Lycoming LTIO-540-J2BD

Service difficulty reports · 442

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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 = 'LTIO540J2BD'
  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 WVBA201405090090Housing · crackedAFTER SUCCESSFUL LANDING, PILOT REPORTED THAT THE LANDING GEAR WOULD NOT EXTEND AND HE HAD TO MANUALLY PUMP DOWN THE GEAR. MAINTENANCE EXAMINATION REVEALED THAT THE RT HYDRAULIC FILTER BOWL HAD RUPTURED IN THE THREADED PORTION APPROXIMATELY 0.25" ABOVE THE O-May 8, 2014 · N4082T · Piper PA31350 · Hydraulic System, MainSDR CA140228006Crankcase · cracked(CAN) DURING REPETITIVE TROUBLESHOOTING FOR REPORTED LT ENGINE OIL LEAK, MAINTENANCE FOUND ENGINE CRANK CASE CRACKED APPROXIMATELY 6" LONG, EXTENDING FROM NR 6 CYLINDER BASE, UPWARD INTO CASE. ENGINE WILL BE REPLACED.Feb 24, 2014 · Piper PA31350 · Reciprocating Engine Power SectionSDR CA140122009Stud · sheared(CAN) DURING INSPECTION FOR A REPORTED OIL LEAK, MAINTENANCE FOUND LOOSE NUT WITH PORTION OF A CYLINDER STUD ATTACHED IN THE LOWER ENGINE COWL. UPON INSPECTION FOUND THE NR 2 CYLINDER LOWER FORWARD CYLINDER MOUNT STUD SHEARED AT CYLINDER BASE. STUD REPLACEDJan 20, 2014 · Piper PA31350 · Reciprocating Engine Cylinder SectionSDR CA140123007Fitting · cracked(CAN) DURING ROUTINE INSPECTION MAINTENANCE FOUND THE FUEL SUPPLY HOSE, FROM FUEL TANK-TO-BOOST PUMP INLET, IN RT WING ROOT WITH HOSE FITTING SLEEVE-NUT PIECE BROKEN AWAY AND HOSE FITTING SLEEVE-NUT AT THE OTHER END WITH HOSE SLEEVE-NUT CRACKED. EVIDENCE OF SEJan 1, 2014 · Piper PA31350 · Aircraft Fuel Distribution SystemSDR KY7A20131218001Duct Clamp · looseENGINE LOST POWER DURING CLIMB & OTHER ACFT REPORTED EXCESSIVE EXHAUST SMOKE. SHUT DOWN & SECURED ENG & RETURNED FOR LANDING. FOUND A LOOSE CLAMP ON THE COMPRESSOR DISCHARGE COUPLING CAUSING INDUCTION AIR TO BE DISCHARGED PRIOR TO REACHING THE ENG INTAKE & CDec 18, 2013 · N66906 · Piper PA31350 · Exhaust TurbochargerSDR KY7A20131217002Linkage · loosePILOT REPORTED THAT HE LOST CONTROL OF E2 DURING CLIMB OUT, ENG WAS UNRESPONSIVE TO THROTTLE MOVEMENT. PILOT SHUT DOWN & SECURED ENG. MX FOUND THAT THE THROTTLE ADJUSTMENT LINKAGE WAS LOOSE ON THE SERVO, DUE TO IMPROPER INSTALLATION, CAUSING THE ADJUSTMENT SDec 17, 2013 · N66906 · Piper PA31350 · Power LeverSDR CA131219009Crankcase · cracked(CAN) DURING INSPECTION OF THE ENGINE IT WAS NOTICED THAT THE RT LOWER FWD RADIUS OF THE RT CRANKCASE WAS CRACKED.Dec 12, 2013 · Piper PA31350 · Reciprocating Engine Power SectionSDR 2013FA0000661Oil Cooler · cloggedRT. ENGINE, OIL TEMP REDLINE (HIGH), OIL PRESSURE LOW (REDLINE). ATTEMPTED TO SLOW ACFT AND UNCONGEAL OIL COOLER. THIS DID NOT HELP. PERFORMED PRECAUTIONARY SHUTDOWN. ON LANDING, MX INSPECTED FOR POSSIBLE OIL COOLER CONGEALING, DUE TO THE EXTREME OAT (-21°F)Nov 19, 2013 · N59826 · Piper PA31350 · Engine Oil CoolerSDR CA131115007Spring · failed(CAN) THE AFFECTED SPRING 71056-03 WAS IN COMPLIANCE WITH AD 98-08-18 AND WAS NOT DUE FOR MANDATORY REPLACEMENT, YET IT FAILED. 