Lycoming TIO-540-J2BD

Service difficulty reports · 868

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 = 'TIO540J2BD'
  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 CA121218013Bolt · missing(CAN) DURING INSPECTION, THE LT ENGINE TURBO ATTACH BOLTS FOUND MISSING. TURBO WAS FOUND RESTING AGAINST THE ENGINE MOUNT AND WAS BEING SUPPORTED BY THE EXHAUST PIPES AND TOP MOUNT BRACKET ONLY. WHEN RE-POSITIONED, INTAKE CASE WAS FOUND UNSERVICEABLE DUE TO Dec 3, 2012 · Piper PA31350 · Exhaust TurbochargerSDR CA121218014Exhaust Duct · cracked(CAN) DURING AN INSPECTION, THE LT AND RT ENGINE EXHAUST TRANSITIONS WERE FOUND CRACKED. BOTH TRANSITIONS REPLACED WITH SERVICEABLE TRANSITIONS.Dec 3, 2012 · Piper PA31350 · Engine Collector/Tailpipe/NozzleSDR CA121218015Plenum · cracked(CAN) DURING INSPECTION, THE RT AND LT FIBERGLASS TURBO INTAKE PLENUMS WERE FOUND CRACKED WITH A TEMPORARY SILICONE REPAIR. BOTH PLENUMS REPAIRED WITH FIBERGLASS.Dec 3, 2012 · Piper PA31350 · Engine Air Intake SystemSDR CA121218016Stud · broken(CAN) DURING PREPURCHASE INSPECTION, RT PROP DE-ICE STUD WAS FOUND UNSERVICEABLE DUE TO BEING BROKEN OFF. DE-ICE POWER WIRE FOUND ATTACHED TO OTHER STUD OR,"DOUBLED UP". STUD REPAIRED AND DE-ICE BOOT POWER WIRE RE-INSTALLED ONTO ORIGINAL POSITION.Dec 3, 2012 · Piper PA31350 · Propeller/Rotor Anti-Ice/De-Ice SystemSDR CA121218017Cable · kinked(CAN) DURING INSPECTION, THE LT ENGINE TACHOMETER CABLE WAS FOUND BADLY KINKED, WITH THE OUTER CASING STARTING TO UNWIND. TACH CABLE REPLACED WITH NEW CABLE.Dec 3, 2012 · Piper PA31350 · Engine RPM Indicating SystemSDR CA121218018Cable · misinstalled(CAN) DURING INSPECTION, THE FLAP DRIVE CABLE WAS FOUND INCORRECTLY ROUTED CAUSING CHAFING ON THE RT RUDDER CABLE AS WELL AS THE FUSELAGE. THE FLAP DRIVE CABLE WAS RE ROUTED AWAY FROM FROM RH RUDDER CABLE. BOTH SYSTEMS RECONNECTED, SAFETIED, AND FULL FUNCTIDec 3, 2012 · Piper PA31350 · Trailing Edge Flap Control SystemSDR CA121219006Selector · leaking(CAN) DURING INSPECTION, RT FUEL SELECTOR FOUND LEAKING, WITH VISABLE STAINING ON AIRFRAME. RT FUEL SELECTOR REMOVED, INSPECTED, ALL O-RINGS REPLACED, NEW ELBOW FITTING INSTALLED. LEAK CHECK WAS C/O, NO DEFECTS.Dec 3, 2012 · Piper PA31350 · Fuel Selector/Shut-Off ValveSDR CA121219007Seat Back · cracked(CAN) DURING PREPURCHASE INSPECTION, PILOT SEAT BACK WAS FOUND CRACKED ON LT REAR BACK SUPPORT. PILOT SEAT BACK REMOVED, UPHOLSTERY REMOVED. SEAT BACK WELD REPAIR C/O. PILOT SEAT REASSEMBLED, AND INSTALLED INTO ACFT. DEFECT RECTIFIED.Dec 3, 2012 · Piper PA31350 · Flight Compartment EquipmentSDR CA121219009Drain Line · missing(CAN) DURING INSPECTION, THE LT ENGINE WAS