tank · cracked(CAN) WHILE BEING STORED IN A HANGAR RIGHT WING WAS DISCOVERED TO BE LEAKING FUEL. UPON FURTHER INSPECTION NR3 FUEL TANK P/N 1516132-16 HAD A CRACK ON TOP NEAR THE TRAILING EDGE. FUEL TANK WAS THEN REMOVED, REPAIRED AND REINSTALLED.Nov 15, 2000 · Cessna 337H · Fuel StorageSDR CA001211004Cam · cracked(CAN) DISCOVERED DURING A 100-HOUR INSPECTION. THE SHIMMY DAMPER ATTACH BRACKET WAS FOUND CRACKED. DUE TO THIS, THE LANDING GEAR (NOSE) WAS REMOVED AND THE STEERING CAM WAS SENT OUT FOR NDT. THE CAM WAS FOUND CRACKED AT THE LOWER FORWARD SHIMMY DAMPER ATTACH Oct 20, 2000 · Cessna 337H · Steering UnitSDR CA001211005Bracket · cracked(CAN) DISCOVERED DURING A 100 HOUR INSPECTION. THE TOP OF THE BRACKET WHERE THE SHIMMY DAMPER ATTACHES WAS FOUND CRACKED.Oct 20, 2000 · Cessna 337H · Landing Gear Steering SystemSDR CA000505013Crankcase · cracked(CAN) CRANKCASE FOUND TO BE A LIGHT DUTY CASE.ENGINE SHOP DISCARDED CASE AND REPLACED IT WITH A NEW HEAVY CASE.Apr 20, 2000 · Cessna 337B · Reciprocating Engine Power SectionSDR AU990090Piston · damaged(AUS) NR 6 CYLINDER PISTON DAMAGED DUE TO DETONATION. METAL CONTAMINATION OF THE ENGINE. ENGINE FACTORY REMANUFACTURED 457.1 HOURS PREVIOUSLY. PART TC: 457.Jan 27, 1999 · Cessna 337G · Reciprocating Engine Cylinder SectionSDR CA981027005Cylinder · cracked(CAN) DURING CRUISE, THE FRONT ENGINE HAD A CYLINDER FAILURE. THE CYLINDER WAS REPLACED AFTER LANDING.Oct 27, 1998 · Cessna 337D · Reciprocating Engine Cylinder SectionSDR CA981109010Crankcase · cracked(CAN) THE REAR ENGINE OF A 337G SKYMASTER WAS REPORTED AS RUNNING ROUGH. INSPECTION FOUND THE SPARK PLUGS FOULED, SO THE PLUGS WERE REPLACED. THE ENGINE RAN SMOOTH AND IT WAS RELEASED FOR RETURN TO SERVICE. ON THE SECOND FLIGHT WHEN POWER WAS REDUCED, THE ENOct 9, 1998 · Cessna 337G · Reciprocating Engine Power SectionSDR AU981084Cylinder · damaged(AUS) NR 2 CYLINDER ROCKER ARM SHEARED OFF AT ATTACHMENT POINT.Aug 20, 1998 · Cessna 337G · Reciprocating Engine Cylinder SectionSDR CA980602057Wing · bird strike(CAN) IN CRUISE, PILOT CAUGHT A FLASH OF MOTION AND HEARD A BIRD IMPACT WITH HIS LEFT WING. DAMAGE WAS VISIBLE FROM THE COCKPIT. WIRES WERE VISIBLE SO ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO BASE. DAMAGE WAS FOUND TO EXTEND FROM STN 204 TO 222. LEADINMay 15, 1998 · Cessna 337G · Wing Main, Frame StructureSDR CA980504019Bearing · corroded(CAN) PROPELLER RECEIVED FOR FIVE YEAR CORROSION INSPECTION. INSPECTION FOUND NR 1 BLADE BEARING RACE CORRODED. BEARING RACE REPLACED.Apr 29, 1998 · Cessna 337G · Propeller Blade SectionSDR CA980311016Blade · damaged(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. PROPELLER BLADES WERE REPAIRED IN THE FIELD AND FOUND TO BE BELOW MANUFACTURERS MINIMUM WIDTHS (LIMITS).Mar 3, 1998 · Cessna 337G · Propeller Blade SectionSDR 