1 FACT THAT MAY HAVE CONTRIBUTED TO ITS PREMATURE FAILURE, THE ACFT DOES NOT HAVE A CONTROL LOCK AND IT HAD BEEN SOP TO LOCK THE COOct 20, 2013 · Piper PA31350 · Elevator Control SystemSDR CA131017013Plunger · failed(CAN) DURING RT ENGINE VALVE GUIDE INSPECTION, SB 388C, WE FOUND THE EXHAUST VALVE HYDRAULIC LIFTER, PLUNGER ASSY, PN78290, BREAK DOWN IN TWO PARTS. NO PROBLEMS WAS SUSPECTED ON THIS ENGINE. UNSERVICEABLE HYDRAULIC LIFTER HAS BEEN REMOVED FROM ENGINE. DURINOct 11, 2013 · Piper PA31350 · Reciprocating Engine Cylinder SectionSDR CA131115006Bolt · failed(CAN) THE PILOT COULD NOT GET THE GEAR TO RETRACT PROPERLY AND WAS ABLE TO GET IT BACK DOWN AND LOCKED. MAINTENANCE FOUND THE LT MAIN GEAR FORK BOLT SHEARED. THE SAME BOLT ON THE RT SIDE WAS REMOVED AND NO DEFECTS FOUND ON IT. BOLTS WHERE REPLACED ON BOTH GOct 8, 2013 · Piper PA31350 · Landing Gear ActuatorSDR CA131011004Wire · burned(CAN) IN FLIGHT CRUISE CONDITION PILOT REPORT ODORS OF SMOKE IN COCKPIT, EMERGENCY PROCEDURE, CLOSE MASTER ELECTRICAL SWITCH, TURN OFF SYS, TURN ELECTRICAL ON, EMERGENCY CALL AND LAND TO CLOSEST AIRPORT. FIRST INVESTIGATION, ALL ELECTRICAL SYS CHECK, AVIONIC Oct 5, 2013 · Piper PA31350 · Air Conditioning System WiringSDR CA130818001Stud · sheared(CAN) ALL BUT 1 CYLINDER BASE STUDS SHEARED OFF. CAUSING LOOSE NR 4 CYLINDER AND BROKEN FUEL INJECTOR LINE. ALSO FAILED EXHAUST SEGMENT.Aug 17, 2013 · Piper PA31350 · Reciprocating Engine Cylinder SectionSDR 9JNR20130832001Points · misinstalledINITIALLY INSPECTED AND TESTED MAGNETO PRIOR TO INSTALLATION, TESTS WERE SATISFACTORY. A GROUND RUN OF THE ENGINE AND MAGNETO OPERATION WAS ALSO SATISFACTORY. FAILURE OF MAGNETO OCCURRED APPROX 20 MINUTES INTO FLIGHT. ON INSPECTING THE MAGNETO AFTER REMOVALAug 15, 2013 · N811CB · Piper PA31 · Magneto/DistributorSDR CA130709013Turbocharger · failed(CAN) AT APPROXIMATELY 7000`, THE RT MANIFOLD PRESSURE STARTED DECREASING, AS MORE POWER WAS APPLIED, THE ENGINE STARTED SURGING. AS A PRECAUTIONARY MEASURE AN EMERGENCY WAS DECLARED. THE RT ENGINE BEGAN TO HAVE SIGNIFICANT DROPS IN MANIFOLD PRESSURE AND WASJul 5, 2013 · Piper PA31350 · Exhaust TurbochargerSDR CA130503001Pump · failed(CAN) PILOT REPORTED TO AMO THE MLG WAS SLOW TO RETRACT. AMO DISCOVERED THE LT HYDRAULIC PUMP FAILED THE