FOUND TO BE MISSING DRAIN LINES FROM THE FUEL PUMP AND THE HYDRAULIC PUMP. NEW DRAIN LINES INSTALLED, DEFECT RECTIFIED.Dec 3, 2012 · Piper PA31350 · Engine Fuel PumpSDR CA121219013Hinge · damaged(CAN) DURING INSPECTION, THE FORWARD BAGGAGE DOOR AFT HINGE WAS FOUND UNSERVICEABLE DUE TO MOUNTING BOLT HOLES BEING NOTCHED OUT, WITH NO EDGE DISTANCE REMAINING. BAGGAGE DOOR AFT HINGE REPLACED WITH NEW HINGE, PN 42541-000 TO RECTIFY DEFECT.Dec 3, 2012 · Piper PA31350 · Fuselage, Door HingeSDR CA121218011Cable · damaged(CAN) DURING PRE-PURCHASE, ANNUAL INSPECTION, AILERON AUTO PILOT ROLL SERVO BRIDAL CABLE FOUND UNSERVICEABLE. NEW MRP CABLE INSTALLED. RIGGING AND FUNCTIONAL CHECKS CARRIED OUT.Nov 29, 2012 · Piper PA31350 · Autopilot Main ServoSDR 2012FA0000756Screen · obstructedRIGHT ENGINE EXPERIENCED POWER LOSS AND ZERO OIL PRESSURE. PILOT FEATHERED AND SHUT DOWN ENGINE. AIRCRAFT SYSTEMS FOUND TO BE WORKING, (I.E. OIL PRESSUERE GAUGE) VISUAL INSPECTION OF OIL FILTER FOUND NOTHING. VISUAL INSPECTION OF SUMP SUCTION SCREEN FOUND A 9"Nov 7, 2012 · N1157S · Piper PA31 · Reciprocating Engine Oil SystemSDR CA121218012Cup · cracked(CAN) DURING INSPECTION, RT FUEL FILTER CUP FOUND LEAKING, CRACK FOUND IN BOWL NEAR SUMP DRAIN. FUEL FILTER CUP REPLACED WITH NEW FILTER CUP. LEAK CHECK C/O - NO DEFECTS.Oct 31, 2012 · Piper PA31350 · Aircraft Fuel Filter/StrainerSDR BSYA2012038Injector · pluggedJUST AFTER TAKEOFF FROM YIP, PILOT NOTICED POWER ON RIGHT ENGINE TO BE LOW AND WITH LOW READINGS ON THE EGT GAUGE. PILOT RETURNED AND LANDED SAFELY AT YIP WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND NR 2 AND NR 6 FUEL INJECTORS PLUGGED, MAINTENANCE CLESep 20, 2012 · N42HD · Piper PA31350 · Fuel Injector NozzleSDR CA120920004Exhaust Port · mismanufactured(CAN) WHEN THE CUSTOMER WAS ATTEMPTING TO INSTALL THE EXHAUST TAIL PIPE, THEY NOTICED THAT THE ID OF THE FLANGE ON THE TURBO WAS MACHINED INCORRECTLY. IT SEEMS THAT THE BEVELED PART OF THE ID WASN`T MACHINED DEEP ENOUGH, WHICH WOULDN`T ALLOW THE TAIL PIPE`S FSep 18, 2012 · Piper PA31350 · Exhaust TurbochargerSDR BSYA2012033Stud · brokenEN ROUTE FROM CLT TO ORL, APPROXIMATELY 90 MINUTES INTO THE FLIGHT THE RIGHT ENGINE STARTED BACKFIRING. THE PILOT PROCEEDED TO SHUT THE ENGINE DOWN AS A PRECAUTIONARY MEASURE AND DIVERTED TO SGJ AND LANDED SAFELY WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FSep 11, 2012 · N3587P · Piper PA31350 · Reciprocating Engine Power SectionSDR CA120905005Pump · failed(CAN) NEW FACTORY O/H FUEL BOOST PUMP INSTALLED AT LAST SCHEDULED MAINTENANCE. PUMP FAILED TO PRODUCE MORE THAN 5 PSI, 44 IS NORMAL ON START THIS MORNING. POWER TO PUMP