Continental O-470R

Service difficulty reports · 255

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 = 'O470R'
  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 2022FA0000499Oil Filter · looseAIRCRAFT IS EQUIPPED WITH AN AIRWOLF REMOTE OIL FILTER ADAPTER MOUNTED ON THE FIREWALL. A TEMPEST EZ TURN OIL FILTER PART # AA48109-1 WAS INSTALLED AT THE LAST OIL CHANGE AND INSTALLED WITHOUT THE USE OF DOW CORNING DC4 LUBRICANT ON THE SEAL AS DIRECTED BY THESep 10, 2022 · N71033 · Cessna 182M · Oil ServicingSDR 2022FA0000518Seat Track · deformedCONDUCT OF AD 2011-10-9, THE AD STATES:"INSPECT THE DIAMETER OF EACH SEAT LOCKING PIN ENGAGEMENT HOLE.. .THE MOST USED HOLES DO NOT HAVE A "DIAMETER", BUT INSTEAD HAVE A HOLE THAT IS ELLIPTICAL IN SHAPE. THUS, MEASUREMENTS FORE AND AFT AND PORT TO STARBOARD MUMay 20, 2022 · N79074 · Cessna 182P · Fuselage, Seat/Cargo Attach FittingsSDR 2022FA0000027Screw · missingTHROTTLE CABLE PORT THROUGH FIRE WALL OUTER SLEEVE LOST LOWER SCREW ALLOWING SHIELD FIREWALL GROMMET ATTACHMENT PART (S-352) HOUSING OF SEAL TO WEAR INTO THE CABLE ALMOST 1/2 WAY INTO INTERIOR CABLE, CAUSING INTERIOR CABLE TO BEGIN TO BIND. REPLACED CABLE WITJan 16, 2022 · Cessna 182L · Power LeverSDR 2021FA0000418Selector Valve · bypassingTHE FUEL SELECTOR VALVE WOULD NOT STOP THE FLOW OF FUEL IN ANY OF THE FOUR DETENTS (OFF-LEFT-BOTH-RIGHT) AT THE FIREWALL FUEL GASCOLATOR DURING AN ANNUAL INSPECTION. THE AIRPLANE HAD SAT IDLE FOR APPROXIMATELY 8 YEARS WITH THE FUEL TANKS FULL. AS I WAS ABOUTDec 21, 2021 · N3513U · Cessna 182F · Fuel Selector/Shut-Off ValveSDR 2021FA0000153Seal · unsecureAIRCRAFT WAS IN CRUISE FLIGHT AND SUDDENLY LOST ENGINE POWER WITH NO PRIOR WARNING. AIRCRAFT PERFORMED EMERGENCY LANDING TO AIRSTRIP WITH NO DAMAGE. UPON INSPECTION IT WAS DETERMINED THAT THE SEAL THAT SURROUNDS THE CONNECTION BETWEEN THE AIR INTAKE AND THE CAApr 25, 2021 · N831PZ · Cessna 182P · Engine Air Intake SystemSDR 2020FA0000520Pump · damagedTHE AIRCRAFT HAD A OIL LEAK. WE FOUND THE THREADS IN THE OIL PUMP HOUSING WERE GAULDED AND THE OIL FILTER ADAPTER THREADS WERE DAMAGED. MOST LIKELY FROM OVER TORQUE. THE PUMP BODY P/N 632563 WAS REPLACED AND AIR WOLF REMOTE OIL FILTER KIT INSTALLED.Dec 4, 2020 · N9266G · Cessna 182N · Reciprocating Engine Oil SystemSDR 2020FA0000500Oil Filter · looseAFTER A FLIGHT FROM CENTRAL ARKANSAS TO SOUTHERN MISSOURI WITH OVERNIGHT STAY, WHILE CONDUCTING A POST FLIGHT INSPECTION THE PILOT REPORTED EXCESSIVE OIL ON THE AIRCRAFT BELLY AND ENGINE COWLING. WHEN QUESTIONED, THE PILOT REPORTED THAT A POST FLIGHT INSPECTNov 14, 2020 · N42064 · Cessna 182L · Reciprocating Engine Oil SystemSDR 2020FA0000499Oil Filter · looseDURING SCHEDULED OIL