Lycoming IO-540-AB1A5

Service difficulty reports · 138

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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 = 'IO540AB1A5'
  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 CA141223006Ignition Switch · broken(CAN) IGNITION SWITCH COULD BE ROTATED COUNTER CLOCKWISE PAST THE "OFF" POSITION AND ENGAGE THE STARTER.Dec 8, 2014 · Cessna 182T · Engine Starting System WiringSDR 2014FA0000622Attach Fitting · brokenDURING ANNUAL INSPECTION, FOUND NOSE GEAR LOWER ATTACHMENT CAST FITTING TO AIRCRAFT FUSELAGE HAD TWO HORIZONTAL ATTACHMENT EARS CRACKED. AFTER REMOVING THE BOLT FROM EACH FITTING EAR, THE EARS CAME OFF, THE EARS APPEAR TO HAVE SNAPPED OFF FROMT THE CAST FITTIOct 2, 2014 · N314DR · Cessna 182S · Fuselage, Landing Gear Attach FittingsSDR CA140714017Doubler · failed(CAN) RIGHT MAIN LANDING GEAR WHEEL FAIRING OUTBOARD DOUBLER FAILED AT THE ATTACH BOLT HOLE. THIS ALLOWED THE FAIRING TO CONTACT THE TIRE WHICH ON LANDING CAUSED THE FAIRING TO BE DRAWN UP UNDER THE TIRE AND DESTROYED.Jul 9, 2014 · Cessna 182T · Main Landing GearSDR 2014FA0000417Setscrew · leakingINSTALLED O/H FUEL SERVO AND RAN IT TO SET THE IDLE MIXTURE SETTING. ACFT SAT OVER THE WEEKEND AND WENT TO COWL THE ENGINE AND NOTICED A SET SCREW AT THE FRONT OF THE SERVO WAS LEAKING FUEL. SCREW IS NOT USED TO ADJUST IDLE MIXTURE AND WAS LOCK WIRED AT THE OJul 8, 2014 · N158FC · Cessna 182T · Fuel Control/Turbine EnginesSDR 2014FA0000405Servo · failedENGINE HAS BEEN RUNNING ROUGH AND VERY RICH AT IDLE. IDLE MIXTURE WAS ADJUSTED DUE TO A RISE OF OVER 100 RPM WHEN CHECKING. ACFT FLEW FOR A FEW MORE HOURS, BUT MIXTURE WAS RICH AGAIN. ALSO WHEN ACFT WAS PARKED OVERNIGHT, FUEL STAIN WAS ON THE GROUND UNDERNEATJun 27, 2014 · N158FC · Cessna 182T · Aircraft Fuel Distribution SystemSDR 2014FA0000396Snap Ring · corrodedPROPELLER WAS OVERHAULED 5 MONTHS, 96 HOURS AGO, AND IS IN FOR INSPECTION. SNAP RING AROUND BASE OF A BLADE AND THE GROOVE IN THE BLADE HAS CORROSION. PROPELLER WAS REMOVED AND BEING SENT BACK FOR REPAIR. NO CORROSION PREVENTATIVE WAS OBSERVED ON THE SNAP Jun 23, 2014 · N158FC · Cessna 182T · Propeller Blade SectionSDR 2013FA0000722Guide · out of toleranceDURING THE PERFORMANCE OF SB 388C, THE EXHAUST VALVE GUIDE CLEARANCE ON NR 4 CYLINDER WAS FOUND TO BE .030". THIS IS THE MAXIMUM CLEARANCE ALLOWED.Dec 12, 2013 · N514H · Cessna 182T · Reciprocating Engine Cylinder SectionSDR JRUR201312050013Exhaust Valve · out of toleranceDURING PERFORMANCE OF SB 388C, FOUND NR 2 CYLINDER EXHAUST VALVE TO GUIDE CLEARANCE MEASURED .032". EXCEEDS THE MAXIMUM ALLOWABLE CLEARANCE OF .030". NR 2 CYLINDER OVERHAULED 502.1 HOURS AGO. MAINTENANCE INSTALLED A NEW, EXHAUST VALVE GUIDE DURING OVERHAULDec 5, 2013 · N715HP · Cessna 182S · Reciprocating Engine Cylinder SectionSDR CA131129002Adapter · clogged(CAN) RESTRICTOR ORIFICE IN MANIFOLD PRESSURE INDICATOR LINE ADAPTOR AT CYLINDER NR 3 FOUND PLUGGED. ORIFICE CLEANED.Nov 27, 2013 · Cessna 182T · Manifold Pressure (MP) IndicatingSDR 2013FA0000693Pump · leakingUPON FIRST START SINCE ENGINE OVERHAUL, FUEL BEGAN LEAKING FROM THE FUEL PUMP OVERBOARD DRAIN. FUEL PUMP WAS A NEW, PN AF-15473. REPLACED THAT FUEL PUMP WITH ANOTHER NEW FUEL PUMP, PN AF-15473. THIS SECOND NEW FUEL PUMP BEGAN LEAKING AFTER APPROXIMATELY 8 HNov 26, 2013 · N354CP · Cessna 182T · Engine Fuel PumpSDR 2013FA0000445Selector Switch · failedACFT HAD PREVIOUS FORCED LANDING RESULTING IN PROP STRIKE CAUSED BY FUEL STARVATION. HAVE BEEN TROUBLESHOOTING A FUEL FEEDING ISSUE SINCE THE ACFT ARRIVED. THE ACFT FEEDS RANDOMLY FROM EITHER TANK WHEN BOTH SELECTED. DURING TROUBLESHOOTING AT ANNUAL, DISCOVAug 9, 2013 · N984PD · Cessna 182S · Fuel Selector/Shut-Off ValveSDR 2013FA0000570Guard · missingFACTORY ELECTRICAL WIRING ON PILOT SIDE PANEL, FWD OF INSTRUMENT PANEL, BETWEEN FUSELAGE STATIONS FS 0.00 AND FS 17.0. THE LT AILERON CABLE IS RUBBING AGAINST VERTICAL WIRE HARNESS. THE WIRE HARNESS IS TIED OFF ABOVE AND BELOW THE AILERON CABLE. THE GUARD Aug 7, 2013 · N718CP · Cessna 182T · Aileron Control SystemSDR CA130729016Indication Sys · malfunctioned(CAN) TRIM INDICATOR PIN CAN BE DISLODGED FROM ITS FULL RT POSITION BY OVERTURNING TRIM WHEEL. RESULTANT INDICATION ERROR WHEN RETURNED TO NEUTRAL, EVIDENT BY POSITION OF RUDDER PEDALS AND CONTROL SURFACE.Jul 26, 2013 · Cessna 182S · Rudder Tab Control SystemSDR JRUR201308090012Exhaust Valve · out of toleranceDURING PERFORMANCE OF SB 388C, FOUND NR 4 CYLINDER EXHAUST VALVE TO GUIDE CLEARANCE MEASURED .031". EXCEEDS MAXIMUM ALLOWABLE CLEARANCE OF .030". NR 4 CYLINDER WAS REPAIRED.Jun 13, 2013 · N18HP · Cessna 182T · Reciprocating Engine Cylinder SectionSDR JRUR201303060011Exhaust Valve · out of toleranceWHILE PERFORMING SB 388C, NR 6 CYLINDER EXHAUST VALVE TO GUIDE CLEARANCE WAS FOUND TO BE .010". BELOW ACCEPTABLE MINIMUM TOLERANCE OF .015". HAD 201 HOURS TIS SINCE SB 388C HAD PREVIOUSLY BEEN PERFORMED. VALVE DRIVEN OUT TO REMOVE IT FOR REAMING OF THE GUIMar 6, 2013 · N17HP · Cessna 182T · Reciprocating Engine Cylinder SectionSDR JRUR201303060010Exhaust Valve · out of toleranceNR 3 EXHAUST VALVE TO GUIDE CLEARANCE WAS FOUND TO BE .012". BELOW ACCEPTABLE MINIMUM TOLERANCE OF .015". 201 HOURS TIS SINCE SB 388C HAD PREVIOUSLY BEEN PERFORMED. VALVE CLEARANCE MEASUREMENT HAD BEEN .020". VALVE HAD TO BE DRIVEN OUT TO REMOVE IT FOR REMar 5, 2013 · N17HP · Cessna 182T · Reciprocating Engine Cylinder SectionSDR 2013FA0000071Engine · fodSHIPPING PLUG WAS REMOVED PRIOR TO INSTALLATION OF PROPELLER ON A ZERO TIME FACTORY REBUILT ENGINE. INSIDE OF THE CRANKSHAFT BORE, A SLIVER OF METAL WAS FOUND. ENGINE INSTALLATION WAS STOPPED. ENGINE MFG WAS