SUFFICIENT, AND MOTOR RUNS, JUST NO REAL PRESSURE PRODUCED. TIME IN SERVICE IS 14 HOURS,Sep 5, 2012 · Piper PA31350 · Fuel Boost PumpSDR CA120822018Exhaust Valve · broken(CAN) THE ACFT HAD AN EXHAUST VALVE, PN LW-16740 BREAK ON LT ENGINE, NR 3 CYLINDER. THE BROKEN PARTS DAMAGED THE PISTON AND CYLINDER HEAD AND ALSO DAMAGED THE TURBOCHARGER, PN LW-12463 TURBINE WHEEL. THE PILOT REPORTED THE ENGINE SLOW TO SPOOL UP, HIGHER EGT,Aug 21, 2012 · Piper PA31350 · Reciprocating Engine Cylinder SectionSDR EPUA20120910001Switch · dirtyDURING APPROACH, AFTER LANDING GEAR SELECTED DOWN, RED LIGHT REMAINED ILLUMINATED, GREEN NOSE WHEEL LIGHT REMAINED EXTINGUISHED AND GEAR HANDLE DID NOT RETURN TO THE NEUTRAL POSITION. CYCLED THE GEAR ATTEMPTED WITH NO POSITIVE RESULT, DISCONTINUED APPROACH AAug 17, 2012 · N4501B · Piper PA31350 · Landing Gear Position and WarningSDR EPUA2012081001Uplock Roller · inoperativeNOSE LANDING GEAR STUCK WHEN LANDING GEAR DOWN SELECTED. NOSE GEAR TRAILED AT A 45 DEGREE ANGLE, RETRACTED OK, THEN WAS HARD TO GET OUT WHEN CYCLED DOWN AGAIN. MAINT SERVICED RESERVOIR AND REPLACED UPLOCK ROLLER.Aug 7, 2012 · N44AC · Piper PA31350 · Landing Gear Retraction/Extension SystemSDR BSYA20120724026Dipstick · unsecureSHORTLY AFTER TAKEOFF FROM FWA, PILOT NOTICED OIL STREAKING OUT OF RIGHT ENGINE. THE PILOT TURNED BACK AND LANDED SAFELY AT FWA WITHOUT INCIDENT. ONCE ON THE GROUND PILOT NOTICED RIGHT ENGINE OIL DIP STICK NOT SECURED. MAINTENANCE REPLACED DIP STICK, CLEANEJul 9, 2012 · N42HD · Piper PA31350 · Reciprocating Engine Oil SystemSDR BSYA2012025Engine · malfunctionedDURING FLIGHT TO ORL, PILOT NOTICED LEFT ENGINE SPUTTERED. PILOT PROCEEDED TO PULL POWER BACK AND LANDED SAFELY AT SAV WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND METAL IN OIL FILTER. MAINTENANCE IS IN PROCESS OF CHANGING LEFT ENGINE.Jul 4, 2012 · N106TG · Piper PA31350 · Engine (Turbine/Turboprop)SDR BSYA2012023Engine · shutdownWHILE PILOT QUICKLY ADVANCED LEFT ENGINE THROTTLE FOR INITIAL TAKEOFF ROLL AT PHX, LEFT ENGINE QUIT. PILOT TAXIED BACK TO RAMP WITHOUT INCIDENT. MAINTENANCE PERFORMED FULL POWER RUN UP AND OPERATIONAL CHECK, NO DEFECTS NOTED.Jun 29, 2012 · N35584 · Piper PA31350 · Engine (Turbine/Turboprop)SDR BSYA2012022Engine · malfunctionedWHILE EN ROUTE TO FWA, PILOT NOTICED THE RIGHT ENGINE RUNNING HOT ALONG WITH SOME VIBRATION. PILOT PROCEDED TO SHUT RIGHT ENGINE DOWN AS A PRECAUTIONARY MEASURE. PILOT NOTIFIED ATC AND LANDED SAFELY AT FWA WITHOUT INCIDENT.Jun 28, 2012 · N711LH · Piper PA31350 · Engine (Reciprocating)SDR CA120530010Piston · cracked(CAN) WHILE PERFORMING SB1233, MAINTENANCE FOUND THE RT MLG ACTUATOR PISTON