CHANGE ON A CONTINENTAL O-470-R RECIPRICATING ENGINE THE MECHANIC NOTED THE TEMPEST OIL FILTER, PART NUMBER AA48110-2, HOUSING APPEARED TO SEPERATING FROM THE BASE AS INDICATED BY A LINE OF UNPAINTED METAL AT THE JUNCTURE OF THE BASE AND HNov 13, 2020 · N42064 · Cessna 182L · Reciprocating Engine Oil SystemSDR 2020FA0000415Fitting · fracturedDURING INSPECTION FOUND FITTING SEPARATED ON RIGHT SIDE AND SEPARATION GAP OPEN APPROXIMATELY .75". NO DAMAGE TO FIREWALL FOUND. NO DAMAGE TO CENTER TUNNEL FOUND. NO LOOSE HARDWARE WAS FOUND. METAL IN SEPARATION SHOWS CRACK WAS APPROXIMATELY 1/2 THROUGH MESep 20, 2020 · N8217G · Cessna 182P · Nose/Tail Landing GearSDR 2020FA0000035Rocker Boss · brokenTHE INFORMATION HAS BEEN FOUND AFTER REMOVAL AND INSPECTION OF CYLINDER NR 1 ROCKER COVER. AFTER RECEIVING A CALL THAT AN AIRCRAFT HAD LANDED WITH ENGINE PROBLEMS OVER THE WEEKEND, I STARTED INSPECTION OF ENGINE. I HAD FOUND THAT THE EXHAUST ROCKER BOSS HAD Sep 18, 2019 · N2883R · Cessna 182K · Reciprocating Engine Cylinder SectionSDR 2018FA0000464Fuel Cap · leakingIN 2015 THE FUEL CAP STCSA2376CE WAS INSTALLED TO PERMANENTLY TERMINATE AD841001R1. THESE FUEL CAPS HAVE BEEN NOTHING BUT PROBLEMS EVER SINCE INSTALLATION. THEY RANDOMLY LEAK LARGE QUANTITIES OF FUEL WITH NO WARNING. IN ONE TRIP AROUND THE PATTERN IT LEAKEDJul 9, 2018 · N2648Q · Cessna 182K · Fuel StorageSDR 2018FA0000118Camshaft · making metalTHE ENGINE APPEARS TO HAVE FAULTY SET OF LIFTERS CAUSING SEVERE DAMAGE TO THE CAMS. PURCHASED WITH 20 HRS ENGINE TIME. CAMS AND LIFTERS WERE INSPECTED ON PRE-BUY AND FOUND TO BE VISUALLY NORMAL WITH BLUEING STILL PRESENT. PERSISTENT HIGH FE ON REGULAR OIL AMar 23, 2018 · N67WW · Cessna 180H · Reciprocating Engine Power SectionSDR 2017FA0000201Solenoid · defectiveTHE SOLENOID WORKED WHEN FIRST INSTALLED. AFTER ONE OR TWO FLIGHTS IT BECAME INTERMITTENT, IT WOULD TAKE MORE THAN ONE FLIP OF THE MASTER SWITCH TO OBTAIN POWER TO THE PANEL AND STARTER. AFTER ANOTHER FLIGHT IT WOULD NOT CLOSE. TESTED THE DEVICE WHILE INSTALLMay 22, 2017 · Cessna 182K · Electrical Power SystemSDR CA150924007Gasket · leaking(CAN) PILOT REPORTED DEFECT, OIL STREAK FOUND DOWN SIDE OF COWL ON PILOT`S SIDE. OIL LEVEL FOUND TO BE DOWN 1 QT FROM BEGINNING OF THE FLIGHT. SUSPECT OIL LEAK. REMOVED COWLS AND INSPECTED FOR OIL LEAKS. FOUND NR 6 CYLINDER ROCKER BOX COVER LEAKING. REMOVEDSep 21, 2015 · Cessna 182E · Reciprocating Engine Oil SystemSDR 3PSR201503200003Link · brokenDURING INSPECTION, IT WAS NOTED THAT THE NR 3 BLADE ROTATED WITHIN THE HUB. DISCOVERED THAT THE BLADE ACTUATING LINK, WAS BROKEN WHICH ALLOWED THE BLADE TO ROTATE. IT WAS UNDETERMINED IF THE LINK WAS BROKEN DUE TO MISHANDLING OF THE PROPELLER