CONTACTED FOR FURTHER EVALUATION AND RECOMMENDATIJan 18, 2013 · N25HP · Cessna 182T · Engine (Reciprocating)SDR JRUR201208140006Exhaust Valve · stuckDURING START, PILOT NOTICED THE ENGINE RAN VERY ROUGH. SHUTDOWN ENGINE AND RESTARTED IT. ENGINE RUNNING SMOOTHER, BUT A VIBRATION WAS NOTED. ENGINE SHUTDOWN AND MECHANIC INVESTIGATED. A COMPRESSION CHECK WAS TAKEN AND NR 3 CYLINDER COMPRESSION WAS 0/80 WITHAug 14, 2012 · N18HP · Cessna 182T · Reciprocating Engine Cylinder SectionSDR 2012FA0000450Magneto · out of toleranceMAGNETO FOUND TO BE OUT OF TIME AT RUN UP. MAGNETO WAS REPLACED.Jul 2, 2012 · N832CP · Cessna 182T · Magneto/DistributorSDR 2012FA0000438Antenna · separatedHAD SEVERAL (FOUR PLUS) FAILURES OF THE WHIP ELT ANTENNA FOR THE ELT. THESE ANTENNA'S WERE INSTALLED BY STC, BY MANUFACTURER. ONE FAILURE SEPARATED AND BECAME LODGED BETWEEN THE LT HORIZONTAL STABILIZER AND ELEVATOR. NO CONTROL ISSUES WERE NOTED.Jun 27, 2012 · N305RC · Cessna 182T · Emergency Locator BeaconSDR 2012FA0000449Magneto · failedMAGNETO COIL FAILED AND POINTS LOOSE.Jun 2, 2012 · N832CP · Cessna 182T · Magneto/DistributorSDR JRUR201205160004Exhaust Valve · stuckENGINE MISSING & VIBRATION ON TAKEOFF. PILOT STATED THAT THE VIBRATION WAS SEVERE AND THOUGHT THE ENGINE WAS GOING TO QUIT. PILOT MADE A 180 DEGREE TURN AND LANDED. UPON INSPECTION, THE NR 2 CYLINDER FAILED A COMPRESSION CHECK. COMPRESSION WAS MEASURED AT 5/May 7, 2012 · N6HP · Cessna 182T · Reciprocating Engine Cylinder SectionSDR JRUR201205160005Exhaust Valve · leakingENGINE MISSING & VIBRATION ON TAKEOFF. PILOT STATED THAT THE VIBRATION WAS SEVERE AND THOUGHT THE ENGINE WAS GOING TO QUIT. LANDED. ON INSPECTION, NR 4 CYLINDER COMPRESSION WAS MEASURED AT 78/80. PERFORMED SB 388C. VALVE TO GUIDE CLEARANCE WAS MEASURED AT .0May 7, 2012 · N6HP · Cessna 182T · Reciprocating Engine Cylinder SectionSDR JRUR201205150001Exhaust Valve · leakingPROPELLER AND ENGINE PULSE CAVITATION IN FLIGHT. SIGNIFICANT OIL LEAK ON GROUND. HAD 19 INCHES MANIFOLD PRESSURE, 2100 RPM WHEN SLOWLY ADVANCING THE RPM. ACFT GROUNDED. MECHANIC PERFORMED A COMPRESSION CHECK ON ENGINE AND FOUND THE NR 6 CYLINDER HAD A COMPMar 6, 2012 · N716HP · Cessna 182T · Reciprocating Engine Cylinder SectionSDR JRUR201205150002Exhaust Valve · leakingPROPELLER AND ENGINE PULSE CAVITATION IN FLIGHT. SIGNIFICANT OIL LEAK ON GROUND. HAD 19 INCHES MANIFOLD PRESSURE, 2100 RPM WHEN SLOWLY ADVANCING RPM. ACFT GROUNDED. MECHANIC PERFORMED A COMPRESSION CHECK ON ENGINE AND FOUND NR 4 CYLINDER HAD AN ACCEPTABLE COMar 6, 2012 · N716HP · Cessna 182T · Reciprocating Engine Cylinder SectionSDR JRUR20120515003Exhaust Valve · leakingPROPELLER AND ENGINE PULSE CAVITATION IN FLIGHT. SIGNIFICANT OIL LEAK ON GROUND. HAD 19 INCHES MANIFOLD PRESSURE, 2100 RPM WHEN SLOWLY ADVANCING RPM. AIRCRAFT GROUNDED. MECHANIC PERFORMED A