TEST, AND REPLACED THE UNSERVICEABLE HYDRAULIC PUMP.Apr 26, 2013 · Piper PA31350 · Hydraulic Pump (Electric/Engine), MainSDR CA130409013Cylinder · separated(CAN) DURING INITIAL APPROACH CREW FELT SEVERE VIBRATION AND BANG FROM RT ENGINE. ENGINE IMEEDIATELY SHUTDOWN AND SECURED. MAINTENANCE FOUND NR 5 CYLINDER ASSY SHEARED FROM CRANKCASE BASE AND ALL 8 CYLINDER MOUNT STUDS SHEARED. CYLINDER WAS PUSHED INTO UPPERApr 1, 2013 · Piper PA31350 · Reciprocating Engine Cylinder SectionSDR CA130408010Cylinder · separated(CAN) FLIGHT CREW REPORTED LOUD BANG, VIBRATION FROM LT ENGINE DURING STABLE CRUISE POWER. IMMEDIATE ENGINE SHUTDOWN PROCEDURE CARRIED OUT. MAINTENANCE FOUND THE NR 2 CYLINDER HAD SEPARATED FROM THE ENGINE CRANKCASE WITH ALL 8 CYLINDER MOUNT STUDS SHEARED. Mar 7, 2013 · Piper PA31350 · Reciprocating Engine Cylinder SectionSDR CA130307004Cylinder Head · cracked(CAN) FORWARD CYLINDER NR 2 FOUND CRACK DURING MAINTEANCE, CRACK IS LOCATED AT TOP BASE THREADED PORTION UNDER EXHAUST PUSH ROD DEPRESSION. CRACK IS APPROXIMATELY 0,750" LONG THRU 3 COOLING FINS AND IS VISIBLE WITH PUSH HSG INSTALLED.Mar 6, 2013 · Piper PA31350 · Reciprocating Engine Cylinder SectionSDR CA121203012Control Cable · binding(CAN) THROTTLE CONTROL STIFF TO OPERATE.Nov 30, 2012 · Piper PA31350 · Power LeverSDR CA121123005Blade · failed(CAN) FLIGHT CREW REPORT ENGINE POWER ROLL BACK DURING CRUISE. ENGINE SHUTDOWN AND SECURED. MAINTENACE FOUND SEVERAL DAMAGED AND BLADE SECTIONS MISSING FROM TURBO COMPRESSOR. NO ENGINE INTERNAL ENGINE DAMAGE FOUND. TURBO REPLACED AND ACFT RELEASED FOR SERVICNov 21, 2012 · Piper PA31350 · Exhaust TurbochargerSDR CA121203010Throttle · binding(CAN) THROTTLE CONTROL STIFF AND GRINDING NOISE.Nov 16, 2012 · Piper PA31350 · Power LeverSDR CA121203011Controller · binding(CAN) LEFT PROP CONTROL STIFF TO OPERATE.Nov 16, 2012 · Piper PA31350 · Propeller Controlling SystemSDR CA121105022Piston Ring · failed(CAN) PILOT FIRST NOTICED MANIFOLD PRESSURE FLUCTUATE ON R/H ENGINE. GAUGES WERE NORMAL AT THIS POINT BUT AFTER TRYING TO ADJUST THROTTLE TO BRING MANIFOLD PRESSURE UP, OIL PRESSURE WENT DOWN. PILOT THEN SHUT DOWN R/H ENGINE AS A PRECAUTIONARY. MAINTENANCE DRANov 2, 2012 · Piper PA31350 · Reciprocating Engine Cylinder SectionSDR CA121015007Piston · damaged(CAN) ON LANDING, THE OIL PRESSURE ON THE LT ENGINE DROPPED TO 35 PSI WHEN THROTTLE AT IDLE. INSPECTION SHOWED OIL FROM BREATHER TUBE ON THE AIRFRAME. COMPRESSION CHECK IDENTIFIED THE NR 3 CYLINDER AT 0/80. CYLINDER REMOVED AND PISTON FOUND DAMAGED AT 2ND RIOct 10, 2012 · Piper PA31350 · Reciprocating Engine Power SectionSDR CA120918025Spar · cracked(CAN) LEFT ELEVATOR