OR HAPPENED DURMar 20, 2015 · Cessna 182H · Propeller AssemblySDR KC2R1218201449609Impulse Coupling · crackedDURING A ROUTINE 500 HR INSPECTION OF THE MAGNETOS, FOUND BOTH IMPULSE COUPLINGS CRACKED AT HUB PLATE, NEAR FULL ADVANCE STOP NOTCH.Dec 18, 2014 · N8937G · Cessna 182N · Magneto/DistributorSDR KC2R2014091049320Impulse Coupling · crackedDURING A 500 HOUR INSPECTION OF MAGNETOS, IMPULSE COUPLING WAS FOUND TO HAVE CRACKS IN THE HUB BASE PLATE, LOCATED AT THE FULL ADVANCE STOP NOTCH. CRACKS RADIATE FROM THE SHARP-CORNERED FEATURE OF THE NOTCH OF THE PLATE. DEFECT DETECTED USING MAGNETIC PARTICSep 10, 2014 · N2019X · Cessna 182H · Magneto/DistributorSDR KC2R20140812001Impulse Coupling · crackedDURING ROUTINE 500 HOUR INSPECTION OF MAGNETO, THE IMPULSE COUPLING WAS FOUND TO BE CRACKED. CRACKS ORIGINATE FROM SHARP CORNERED FEATURE OF IMPULSE COUPLING FLYWEIGHT BASE PLATE. THIS CORNER FORMS THE FULL ADVANCE STOP OF THE IMPULSE COUPLING. CRACK DISCOVAug 12, 2014 · N3138R · Cessna 182L · Magneto/DistributorSDR KC2R20140812002Impulse Coupling · crackedDURING ROUTINE 500 HOUR INSPECTION OF MAGNETO, THE IMPULSE COUPLING WAS FOUND TO BE CRACKED. CRACKS ORIGINATE FROM SHARP CORNERED FEATURE OF IMPULSE COUPLING FLYWEIGHT BASE PLATE. THIS CORNER FORMS THE FULL ADVANCE STOP OF THE IMPULSE COUPLING. CRACK DISCOVEREAug 12, 2014 · N3138R · Cessna 182L · Magneto/DistributorSDR NI6R201496120013Piston · out of toleranceDISCOVERED DURING INSTALLATION OF NEW PISTONS AND RINGS INTO NEW CYLINDER ASSY. FIRST AND SECOND PISTON RINGS DID NOT MEET NEW PARTS TOLERANCES IAW TABLE OF LIMITS CHART 2 IN CONTINENTAL MOTORS O/H MANUAL 72-30-14. ORDERED SECOND SET OF RINGS AFTER CONVERSATJun 12, 2014 · N2774Q · Cessna 182K · Reciprocating Engine Power SectionSDR CA140321011Lead · misinstalled(CAN) DURING ENGINE MAGNETO TIMING/SYNCHRONIZATION, FOUND IGNITION SWITCH POSITIONS INCORRECT. TROUBLESHOOTING DETERMINED LT AND RT "P" LEADS REVERSED ON MAGNETOS.Feb 9, 2014 · Cessna 182N · Ignition System WiringSDR CA140321012Bulkhead · cracked(CAN) FS 230.18 BULKHEAD FOUND BADLY CRACKED IN THE AREAS OF THE RUDDER TRAVEL STOPS. ALSO NOTED PREVIOUSLY STOP DRILLED CRACKING.Feb 9, 2014 · Cessna 182N · Fuselage Main, BulkheadSDR CA140321013Brake Assy · misinstalled(CAN) VISUAL INSPECTION FOUND LT AND RT BRAKE INSTALLATION UNAPPROVED FOR USE ON INSTALLED WHEELS. ALSO FOUND BRAKES INSTALL BACKWARDS. ON AFT SIDE OF WHEEL.Feb 9, 2014 · Cessna 182N · BrakeSDR CA140322001Governor · leaking(CAN) PROPELLER GOVERNOR, CSU, FOUND TO BE LEAKING ENGINE OIL HEAVILY FROM THE CONTROL SHAFT.Feb 9, 2014 · Cessna 182N · Propeller GovernorSDR CA140124005Universal Joint · cracked(CAN) WHEN CONTROL YOKE U WAS REMOVED FROM THE ACFT