THREADED END CRACKED APPROXIMATELY .2500" AND A PIECE OF THREADED ROD PORTION APPROXIMATELY .2500" X .2500" MISSING FROM END OF PISTON THREADED END. ACTUATOR REPLACED.May 29, 2012 · Piper PA31350 · Landing Gear ActuatorSDR CA120517007Cylinder Head · cracked(CAN) FOUND CYLINDER HEAD CRACK UNDER INTAKE PUSH ROD AREA. I DID CHECK WITH O/H SHOP. THEY SUPPORT THE THEORY OF "SHOT/QUICK COOLING". THE CYLINDER WAS AT THE POSITION NR 1, THE MOST EXPOSE TO COOL EXTERNAL AIR.May 16, 2012 · Piper PA31350 · Reciprocating Engine Cylinder SectionSDR CA120514007Cylinder · cracked(CAN) DURING ROUTINE INSPECTION A FUEL LEAK WAS NOTED ON THE NR 2 CYLINDER AROUND THE INTAKE PORT. UPON FURTHER INVESTIGATION, A CRACK WAS NOTED IN THE CYLINDER WALL JUST ABOVE THE INTAKE PORT. THE CRACK IS APPROXIMATELY 1" IN LENGTH. THE CYLINDER WAS REPLAMay 9, 2012 · Piper PA31350 · Reciprocating Engine Cylinder SectionSDR 2012FA0000233Line · leakingDURING CRUISE, PILOT SMELLED FUEL. AFTER LOOKING AROUND THE COCKPIT, PILOT NOTICED A SMALL FUEL STAIN ON THE COPILOT'S CARPET. THE ACFT IMMEDIATELY DEVERTED TO THE NEAREST AIRPORT. AFTER TROUBLESHOOTING, FOUND FUEL FLOW INDICATOR FLEXABLE FUEL HOSE PETRIFIApr 20, 2012 · N33MV · Piper PA31350 · Engine Fuel DistributionSDR CA120502016Crankcase · cracked(CAN) ON A ROUTINE INSPECTION, THE AME NOTICED AN 1.5" CRACK UNDER THE PROPELLER GOVERNOR EXTENDING DOWN TOWARD THE STARTER MOUNTING PLATE. DESPITE EXTENSIVE RESEARCH WE HAVE NOT BEEN ABLE TO COME UP WITH A ROOT CAUSE ON TO WHY THE CRACK HAPPENED IN SUCH AN UApr 9, 2012 · Piper PA31350 · Reciprocating Engine Power SectionSDR CA120224012Magneto · failed(CAN) MAGNETO FAILED.Feb 24, 2012 · Piper PA31350 · Magneto/DistributorSDR WVBA2012020312542Brace · crackedCRACKS IN AFT MAIN GEAR SIDE BRACE FITTING ASSEMBLY P/N 40294-00. WE INITIATED A DYE PENETRANT INSPECTION PROGRAM ON THE FORWARD AND AFT MAIN GEAR SIDE BRACE FITTING ASSEMBLIES OF OUR PIPER CHIEFTAIN NAVAJO FLEET. THE INITIAL INSPECTION OF OUR AIRCRAFT REVEAFeb 2, 2012 · N4082T · Piper PA31350 · Main Landing Gear Attach SectionSDR CA120119010Wheel · broken(CAN) DURING PREDEPARTURE GROUND RUN, CREW WAS ADVISED BY TOWER OF A SMALL FIRE NEAR NOSE WHEEL AREA.EMERGENCY EQUIPMENT RESPONDED AND WHEN CREW EVACUATED AIRCRAFT FIRE HAD EXTINGUISHED. MAINTENANCE FOUND COMBUSTION HEATER COMBUSTION AIR SWITCH CONTACTS CLOSEDJan 16, 2012 · Piper PA31350 · Heating SystemSDR CA120116012Pressure Switch · inoperative(CAN) TOWER CONTACTED FLIGHT CREW TO ADVISE CREW OF A SMALL FIRE NEAR THE NOSE LANDING GEAR AREA. FLIGHT CREW EVACUATED THE AIRCRAFT TO INVESTIGATE THE FIRE. AIRPORT EMERGENCY EQUIPMENT ARRIVED BUT FIRE