COMPRESSION CHECK ON THE ENGINE AND FOUND THE NR 2 CYLINDER HAD AN ACMar 6, 2012 · N716HP · Cessna 182T · Reciprocating Engine Cylinder SectionSDR CA120306009Exhaust Valve · seized(CAN) AFTER LEVELING OFF AT 4000` ENGINE WAS RUNNING FINE FOR ABOUT A MINUTE. SUDDENLY THERE WAS A SMALL VIBRATION THAT LASTED ABOUT 30 SECONDS THEN IT TURNED INTO A LARGE VIBRATION THAT GOT WORSE. PILOT REQUESTED IMMEDIATE LANDING AND REDUCED POWER WHICH CAMar 5, 2012 · Cessna 182S · Reciprocating Engine Cylinder SectionSDR CA120316006Bulkhead · dented(CAN) 3 DENTS, GOING FORWARD ON LOWER PORTION OF FS 209.0 BULKHEAD. ESTIMATED DENT DEPTH APPROXIMATE 0.185". APPEARS TO HAVE BEEN THIS WAY DURING MFG AS THERE ARE BUCKING BAR MARKS ON FORWARD FACE OF THE BULKHEAD WHICH ARE CONSISTENT WITH SURROUNDING STRUCTUROct 13, 2011 · Cessna 182T · Fuselage Main, BulkheadSDR 2011FA0000669Connecting Rod · failedINSTALLED CRANKSHAFT KIT 05K23580 TO C/W AD 06-02-09 CRANKSHAFT RETIREMENT. KIT INCLUDES NEW CRANK, NEW BEARINGS, ROD BOLTS AND NUTS. NEW PISTON RINGS, SEAL AND GASKET SET. ENGINE TEST RAN AND TEST FLOWN. ENGINE RAN FOR APPROX 40 HRS OF TROUBLE FREE OPERATAug 28, 2011 · N23735 · Cessna 182S · Reciprocating Engine Power SectionSDR 2011FA0000447Resistor · burned outDURING CRUSE, HAD A RESISTOR AND A ZENER DIODE (WHICH IS PART OF THE RADIO DIMMER SWITCHING CIRCUIT) FAILED IN FLIGHT. THIS FAILURE CAUSED A LARGE AMOUNT OF SMOKE IN THE CABIN THE PILOT LANDED THE ACFT AT THE AIRPORT. THIS SWITCH IS PART OF STC SA01216WI. THJun 18, 2011 · N482CA · Cessna 182T · Flight Compartment LightingSDR 2011FA0000219Points · corrodedAT THE LAST ANNUAL INSP, FOUND THE RT MAG POINTS PITTED AND REPLACED WITH A NEW SET OF M-3081 POINTS. CUSTOMER CALLED AS WAS HAVEING PROBLEMS WITH THE RT MAG, DEAD, NO SPARK. UPON INVESTIGATION, THE PROBLEM WAS THE POINTS TAB WAS BROKEN AND LAYING IN THE CASMar 22, 2011 · N6182U · Cessna 182T · Magneto/DistributorSDR 2011FA0000140Distributor Blk · burnedREMOVED LEFT MAGNETO FOR 500 HOUR INSPECTION AND FOUND DISTRIBUTOR BLOCK ASSEMBLY BURNED THROUGH AND PIECES FLOATING AROUND INSIDE MAGNETO. LARGE AMOUNT OF DUST COATED SURFACES AND BURNING EVIDENT ON COIL AND ROTOR HOUSING. CARBON BRUSH AND CAM ARE EXTREMELYMar 1, 2011 · N352CP · Cessna 182T · Magneto/DistributorSDR JRUR2011030119HPGasket · leakingRED DYE LEAKING FROM TWO SCREWS THAT ATTACH THE PROPELLER BALANCE RING TO THE HUB. THE PROPELLER HAS 640.1 HOURS SINCE OVERHAUL. THE PROPELLER HAS THE (OLD) STYLE HUB GASKET THAT REQUIRES A BLACK PERMATEX SEALANT TO BE USED.Feb 25, 2011 · N19HP · Cessna 182T · Propeller Hub SectionSDR JRUR2010122019HPDoubler · cracked(JRUR) A 1.5 INCH LONG CRACK WAS DISCOVERED IN THE FIREWALL FWD DOUBLER (PN 0753600-24). THE CRACK WAS LOCATED ON THE LOWER LT QUADRANT OF THE FWD FIREWALL DOUBLER. THE CRACKED LOCATION CAN BE FOUND BY LOCATING