FOR REPAIRS TO SUPPORT STRUCTURE A CRACK WAS FOUND ON BOTH TOP AND BOTTOM SIDES OF CO-PILOT CONTROL YOKE UNIVERSAL JOINT STARTING FROM THE BOLT HOLES AND PROGRESSING TO THE AFT END OF THE U-JOINT. THESE CRACJan 22, 2014 · Cessna 180H · Control Column SectionSDR CA130530009Contact · failed(CAN) UPON ENGINE RUN-UP BEFORE TAKEOFF IT WAS FOUND THAT THE LT MAGNETO WAS VERY ROUGH AND CAUSING THE ENGINE TO BACK FIRE. ACFT WAS RETURNED TO HANGER FOR MAINTENANCE. IT WAS DISCOVERED THAT THE LOWER CONTACT PAD ON THE PN 10-357174 CONTACT ASSY HAD BECOMEMay 29, 2013 · Cessna 182E · Magneto/DistributorSDR CA121101002Riser · cracked(CAN) DURING 50 HR INSPECTION, CRACKED INTAKE MANIFOLD RISER, PN G27658A1 FOUND AT LT SIDE MOUNT AT OIL SUMP FLANGE PERIMETER. CRACKED DUE TO UNEVEN MOUNT SURFACE ON SUMP FLANGE, WELD. ADVISED WARRANTY CLAIM SUBMITTED. REPLACEMENT PARTS ON ORDER.Oct 31, 2012 · Cessna 180F · Reciprocating Engine Front SectionSDR CA120913002Propeller · misoverhauled(CAN) PROPELLER SENT TO MY SHOP WITH POSSIBLE INTERNAL OIL LEAK. NO INTERNAL OIL LEAK, BUT AFTER A VISUAL INSPECTION, DISCOVERED MAJOR ISSUES OF NON-COMPLIANCE FROM LAST O/H. THE O/H WAS DONE IN 2010. I HAVE BEEN IN CONTACT WITH ABOUT THIS, AND COURSE OF ASep 12, 2012 · Cessna 182J · Propeller AssemblySDR CA120718005Snap Ring · failed(CAN) WHILE IN CRUISE FLIGHT, PILOT NOTICED INCREASED RPM AND VIBRATION. PILOT DECREASED RMP AND CARRIED OUT A PRECAUTIONARY LANDING. PROPELLER TECH HISTORY, PROPELLER O/H 21-FEB-11 -AT 1.3 TSO PROPELLER BLADES REPAINTED DUE TO POOR ADHESION -AT 36.1 TSO ACJul 13, 2012 · Cessna 182G · Propeller AssemblySDR CA120403009Exhaust Duct · cracked(CAN) ON INSTALLATION OF THE NEW EXHAUST SYS, THE AME CONDUCTED A FINAL INSPECTION OF THE COLLECTOR AND FOUND 3 HUGE CRACKS ON THE FLANGE WHERE A WELD HAD BEEN CARRIED OUT. THE MFG WAS CONTACTED AND A REPLACEMENT WAS SENT. THIS EXHAUST SHOULD HAVE NEVER PASSApr 3, 2012 · Cessna 180J · Engine Collector/Tailpipe/NozzleSDR 2012FA0000124Piston · failedNUMBER 5 CYLINDER ON O-470 ENGINE WITH APPROXIMATELY 300 HOURS EXPERIENCED PISTON FAILURE DUE TO WHAT APPEARS AT FIRST IMPRESSION DETONATION. HOWEVER, PISTON IS BELIEVE TO HAVE FAILED DUE TO FLAW IN MANUFACTURE OR EXPERIENCE DAMAGE SUCH AS DROPPING PRIOR TO INFeb 20, 2012 · N71890 · Cessna 182M · Reciprocating Engine Cylinder SectionSDR 2011FA0000675Casting · crackedCASTING CRACK FOUND BY VISUAL INSPECTION DURING COURSE OF ANNUAL INSPECTION. THE CRACK IS LOCATED ON THE FORWARD END OF THE SUPPORT CASTING AND RUNS FROM 1/4 INCH FROM MOUNT HOLES ON THE OUTBOARD SIDE TO WITHIN 1/4 INCH OF THE MOUNT HOLES ON THE INBOARD SIDE Oct 13, 2011 · N4944P · Cessna 182G · Fuselage, Landing Gear Attach FittingsSDR 