HAD ALREADY EXTINGUISHED. ALL AREAS OF THE AIRCRAFT WERE Jan 13, 2012 · Piper PA31350 · Heating SystemSDR BSYA2011035Nozzle · dirtyAFTER DEPARTING PILOT HAD LEFT ENGINE RUNNING ROUGH, DIVERTED. MAINTENANCE CLEANED FUEL NOZZLES AND CHANGED ALL SPARK PLUGS, OPS CHECKED GOOD.Dec 2, 2011 · N40919 · Piper PA31350 · Fuel Injector NozzleSDR CA111205001Line · cracked(CAN) IT WAS NOTICED THAT THE LT OLEO WAS LEAKING FLUID AND LOOSING PRESSURE, AFTER DISMANTLE OF THE BRACKET THAT HOLDS THE BRAKE LINE, A 1.5" CRACK WAS NOTICED. THE PART WAS REPLACED AND ACFT RETURNED TO SERVICE.Nov 19, 2011 · Piper PA31350 · Landing Gear Brake SystemSDR CA111109004Exhaust Duct · unserviceable(CAN) DURING 100 HR INSP, FOUND CYLINDER NR 4 EXHAUST RISER BULGED AT COLLECTOR, BULGE IS CONSISTENT WITH DIRECTION OF CYLINDER NR 4 EXHAUST FLOW. UPON REMOVAL, NOTICED THE EXHAUST TO BE QUITE THIN AND APPEARED TO HAVE LOST MATERIAL. A GENTLE TAP WITH A SOFTNov 8, 2011 · Piper PA31350 · Engine Collector/Tailpipe/NozzleSDR BSYA2011033Fuel Nozzle · dirtyAFTER DEPARTING BDL HAD BOTH ENGINES SURGING, RETURNED TO BDL. MAINTENANCE CLEANED LEFT ENGINES FUEL NOZZLES AND ON THE RIGHT ENGINE REPLACED NR 1, 2, 3 & 5 FUEL NOZZLES, BOTH ENGINES OPS CHECKS GOOD.Sep 13, 2011 · N225TM · Piper PA31350 · Fuel Injector NozzleSDR CA110912001Wire · broken(CAN) PILOT PERFORMED NON-EVENT LANDING WITH NO INDICATION OF THE NOSE GEAR DOWN AND LOCKED. ON APPROACH, THE PILOT SELECTED GEAR DOWN, WITH ONLY TWO MAIN GEARS DOWN AND LOCK INDICATION (2 GREEN LIGHTS). THE NOSE GEAR DOWN AND LOCK GREEN LIGHT DID NOT ILLUMISep 4, 2011 · Piper PA31350 · Landing Gear System WiringSDR FVJA20110827002Oil System · leakingAFTER DEPARTURE, WHILE IN THE CLIMB, ACFT EXPERIENCED SMOKE COMING FROM THE RT ENGINE COWL LOUVER DOORS AND VISIBLY HAD OIL EXITING THE ENGINE COWL UPPER DOOR (OIL FILL ACCESS) AND THE INBD SIDE OF THE ENGINE COWLS. THE ENGINE WAS SECURED AND THE ACFT RETURNEAug 27, 2011 · N3LA · Piper PA31350 · Turbine Engine Oil SystemSDR 2011F00190Probe · malfunctionedCHT GAUGE IN COCKPIT PEGGED HIGH. ALL OTHER INDICATIONS NORMAL. ACFT RETURNED TO BASE. CHT PROBE FOUND TO HAVE AN OPEN CIRCUIT.Aug 23, 2011 · N46FA · Piper PA31350 · Cylinder Head Temperature (CHT) Indicating SystemSDR 2011FA0000526Lead · brokenLT ENGINE IGNITION HARNESS LEAD THAT ATTACHES TO THE SPARK PLUG IS A 90 DEGREE TUBING WITH BRAZED COUPLERS. THESE BRAZED COUPLERS ARE CRACKING AND BREAKING, REQUIRING THEIR UNSCHEDULED REPLACEMENT. 