INSPECTED FOR CRACKS ON SPAR. CRACK FOUND APPROXIMATELY 7" INBD OF OUTER ELEVATOR HINGE BRACKET. ELEVATOR REMOVED, SPAR PN 40075-9, REMOVED. SPAR PN 40075-20 INSTALLED. ELEVATOR CHECKED FOR BALANCE AND REINSTALLED TO ACFT.Sep 14, 2012 · Piper PA31350 · Elevator, Spar/RibSDR CA120904010Bolt · broken(CAN) ON TAKEOFF LT MAIN GEAR UPPER TORQUE LINK BOLT FAILED CAUSING THE TIRE TO PIVOT AND DAMAGED THE TIRE.Aug 27, 2012 · Piper PA31350 · Landing Gear Retraction/Extension SystemSDR CA120823009Bearing · worn(CAN) DURING SCHEDULED MAINTENANCE, 100 HR INSPECTION, IN ADJUSTING POINTS, THE AME NOTICED BRASS SHAVINGS OR DEBRIS IN THE MAGNETO. CLOSER INSPECTION SHOWED THAT ONE GEAR AXLE HAD EXCESSIVE SIDE TO SIDE PLAY DUE TO A FAILED TOP BEARING. PLAY IS APPROXIMATELAug 23, 2012 · Piper PA31350 · Magneto/DistributorSDR KY7A201207260001Exhaust Pipe · brokenPILOT REPORTED ENGINE FAILED ON CLIMBOUT. PILOT SECURED ENGINE AND RETURNED FOR UNEVENTFUL LANDING. MAINTENANCE PERSONNEL FOUND BROKEN FLANGE ON EXHAUST PIPE UPSTREAM OF TURBOCHARGER. ENGINE FAILURE CAUSE WAS LOSS OF EXHAUST SUPPLY TO TURBOCHARGER WHICH STARVEJul 26, 2012 · N106RE · Piper PA31350 · Engine Collector/Tailpipe/NozzleSDR 2012F00140Spark Plug · mismanufacturedINSTALLED NEW CRHB32E MASS ELECTRODE PLUGS 96.7 HOURS AGO. WHEN DIAGNOSING A ROUGH CLIMB POWER FOUND: 6 PLUGS WITH NO CONTINUITY. THE OTHER 6 MEASURED 1.424K OHMS, 1.266K OHMS, 1.394K OHMS, 1.427K OHMS, 1.123K OHMS, 2.166K OHMS. OF THOSE 6 PLUGS, 3 WERE FOUJul 20, 2012 · Spark Plug/IgniterSDR CA120711005Transmitter · erratic(CAN) CREW REPORTED LT OUTBOARD FUEL INDICATING 3/8 OF A TANK OF FUEL WHEN LT ENGINE MISSED AND LT FUEL BOOST PUMP LOW PRESSURE LIGHT ILLUMINATED. CREW SWITCHED TO INBD TANK. MAINTENANCE FOUND LT OTBD FUEL TANK EMPTY AND BOTH LT OTBD TANK, INBD & OTBD FUEL SJul 10, 2012 · Piper PA31350 · Fuel Indicating SystemSDR CA120709008Hsi · faulty(CAN) ON A ROUTINE FLIGHT, THE PILOT NOTICED ON THE CLIMBOUT THAT THE CO-PILOT ATTITUDE INDICATOR (ADI) WAS SLOW TO ERRECT AND LAZEY. MAINTENANCE REPLACED THE HSI, HORIZ SITUATION INDICATOR, AND GROUND FUNCTION CHECKED THE SYS SERVICABLE.Jul 6, 2012 · Piper PA31325 · Attitude and Direction Data SystemSDR WVBA2012F00119Fan · seizedENROUTE, PILOT BEGAN TO DETECT SMOKE. RETURNED TO DEPARTURE. DURING RETURN, PILOT SHUTDOWN ELECTRICAL SYS & LANDED WITHOUT INCIDENT. AFTER ELECTRICAL SYS WAS SHUTDOWN, PILOT NOTICED A DECREASE IN THE ODOR OF SMOKE. MX DISCOVERED THE LEFT INTERIOR VENT FAJun 26, 2012 · N59826 · Piper PA31350 · Air Distribution FanSDR CA120612013Piston · cracked(CAN) DURING THE EVENT 4 INSPECTIONS, THE AME WAS CARRYING OUT SB1233 LANDING GEAR ACTUATOR