THE "BRACKET-PARKING BRAKE CONTROL" AFT OF THE Dec 20, 2010 · N19HP · Cessna 182T · Nacelle/Pylon, Bulkhead/FirewallSDR JRUR2010121518HPDoubler · crackedA CRACK WAS DISCOVERED IN THE FIREWALL FORWARD DOUBLER. THE CRACK IS LOCATED BEHIND THE "COWL EXIT RAMP- RIGHT HAND" (P/N 0752732-2 SEE MANUFACTURE IPC REV 19 53-10-00 ITEM 241). THE LONGEST SECTION OF CRACK IS 6 INCHES LONG. THERE IS ALSO A SECONDARY CRACK (3Dec 15, 2010 · N18HP · Cessna 182T · Nacelle/Pylon, Bulkhead/FirewallSDR JRUR20101215910HPDoubler · cracked(JRUR) A CRACK WAS DISCOVERED IN THE FIREWALL FWD DOUBLER (PN 0753600-24). THE CRACK WAS LOCATED BEHIND THE COWL EXIT RAMP- RT (PN 0752732-2). THE CRACK WAS 2-3 INCHES LONG. THIS AREA IS VERY DIFFICULT TO INSPECT ON A P1 (50 HR) WITH THE LOWER COWLING INSTALLOct 4, 2010 · N910HP · Cessna 182T · Nacelle/Pylon, Bulkhead/FirewallSDR CA100809026Exhaust Valve · stuckACFT DEPARTED FOR LOCAL FLIGHT OVER CITY, ON TAKEOFF EVERYTHING NORMAL, IN CLIMB ENGINE STARTED TO RUN ROUGH. PILOT LEVELED OUT AT 1000 FT AND RETURNED TO AIRPORT. LANDED WITH OUT ANY PROBLEMS. ACFT WAS RUN UP NEXT MORNING STILL RUNNING ROUGH AND MIXTURE WAS Aug 6, 2010 · Cessna 182S · Reciprocating Engine Cylinder SectionSDR 2010FA0000512Brushes · wornUPON DISASSEMBLY OF THE LT MAGNETO FOR RECOMMENDED SLICK 500 HR. MAGNETO INSP, FOUND THE DISTRIBUTOR BRUSH BADLY WORN AND ABOUT TO BREAK OFF. WEAR IS EXACTLY AS DESCRIBED IN SB3-08A FIG 1, ALTHOUGH MUCH MORE EXTREME. THIS MAGNETO SN AND MFG DATE ARE WELL OUTSMay 27, 2010 · N182VM · Cessna 182T · Magneto/DistributorSDR 2010FA0000513Brushes · wornUPON DISASSEMBLY OF THE RT MAGNETO FOR RECOMMENDED 500 HR. MAGNETO INSPECTION, FOUND THE DISTRIBUTOR BRUSH BADLY WORN. WEAR IS EXACTLY AS DESCRIBED IN SB3-08A FIG 1, ALTHOUGH MORE EXTREME. THIS MAGNETO SN AND MFG DATE ARE WELL OUTSIDE OF THE AFFECTED APPLICABIMay 27, 2010 · N182VM · Cessna 182T · Magneto/DistributorSDR 2009FA0001016Valve · stuckON START UP AND TAXI OUT OF THE ACFT, THE EXHAUST AND INTAKE VALVES STUCK. THIS CAUSED BOTH PUSH RODS TO BEND. AND THE LIFTER PLUNGER WAS LOCKED UP UPON FURTHER INSP. THE ENG WAS USING W100 OIL AND HAD ONLY 634.8 HOURS SINCE NEW.Oct 29, 2009 · N46PD · Cessna 182S · Reciprocating Engine Cylinder SectionSDR 2009FA0000514Exhaust Valve · stuckDURING COMPLIANCE OF SB 388C, 3 EXHAUST VALVE GUIDES FAILED TO HAVE SERVICEABLE MEASUREMENTS. NR 4 CYL EXHAUST VALVE STUCK FULLY CLOSED. VALVE MOVEABLE WITH MINIMAL PRESSURE, NO DAMAGE TO OTHER COMPONENTS. NR 6 CYL EXHAUST VALVE GUIDE CLEARANCE MEASURED .03Jun 12, 2009 · N716HP · Cessna 182T · Reciprocating Engine Cylinder SectionSDR 2009FA0000513Exhaust Valve · stuckNR 6 CYLINDER EXHAUST VALVE STUCK DURING TAKEOFF CLIMB. PILOT NOTED A SEVERE VIBRATION WHEN POWER WAS REDUCED AS HE LEVELED OFF. PILOT IMMEDIATELY RETURNED TO THE AIRPORT AND LANDED. VISUAL