98ZZZX874Pump · failedFOLLOWING TAKEOFF, AIRSPEED SLOWED. REAR ENGINE INSTRUMENTS INDICATED ENGINE WAS LOSING POWER. OIL PRESSURE WAS DROPPING AND THE PROPELLER WENT INTO FEATHER. THE ENGINE WAS SHUT DOWN AND A LANDING WAS MADE. AN INSPECTION OF THE ENGINE DETERMINED THE OIL PUFeb 5, 1998 · N132CM · Cessna 337H · Reciprocating Engine Oil SystemSDR 97ZZZX3017Spring · brokenCUSTOMER COMPLAINED THAT UPON PERFORMING REAR ENGINE MAGNETO CHECK, ONE MAGNETO PRODUCED NO DROP, THE OTHER MAGNETO WOULD CAUSE ENGINE DECELERATE TO THE POINT OF STOPPING. MAGNETO'S WERE REMOVED AND INSPECTED. FOUND IMPULSE COUPLING SPRING BROKEN. THIS IS TJun 24, 1997 · Cessna 337G · Magneto/DistributorSDR CA970722043Gear Switch · bent(CAN) NOSE WHEEL RETRACTED AND COULD NOT BE EXTENDED DUE TO FAILURE OF THE SQUAT SWITCH BRACKET TO MAKE POSITIVE CONTACT WITH THE SWITCH. THE AIRCRAFT MADE A NOSE WHEEL GEAR UP LANDING.May 28, 1997 · Cessna 337G · Landing Gear Retraction/Extension SystemSDR CA960927007Alternator · broken drive(CAN) THE ALTERNATOR FAILED IN FLIGHT AND GROUND INSPECTION REVEALED THE DRIVE SHAFT HAD SHEARED.Sep 18, 1996 · Cessna 337G · DC Generator-AlternatorSDR CA960715011Alternator · broken shaft(CAN) THE ALTERNATOR DRIVE SHAFT FAILED AT THE BASE OF THE ALTERNATOR. THIS SHAFT APPEARED TO BE CRACKED OR HAD A PREVIOUS FLAW. THIS ALLOWED THE REMAINING SHAFT AND DRIVE GEAR TO MOVE FORWARD RUBBING ON THE CAM GEAR. THE RUBBER BUSHING, P/N 632050, AND METAL Jul 1, 1996 · Cessna 337G · DC Generator-AlternatorSDR CA960619031Counterweight Pl · broken(CAN) THE ENGINE DEVELOPED A SLIGHT VIBRATION INFLIGHT. THE ENGINE OIL PRESSURE & VACUUM SUCTION DROPPED TO ZERO. THE STANDBY VACUUM RESTORED SUCTION. THE ENGINE OPERATING TEMPERATURE INCREASED BUT STAYED IN THE GREEN. THE MANIFOLD PRESSURE WAS NORMAL. POST FLJun 10, 1996 · Mooney M20K · Reciprocating Engine Power SectionSDR CA960604003Cylinder · not firing(CAN)IN CRUISE AT 9.5K, ENGINE RAN ROUGH AND BACKFIRED, SHUTDOWN.May 24, 1996 · Cessna 337G · Reciprocating Engine Cylinder SectionSDR CA960502049Piston Pin · fractured(CAN) CLIMBING THROUGH 5,200 FEET, REAR ENGINE RPM STARTED FLUCTUATING 200-300 RPM. OIL PRESSURE DROPPED TO ZERO, ENGINE FEATHERED. ENGINE TEARDOWN REVEALED BROKEN PISTON PIN. SUPERIOR AIR PART.Apr 15, 1996 · Cessna 337G · Reciprocating Engine Cylinder SectionSDR CA960422008Cylinder Head · cracked(CAN)FRONT ENGINE #5 CYLINDER CRACKED APPROXIMATELY 3 INCHES LONG ACROSS THE ROCKER ARM CAVITY AREA.Apr 11, 1996 · Cessna 337G · Reciprocating Engine Cylinder SectionSDR CA960422009Bulkhead · cracked(CAN)REAR ENGINE PROP SPINNER BULKHEAD ASSEMBLY CRACKED IN NUMEROUS PLACES STARTING AT THE PROP MOUNTING HOLES RUNNING RADIALLY TO OUTER DIAMETER.Apr 11, 1996 · Cessna 337G · Propeller Spinner Section
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