ROD-END REPLACMENT. THE AME NOTICED THAT THE LT MLG ACTUATOR PISTON, THREADED PORTION APPEARED CRACKED BY THE NU. UPON REMOVAL FROM THE ACFT, THE ACTUATOR WAS PROVEN Jun 12, 2012 · Piper PA31350 · Landing Gear ActuatorSDR CA120612014Fork · sheared(CAN) IN THE PROCESS OF REMOVING THE ACTUATOR FROM LT MLG, THE AME FOUND THE MAIN GEAR LOCK ROD ATTACHMENT FORK, ITEM -18, PN 41789-00, SHEARED IN HALF, AND IT CAME APART IN THE AME`S HANDS.Jun 12, 2012 · Piper PA31350 · Landing Gear ActuatorSDR CA120612010Controller · leaking(CAN) FOUND OIL LEAKING FROM RT ENGINE INTAKE MANIFOLD PLENUM DRAIN. MAINTENANCE INVESTIGATION REVEALED OIL COMING FROM THE RT ENGINE DIFFERENTIAL PRESSURE CONTROLLER INTERNALLY LEAKING OIL INTO ENGINE INTAKE MANIFOLD. CONTROLLER REPLACED AND NO FURTHER LEAKJun 11, 2012 · Piper PA31350 · Reciprocating Engine Cylinder SectionSDR CA120606008Engine · making metal(CAN) HEAVY METAL FLAKES CONTAMINATION FOUND IN THE OIL FILTER & METAL CHUNK WITH FLAKES IN THE OIL SCREEN. METAL IS ALUMINIUM, NON MAGNETIC.Jun 6, 2012 · Piper PA31350 · Engine (Reciprocating)SDR CA120608007Tube · split(CAN) DURING TAXI OUT NOSE WHEEEL TIRE WENT FLAT. MAINTENACE REPLACED NW ASSY. INVESTIGATION REVEALED TIRE TUBE SIDEWALL SPLIT APPROXIMATELY .5".Jun 6, 2012 · Piper PA31350 · Tire TubeSDR T8VA20120605002Engine · shutdownDURING CRUISE AT 7000FT, THE RIGHT ENGINE BEGAN RUNNING ROUGH AND LOOSING POWER. THE ENGINE STALLED OUT AND COMPLETELY SHUT DOWN. FOLLOWED AIRCRAFT CHECKLIST AND ATTEMPTED TO RESTART THE ENGINE UNSUCCESSFUL. SECURED FAILED ENGINE ACCORDINGLY TO THE AIRCRAFTJun 5, 2012 · N713WT · Piper PA31350 · Engine (Reciprocating)SDR CA120605008Valve · failed(CAN) DURING TAKEOFF, THE CONTROL TOWER REPORTED BLACK SMOKE COMING FROM RT ENGINE AREA. PILOT COULD NOT GET ABOVE 30" MANIFOLD PR. FROM RT ENGINE. ACFT RETURNED AND ENGINE SHUTDOWN DRILL CARRIED OUT ON LANDING. MAINTENANCE FOUND RT ENGINE TURBO WASTE GATE Jun 1, 2012 · Piper PA31350 · Exhaust TurbochargerSDR CA120530011Tube · punctured(CAN) NW TIRE REPORTED FLAT DURING TAXI OUT FOR TAKEOFF. MAINTENANCE FOUND THE TIRE TUBE SPLIT APPROXIMATELY .2500" ALONG TUBE SIDEWALL. THIS IS A RECURRING PROBLEM WITH MULTIPLE REPEATS, ALWAYS WITH RELATIVELY NEW TIRES AND TUBES. INSTALLATION PROCEDURES RMay 30, 2012 · Piper PA31350 · Tire TubeSDR CA120530009Piston · cracked(CAN) WHILE CARRYING OUT SB1233, MAINTENANCE FOUND THE RT MLG ACTUATOR PISTON THREADED END SPLIT, CRACKED ABOUT 2500", LONGITUDINALLY. FROM THREADED END TOWARDS PISTON HEAD, ACTUATOR REPLACED.May 29, 2012 · Piper PA31350 · Landing Gear ActuatorSDR CA120504011Downlock · lack of lube(CAN) ON APPROACH TO LANDING, PILOT LOWERED