2 HAVE REQUIRED REPLACEMENT IN 283.5 HOURS TIME IN SERVICE.Aug 16, 2011 · N828KT · Piper PA31350 · Ignition Harness (Distribution)SDR CA110803032Pump · failedAFTER 3.7 HRS OF INSTALLING AN O/H HIGH ALTITUDE BOOST PUMP, IT FAILED ON ENGINE START UP. THE PUMP WAS REMOVED WITH NO FUTHER INCIDIENT.Jul 21, 2011 · Piper PA31350 · Fuel Boost PumpSDR CA110717001Pump · failedDURING LEVEL CRUISE FLIGHT IT WAS NOTED THAT THE "HIGH ALTITUDE FUEL BOOST PUMP RT" CIRCUIT BREAKER HAD POPPED. THE ACFT CONTINUED ITS FLIGHT BACK. MX CONFIRMED THE PUMP HAD FAILED INTERNALLY. A NEW PUMP WAS INSTALLED WITHOUT FURTHER INCIDENT.Jul 13, 2011 · Piper PA31350 · Fuel Boost PumpSDR 2011F00128Audio Panel · failedPILOT LOST VHF COMMUNICATIONS. PROCEEDED TO LAND WITHOUT INCIDENT. THE AUDIO PANEL WAS REMOVED AND FOUND TO BE DEFECTIVE , NO EXTERNAL VISIBLE DAMAGE WAS OBSERVED . THE AUDIO PANEL WAS SHIPPED TO MANUFACTURER FOR REPAIR OR EXCHANGE.Jun 1, 2011 · N27478 · Piper PA31350 · Audio Integrating SystemSDR N5C2011F00001Audio Panel · failedPILOT LOST VHF COMMUNICATIONS. AFTER FAILED ATTEMPTS TO CONTACT ATC THE PILOT THEN ENTERED "7600" INTO THE TRANSPONDER. THE ACFT PROCEEDED AND WAS GIVEN GREEN LIGHT TO LAND WITHOUT INCIDENT. THE AUDIO PANEL WAS REMOVED BY AVIONICS AND FOUND TO BE DEFECTIVE,May 28, 2011 · N27478 · Piper PA31350 · Audio Integrating SystemSDR FXTA20110411006Starter · brokenSTARTER BENDIX GEAR BROKE IN THREE PIECES ON DRIVE SHAFT.Apr 9, 2011 · N4118G · Piper PA31350 · Engine StarterSDR 2011FA0000231Gear · misinstalledPART WAS INSTALLED NEW FROM MFG. DISTRIBUTOR APPEARS TO HAVE BEEN ASSEMBLED WITH FINGER, NOT PROPERLY LOCATED. APPROX 15 DEGREES OUT OF ALIGNMENT. MINOR ENGINE ROUGHNESS OR SUBJECTIVE SIGN AND WAVE, WITHIN NORMAL PARAMETERS. DEFAULT DISCOVERED AT CURRENT IMar 29, 2011 · N88TG · Piper PA31350 · Magneto/DistributorSDR BSYA2011013Setscrew · missingAIRCRAFT EN ROUTE FROM DPA TO YIP FLYING AT 10,000FT WHEN THE LEFT ENGINE LOST MANIFOLD PRESSURE, PILOT SHUT DOWN ENGINE AND DECLARED AN EMERGENCY AND RETURNED TO DPA LANDED NO PROBLEMS. MAINTENANCE FOUND THAT THE PROPELLER GOVERNOR IDLER GEAR SHAFT SET SCREWMar 9, 2011 · N22427 · Piper PA31350 · Propeller GovernorSDR BSYA2011003Turbocharger · failedRT ENGINE TURBOCHARGER QUIT SHORTLY AFTER TAKEOFF. MANIFOLD PRESSURE DROPPED TO 38". ACFT THEN RETURNED TO DEPARTURE. MX R & R TURBOCHARGER, OPS CHECKS GOOD.Jan 10, 2011 · N4UE · Piper PA31350 · Exhaust TurbochargerSDR CA110111006Filter · rupturedLANDING GEAR WOULD NOT COME DOWN, HAD TO DO A EMERGENCY EXTENSION. IT WAS FOUND THAT THE RIGHT HYDRAULIC FILTER CANISTER HAD RUPTURED AT THE BASE OF THE THREADS CAUSING LOSS OF HYDRAULIC FLUID, A NEW HYDRAULIC FILTER HOUSING WAS INSTALLED AND THE ENTIRE HYDRAJan 8, 2011 · Piper PA31350 · Hydraulic Filter, Main
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