INSP REVEALED THAT THE NR 6 CYL EXHAUST VALVE HAD STUCK. PUSH ROD AND Jun 2, 2009 · N18HP · Cessna 182T · Reciprocating Engine Cylinder SectionSDR CA090218002Wire · damaged(CAN) DURING MASTER SWITCH SELECTION TO ON, NO POWER WAS OBSERVED ANYWHERE IN ACFT. TROUBLESHOT A FEW TIMES, EVERY TIME, WHEN MX TRIED TO DUPLICATE SNAG, UNABLE TO FAULT. FINALLY, WAS ABLE TO FAULT, FOUND THAT BUSS (BUS) TIE STRAP FROM ALTERNATOR CONTACTOR (SNov 11, 2008 · Cessna 182S · Electrical Power System WiringSDR 2008FA0000688Pump · crackedPUMP HOUSING CRACKED ALONG SEAM. POSSIBLE WEAK SPOT UPON MANUFACTURING. (K)Oct 1, 2008 · N66419 · Cessna 182S · Engine Fuel PumpSDR 2008FA0000735Gear · damagedWHILE PERFORMING SB03-08, FOUND THE DISTRIBUTOR GEAR DRIVE GEAR WEARING PREMATURELY AND CAUSING GEAR DUST INSIDE MAGNETO. GEAR MATERIAL WAS COMING OFF CAUSING IT TO COLLECT INSIDE DISTRIBUTOR CAP. ALSO, FOUND EXCESSIVE AMOUNT OF OIL INSIDE MAGNETO. REPLACED MASep 25, 2008 · N658PW · Cessna 182T · Magneto/DistributorSDR 2008FA0000404Distributor Blk · misrepairedDURING INTERNAL MAGNETO INSPECTION, FOUND DISTRIBUTOR BLOCK SPOT FACED AREA FOR POLES. APPEARS TO BE INCORRECTLY SPOT FACED. MATERIAL THAT WAS LEFT BEHIND HAS THE SAME LOFT AS BEARING BOSS AREA ON DISTRIBUTOR BLOCK. THIS CAUSES THE FINGER ON THE DISTRIBUTORJun 17, 2008 · N658PW · Cessna 182T · Magneto/DistributorSDR 2008FA0000270Attach Fitting · crackedDISCOVERED CRACK DURING ANNUAL INSPECTION. (2) LONG CRACKS APPROXIMATELY (1) INCH ON (1) SIDE OF THE FITTING ONLY, (1) AT THE LT LOWER ATTACHMENT AND THE OTHER JUST AFT AND LT OF THE AREA WHERE THE STRUT BARREL IS SECURED. SUSPECT HARD LANDING BUT NO OTHER Apr 3, 2008 · N783WB · Cessna 182T · Nose/Tail Landing Gear Strut/AxleSDR CA080320007Gasket · looseAD2008-06-51 FUEL INJECTION SERVO PLUGS, SERVO PLUGS FOUND LOOSE UPON INSPECTION. SERVO PLUG SEALS REPLACED WITH NEW AS PER THE CONVERSATION WITH PRECISION AIRMOTIVE REPRESENTATIVE. ENGINE REMANUFACTURE DATE OF SEPT 8, 2004 DOES NOT FALL WITHIN THE DATES SPEMar 14, 2008 · Cessna 182T · Fuel Control/Turbine EnginesSDR 2007FA0000963Fitting · chafedLOWER STRUT SUPPORT FITTING CLAMPING RING CENTER BORE IS NOT CENTERED. THIS CAUSES THE STEERING COLLAR AND LOWER STRUT SUPPORT TO CHAFE AND FOR METAL TO METAL CONTACT TO OCCUR. HAVE TRIED TWO OTHER NEW LOWER STRUT SUPPORT FITTING RESULTING WITH METAL TO METAOct 18, 2007 · N6025D · Cessna 182T · Nose/Tail Landing Gear Strut/AxleSDR 2007FA0000900Control Cable · wornCONTROL CABLE, (P/N 0510105-189), FOUND WORN TO REPLACE LIMITS IAW AC43.13-1A, CABLE INSPECTION. CABLE WAS WORN DUE TO CONSTANT CONTACT WITH MICARDA GUARD PLATE OVER FUEL LINES AT FUEL SELECTOR AREA JUST FORWARD OF FRONT SEATS. THE CABLES ARE IN CONSTANT CONOct 12, 2007 · N7262Y · Cessna 182S · Elevator Control System
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