GEAR. HAD GREEN DOWN LIGHTS ON NOSE AND LT MAIN GEAR BUT NOT ON RT MAIN. ABORTED LANDING CIRCLED AIRPORT WHILE TRYING TO GET GEAR DOWN WITH THE HYD PUMP AND BY USING THE HAND PUMP. DID NOT GET AN INDICATION ON RT May 3, 2012 · Piper PA31350 · Landing Gear Retraction/Extension SystemSDR CA120503003Fuel Nozzle · leaking(CAN) ACFT RETURNED AFTER T/O WITH LLT ENGINE INDICATING LT ENGINE EGT AND CHT TEMPERATURES AT RED LINE LIMITS. MAINTENANCE FOUND NR 5 CYLINDER FUEL INJECTOR LINE AND NOZZLE THREADS STRIPPED AND SLIGHTLY LEAKING. ALL OTHER CYLINDER FUEL INJECTOR NOZZLES FOUApr 27, 2012 · Piper PA31350 · Fuel Injector NozzleSDR CA120424009Cylinder · cracked(CAN) CYLINDER CRACK BARREL FROM HEAD FLANGE TOWARD CYLINDER ATTACHMENT FLANGE UNDER PUSHROD AREA. CYLINDER WAS REMOVED DUE TO LOW COMPRESSION PROBLEM, FOUND CRACK DURING REMOVAL. CRACK LENGTH 2.5". CYLINDER WAS INSTALLED NEW AT O/H AND WAS REMOVED DURING CApr 24, 2012 · Piper PA31350 · Reciprocating Engine Cylinder SectionSDR CA120223011Cap · fractured(CAN) DURING TROUBLESHOOTING BY MAINTENANCE FOR A HARD STARTING RT ENGINE, MAINTENACE FOUND ONE ENTIRE SIDE OF MAGNETO CAP FRACTURED AWAY. 2 SIDEWALL PIECES FOUND IN AFT LOWER COWLING. UNABLE TO DETERMINE CAUSE. MAGNETO PRESSURIZATION VALVE AND SYS CHECKED SFeb 23, 2012 · Piper PA31350 · Magneto/DistributorSDR CA120224003Nut · broken(CAN) DURING ENGINE GROUND RUN, IT WAS FOUND THAT THE RT ENGINE WOULD NOT MEET OIL OPERATING TEMPERATURE. MAINTENANCE FOUND THAT THE RT ENGINE OIL TEMP CONTROL VALVE SPRING RETAINING NUT WAS SHEARED OFF AND WAS FOUND IN OIL COOLER SUPPLY HOSE. THE VERNATHERM,Feb 21, 2012 · Piper PA31350 · Engine Oil TemperatureSDR CA120220005Hinge · damaged(CAN) ACFT RETURNED AFTER TAKEOFF WITH THE UPPER CABIN DOOR OPEN. NO FAULTS FOUND WITH DOOR LOCKING MECHANISM. DOOR UPPER FWD HINGE FOUND DAMAGED AND PULLED DUE TO BEING OPEN IN FLIGHT. SUSPECT THAT THE DOOR NOT LOCKED PROPERLY PRIOR TO TAKEOFF. UPPER DOORFeb 17, 2012 · Piper PA31350 · Fuselage, Door HingeSDR CA120210006Case · leaking(CAN) THE PILOT REPORTED RT ENGINE OIL LEAK. THE MAINTENANCE INSPECTION FOUND THE RT ENGINE, PN LTIO-540-J2BD CASE WAS CRACKED. THE CRACK IS LOCATED ON THE LT SIDE AT THE FWD BASE OF CYLINDER NR 2 AND IS APPROXIMATELY 4" IN LENGTH. ENGINE WILL BE REPLACED. Feb 8, 2012 · Piper PA31350 · Reciprocating Engine Power SectionSDR CA120206007Tube · split(CAN) NOSE WHEEL TIRE REPORTED FLAT DURING TAXI. MAINTENANCE REPLACED WHEEL/TIRE ASSY WITH SERVICEABLE ASSY, INVESTIGATION REVEALED A SPLIT IN THE TIRE TUBE SIDEWALL AREA APPROXIMATELY .5" IN.Feb 3, 2012 · Piper PA31350 · Tire Tube
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