Continental IO-550 series

Service difficulty reports · 239

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 = 'IO550'
  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 2009FA0000345Control Cable · brokenAILERON CABLE SWAGE BROKE, CAUSING LOSS OF AILERON CONTROL.Apr 27, 2009 · N934V · Beech V35B · Aileron Control SystemSDR 2009FA0000295Flange · crackedCUSTOMER REPORTED LARGE OIL LEAK. INSPECTED AND FOUND NR 2 STANDBY ALTERNATOR MOUNTING FLANGE CRACKED. .7500 OF THE FLANGE HAD COMPLETELY SEPARATED FROM THE ALTERNATOR. ONLY ONE MOUNTING STUD HELD THE ALTERNATOR ON THE ENGINE. CORRECTIVE ACTION WAS TO INSTApr 14, 2009 · N256CD · Cirrus SR22 · DC Generator-AlternatorSDR 2009FA0000442Starter · damagedSTARTER ADAPTER FAILURE 3 TIMES SINCE BUYING THE ACFT NEW IN NOV 02. THE MFG SUPPLIED STARTER DOES NOT RELEASE THE STARTER ADAPTER AFTER START UP CAUSING DAMAGE TO THE ADAPTER. FAILURE IS NOTED AS THE STARTER FAILS TO TURN THE PROP BUT THE SOUND OF THE STARTERFeb 18, 2009 · N406C · Cirrus SR22 · Engine StarterSDR 2009FA0000055Duct · dislodgedTHE BYPASS DOOR ON THE ENGINE AIR INDUCTION FILTER DUCT TO THE THROTTLE BODY WAS FOUND LAYING IN THE BOTTOM OF THE DUCT, THE DOOR PIN HAD FALLEN OUT AND THE DOOR, THE SPRING, AND THE HINGE PIN WERE FOUND IN THE BOTTOM OF THE DUCT , NO PARTS HAD GONE ANY FURTHEFeb 3, 2009 · N602MB · Cessna U206G · Engine Air Intake SystemSDR 2009FA0000424Bearing · damagedPILOT REPORTED PITCH OSCILLATIONS WITH AUTOPILOT ENGAGED. AUTOPILOT WAS DISENGAGED MANUALLY, AND ACFT WAS HAND FLOWN TO DESTINATION. AUTOPILOT COMPUTER, PITCH SERVO, AND FLIGHT COMMAND INDICATOR REMOVED AND SENT OUT FOR BENCH TEST. FLIGHT COMMAND INDICATOR Jan 14, 2009 · N628SF · Beech 58 · Autopilot SystemSDR 2008FA0000681Cylinder · crackedAIRCRAFT OWNER REPORTED SEVERE VIBRATION. AFTER INSPECTION IT WAS FOUND THAT SPINNER BULKHEAD WAS SEVERELY CRACKED. AFTER FURTHER INSPECTION NR 1 CYLINDER WAS FOUND TO BE CRACKED ALL AROUND THE CIRCUMFERENCE OF THE CYLINDER DIAMETER. THE CRACK WAS RIGHT AT THOct 14, 2008 · N6036 · Beech A36 · Reciprocating Engine Cylinder SectionSDR 2008FA0000639Hinge · corrodedFLAP HINGES IN ALL POSITIONS BOTH LT AND RT HAVE INTERGRANDULAR CORROSION NEAR THE POINT OF FAILURE. PN 13431-003, PN 13431-004, 13432-002, QTY 2, 13433-006, 13433-005. CONDITION WAS FOUND AT ANNUAL INSPECTION. (K)Sep 2, 2008 · N121HC · Cirrus SR22 · Trailing Edge FlapsSDR 2008FA0000589Drive Shaft · shearedTHIS AC HAS HAD 5 FAILURES OF THE AIR CONDITIONING COMPRESSOR DRIVE SHEAR SHAFT. THE AVERAGE TIME BETWEEN FAILURES IS 35.8 HOURS. THE SAME SHAFT BUILT BY ANOTHER MFG, HAS HAD ZERO FAILURES. WE HAVE HAD SEVERAL FAILURES IN DIFFERENT AC WITH THIS PART. THE DESIGAug 26, 2008 · N433CF · Cirrus SR22 · Cabin Compressor SystemSDR 2008FA0000565Intake Duct · crackedMFG SUPPLIED ENGINE INTAKE DUCT BEFORE THE AIR FILTER IS SUBJECT TO CRACKING IN MULTIPLE LOCATIONS. THIS PARTICULAR AC AND ANOTHER