2011FA0000561Bulkhead · crackedWHILE PERFORMING A VISUAL INSP OF THE AFT FUSELAGE BULKHEAD IAW AD 72-07-09; DISCOVERED CRACKS IN THE AFT BULKHEAD BETWEEN THE RUDDER CABLE CUTOUT AND THE BULKHEAD FLANGE (BOTH SIDES). FOLLOWING THE INSTRUCTIONS IN THE AD, PERFORMED A TORQUE CHECK OF THE BOLJul 28, 2011 · N91568 · Cessna 182M · Fuselage Main, BulkheadSDR 2011FA0000143Muffler · obstructedTHE STARBOARD MUFFLER BAFFLE CONE BROKE LOOSE FROM THE MUFFLER HOUSING AND OBSTRUCTED THE EXHAUST PIPE, CREATING BACK PRESSURE IN THE EXHAUST SYSTEM WHICH CAUSED THE ENGINE TO LOSE POWER. THE SUBSEQUENT FORCED LANDING ACCIDENT SUBSTANTUALLY DAMAGED THE AIRCRAFMar 2, 2011 · N3420U · Cessna 182F · Engine Noise SuppressorSDR MROA20102Cylinder · leakingROUTINE DIFFERENTIAL COMPRESSION TEST RESULTING IN A 48/80 READING WAS CAUSED BY A LEAKING EXHAUST VALVE. THE CYLINDER ASSY WAS R & R WITH A NEW CYLINDER ASSY.Nov 26, 2010 · N42801 · Cessna 182L · Reciprocating Engine Cylinder SectionSDR 2010FA0001154Piston · crackedACFT WAS IN CRUISE FLIGHT AND EXPERIENCED AN ENGINE FAILURE. THE CASE WAS CRACKED ABOVE THE NR5 CYLINDER AND INSP THROUGH THE OIL FILLER TUBE REVEALED TNE NR5 PISTON WAS COMPLETELY DESTROYED. THIS ENGINE WAS O/H 17 YEARS AGO. INSP REVEALED THE ACFT IS CURREOct 19, 2010 · N808HC · Cessna 182L · Reciprocating Engine Power SectionSDR CA101230006Cylinder · separatedDURING A 100 HR ANNUAL INSP IT WAS OBSERVED THAT NR 3 CYL BARREL HAD SEPARATED FROM THE HEAD. THE CYL WAS REPLACED WITH NEW WITH NO FURTHER INCIDENTS.Oct 7, 2010 · Cessna 180J · Reciprocating Engine Cylinder SectionSDR CA100218008Cylinder · damaged(CAN) DURING A 100 HOUR INSP, A ROUTINE COMPRESSION TEST WAS CARRIED OUT AS PART OF ENGINE ON CONDITION PROGRAM IAW AN B041. A LEAK WAS NOTED ASSOCIATED WITH LOW COMPRESSION ON THE NR 5 CYL ASSY AT TOP DEAD CTR. THE PISTON WAS THEN PLACED AT BOTTOM DEAD CTR ANFeb 18, 2010 · Cessna 182P · Reciprocating Engine Cylinder SectionSDR 2009FA0000721Attach Fitting · damagedCOMPIED WITH AD72-07-09 DATED 10/17/74 BY INSP AND FOUND SIGNS OF WORKING AT LEFT SIDE AND RIGHT SIDE AFT VERTICAL FIN ATTACHMENT BOLTS. PERFORMED DYE PENETRANT INSP IAW PARA C,1, D, 1 AND 2 WITH NO CRACKS FOUND. CHECKED ATTACHMENT HOLES FOR EXCESSIVE ELONGAJul 10, 2009 · N42154 · Cessna 182L · Vertical Stabilizer, Attach FittingsSDR 2009FA0000281Reinforcement · crackedFOUND DURING ANNUAL INSP, LT ATTACHMENT PIVOT POINT FOR HORIZ STAB (REINFORCEMENT ASSY PN 07120487) CRACKED AT BOLT HOLE EXTENDING TO EDGE OF BRACKET. REPLACED REINFORCEMENT ASSY AND IB BRACKET PN 0712302-1. ACFT TT AND PART TT 7201. (K)Mar 31, 2009 · N5441B · Cessna 182 · Horizontal Stabilizer StructureSDR CA081107003Seat Track · cracked(CAN) 3 CRACKS LT PAS RAIL, 1 CRACK LT PILOTS RAIL, SEAT RAILS SOME WEAR, WEAR WITHIN LIMITS.Nov 3, 2008 · Cessna 182J · Fuselage, Seat/Cargo Attach FittingsSDR 2008FA0000574Impulse Coupling · failedPILOT PERFORMED PRE-FLIGHT INSP DISCOVERED OIL ON FWD PORTION OF COWLING, SLIGHT OIL RESIDUE ON WINDSHIELD. MECHANIC REMOVED TOP COWLING TO INVESTIGATE, DISCOVERED MAGNETO HOUSING SHATTERED AT AREA IMMEDIATELY ADJACENT TO IMPULSE COUPLING. APPARENTLY IMPULSEAug 15, 2008 · N92551 · Cessna 182N · Magneto/DistributorSDR CA080711005Piston · broken(CAN) A PIECE OF NR 2 PISTON SKIRT WAS BROKEN OFF AT THE OIL CONTROL RING GROOVE.Jun 20, 2008 · Cessna 182K · Reciprocating Engine Cylinder SectionSDR 2008FA0000074Cylinder · damagedWHILE PERFORMING A COMPRESSION CHECK TO FIND AN OIL LEAK, FOUND NR 1 CYLINDER WITH O COMPRESSION. PULLED CYLINDER OFF AND FOUND THE PLATING ON THE CYLINDER LOOSE AND FLAKING OFF. (K)Jan 15, 2008 · N1928X · Cessna 182H · Reciprocating Engine Cylinder SectionSDR CA071212025Hub · corroded(CAN) AT OVERHAUL PROPELLER HUB WAS STRIPPED OF PAINT FINISH. ENTIRE OUTER SURFACE OF HUB AND BLADE O-RING GROOVES WERE CORRODED BEYOND LIMITS. HUB WAS RETURNED TO MFG FOR EVALUATION. (TC NR 20071212025)Dec 12, 2007 · Cessna 180J · Propeller Hub SectionSDR 2007FA0000840Carburetor · failedPILOT REPORTED THAT AFTER A NORMAL START, HE WAS UNABLE TO ADVANCE THE THROTTLE CONTROL TO CRUISE OR TAKEOFF POWER. A PARTIAL DISASSEMBLY OF THE CARBURETOR REVEALED THAT THE AIR METERING PIN/AIR METERING JET WAS BLOCKING THE THROTTLE SHAFT TRAVEL. THE CARBURAug 18, 2007 · N2347R · Cessna 182G · Fuel Control/Reciprocating EnginesSDR CA070823010Torque Tube · loose(CAN) MINOR PLAY (UP AND DOWN) ON THE RT ELEVATOR CAUSE BY LOOSE RIVETS ON THE TORQUE TUBE (TC NR 20070823010)Jul 25, 2007 · Cessna 182G · Elevator StructureSDR CA070830002Hub · cracked(CAN) HUB THREADS FOUND CRACKED DURING OVERHAUL PROCESS (TC NR 20070830002)Jul 19, 2007 · Cessna 180E · Propeller Hub SectionSDR 2007FA0000637Piston · fracturedAFTER INSTALLING NEW CYLINDER ASSY SA47006S-A20P WITH NEW PISTON ASSY PN SA640518, WE WERE PERFORMING BREAK IN RUN AT LOW POWER, FIRST AT 800 RPM FOR 2 MIN. SHUTDOWN ENGINE, CLEANED FOULED PLUGS DUE TO OIL IN CYLINDER FROM ASSY. RAN ENGINE AT 1000 RPM FOR 3 Jun 13, 2007 · N1858X · Cessna 182H · Reciprocating Engine Power SectionSDR 2007FA0000634Support · crackedMECH DISCOVERED ON A 50 HR INSP, THE SUPPORT COLLAR ON THE AIRBOX MOUNTED TO THE CARBURETOR WAS CRACKED. THIS COULD LEAD TO THE SEPARATION OF THE AIRBOX FROM THE CARBURETOR AND LOSS OF POWER. PN 0750288 WAS REPLACED WITH NEW SUPPORT COLLAR PN 0750288-1 IAW SMay 20, 2007 · N2803Y · Cessna 182E · Engine Air Intake System
Back to Continental O-470R