IDENTICAL MODEL AC THIS FACILITY MAINTAINS, HAVE BEEN CONVERTED TO ANOTHER ENGINE AFTER THE STC CONVERSION. CRACKING PROBLEM HAAug 13, 2008 · N602MB · Cessna TU206G · Engine Air Intake SystemSDR 2008FA0000378Transmitter · malfunctionedFOLLOWING ACTIONS WERE TAKEN AS A RESULT OF A PRECAUTIONARY LANDING, WHERE PILOT REPORTED A LOSS OF OIL PRESSURE. AT CRUISE, AT 8000 FT, OIL PRESSURE ANNUNCIATOR LIGHT ILLUMINATED, OIL PRESSURE GAUGE INDICATED NO OIL PRESSURE. AFTER LANDING, OIL PRESSURE REApr 15, 2008 · N748CD · Cirrus SR22 · Engine Oil PressureSDR 2008FA0000264Pump · failedVACUUM PUMP FAILED TO DEVELOP ANY AIR OUTPUT UPON INSTALLATION. REMOVED PUMP AND INSPECTED, SUSPECT VANES ARE NOT SLIDING OUT AGAINST CYLINDER WALL THUS NOT ALLOWING ANY AIR TO BE DEVELOPED. (K)Apr 2, 2008 · N8050U · Beech 58 · Vacuum Distribution SystemSDR HYT2008F00000Hose · failedMETERED FUEL PRESSURE HOSE FAILED. THIS HOSE RUNS FROM THE FUEL INJECTOR DISTRIBUTOR TO THE FIREWALL. LOW PRESSURE TEST OF FAILED HOSE REVEALED MULTIPLE LEAKS ALONG LENGTH OF HOSE. HOSE WAS INSTALLED NEW ON 4/8/03/ HOSE FAILURE NOTED ON 2/26/08 WHEN ENGINEFeb 26, 2008 · N91027 · Cessna 207 · Aircraft Fuel Distribution SystemSDR FAA2008123001Pilot Valve · brokenPROPELLER WENT TO FEATHER IN FLIGHT AND WAS UNABLE TO UNFEATHER. AFTER RECEIVING THE GOVERNOR FOR INSPECTION IT WAS DISCOVERED THAT THE BOTTOM END OF THE PILOT VALVE (P/N 5221-220) HAD BROKEN OFF AND WAS MISSING. IT WAS PRESUMED THAT IT EXITED THE BOTTOM END OJan 23, 2008 · N401BC · Beech 58 · Propeller Controlling SystemSDR 2007FA0001106Wire Harness · damagedALTERNATOR FAILED ON FIRST FLIGHT AFTER INSTALLATION FROM OVERHAUL. FOUND FIELD WIRE RIPPED OUT OF FIELD BRUSH AND BARE WIRE DEBRIS INSIDE ALTERNATOR CASE. SUSPECT WIRE EPOXY HOLD DOWN VIBRATED LOOSE ALLOWING ROTOR ASSEMBLY TO SNAG WIRE.Dec 22, 2007 · N1501C · Cirrus SR22 · Electrical Power System WiringSDR FAA010208001Unknown · malfunctionedPFD AND GPS/NAV1 BOTH REBOOTED AT THE SAME TIME. RESTARTED WITHOUT GOING THROUGH EITHER ITS STANDARD INITIALIZATION OR ITS FAST START ROUTINE. THE AUTOPILOT SEEMED TO BE STILL ENGAGED BUT THE VS SELECTION, QNH, ALTITUDE PRE-SELECT AND HEADING WERE RESET AND Nov 30, 2007 · N123DV · Cirrus SR22 · Electrical Power System WiringSDR 2009FA0000443Wire · looseROLL TRIM ACTUATOR HAS MALFUNCTIONED ON 3 OCCASSIONS SINCE BUYING ACFT NEW IN 02. IN EACH CASE THE WIRES LEADING TO THE ELECTRIC MOTOR HAD COME LOOSE CAUSING THE TRIM ACTUATOR TO HOLD FULL LT AILERON. WITHOUT OVERPOWERING THE UNIT A FATAL CRASH WOULD HAVE RESUSep 12, 2007 · N406C · Cirrus SR22 · Flight Control System WiringSDR 2007FA0000822Pin · shearedTHE LOWER IB BUSHING ON THE LOWER TORQUE LINK KNEE WAS DRY AND THE PIVOT PIN WHICH RIDES IN THE BUSHING WAS VERY TIGHT POSSIBLY DUE TO A PLUGGED GREASE ZERK FITTING. THIS APPARENTLY CAUSED THE CLEVIS RETAINING PIN TO SHEAR (AS EVIDENCED BY THE SHEAR MARKS ON TSep 4, 2007 · N998PL · Beech A36 · Main Landing GearSDR 2007FA0000524Engine · failedON MAY 11, 2007 AT APPROXIMATELY 1815 EST, 2205Z, A BEECH BE-36-A36 BONANZA, N814JG, S/N E-2622, AT CRUISE HAD A DECREASE IN ENGINE CYLINDER TEMPERATURE, FOLLOWED BY A LOSS OF OIL PRESSURE AND ENGINE POWER WITH SUBSEQUENT ENGINE FAILURE. THE AIRCRAFT MADE AN EMay 11, 2007 · N814JG · Beech A36 · Engine (Reciprocating)SDR 050207Rod End · brokenCABIN DOOR DEPARTED AIRCRAFT IN FLIGHT DUE TO THE ROD END HINGE FAILURE. IT APEARS THE ROD END FAILED DUE TO FATIGUE. THE ROD END SHOULD BE MADE OF A STRONGER MATERIAL.May 2, 2007 · N299JW · Cirrus SR22 · Passenger/Crew DoorsSDR 2007FA0000375Control Cable · interferenceDURING INSPECTION FOUND INTERFERENCE BETWEEN RUDDER/AILERON INTERCONNECT SYSTEM AND RT AILERON CABLE. CHECKED RIGGING AND FOUND CABLE CLAMP ON RT AILERON CABLE OUT OF POSITION. VISUAL INSPECTION INDICATES NO MOVEMENT BETWEEN CABLE AND CLAMP AND RECORDS REVIEW Apr 27, 2007 · N220SR · Cirrus SR22 · Rudder Control SystemSDR ODAR3Alternator · destroyedOWNER REPORTED NR 2 ALTERNATOR LIGHT ILLUMINATED. REMOVED TOP COWLING TO INSPECT NR 2 ALTERNATOR. FOUND NR 2 ALTERNATOR BROKEN OFF AT MOUNTING PLATE BY (3) STUDS. ONE STUD STILL ATTACHED WITH NUT, BUT LOOSE. REMOVED P/N BC410-1, S/N 0921403. PICTURES AVAILApr 11, 2007 · N15DR · Cirrus SR22 · AC Generator-AlternatorSDR 15DRAlternator · destroyedOWNER REPORTED NR2 ALTERNATOR LIGHT ILLUMINATED. REMOVED TOP COWLING TO INSPECT NR2 ALTERNATOR. FOUND NR2 ALTERNATOR BROKEN OFF AT MOUNTING PLATE BY (3) STUDS. ONE STUD STILL ATTACHED WITH NUT, BUT LOOSE. REMOVED P/N BC410-1, S/N 0921403.Apr 11, 2007 · N15DR · Cirrus SR22 · AC Generator-AlternatorSDR ODAR15DR1Alternator · destroyedOWNER REPORTED NR2 ALTERNATOR LIGHT ILLUMINATED. REMOVED TOP COWLING TO INSPECT NR2 ALTERNATOR. FOUND NR2 ALTERNATOR BROKEN OFF AT MOUNTING PLATE BY (3) STUDS. ONE STUD STILL ATTACHED WITH NUT, BUT LOOSE. REMOVED P/N BC410-1, S/N 0921403.Apr 11, 2007 · N15DR · Cirrus SR22 · AC Generator-AlternatorSDR A6Y2007F00001Cooling Fan · out of positionAPPROXIMATELY 20 MINUTES INTO THE FLIGHT PILOT SUSPECTED AN ELECTRICAL BURNING ODOR. HE NOTICED SOME SMOKE COMING FROM UNDER INSTRUMENT PANEL. AT THAT TIME HE COMPLETED THE MEMORY ITEMS FOR (ELECTRICAL SMOKE OR FIRE). AFTER 1 TO 2 MINUTES SMOKE AND ODOR DISMar 4, 2007 · N8257H · Beech 58 · Communications SystemSDR 2007FA0000171Torque Tube · bindingDURING REPLACEMENT OF ORIGINAL EQUIPMENT TORQUE TUBE (P/N 5045010-18/19) WITH MFG REPLACEMENT P/N 5045010-32/33 INTERFERENCE BETWEEN THE TORQUE TUBE AND AIRFRAME ATTACHMENT FITTING WAS DISCOVERED. RIGGING THE MLG TO ACHIEVE A .1250 DROP OFF WAS IMPOSSIBLE DUEFeb 20, 2007 · N467DB · Cessna 340A · Landing Gear Retraction/Extension SystemSDR 2006FA0001193Pump · burned outSMOKE IN THE COCKPIT, AND ELECTRICAL BURNING SMELL WERE OBSERVED AFTER TAKEOFF, AFTER THE GEAR WAS RETRACTED. THE HEATER HAD BEEN IN OPERATION APPROXIMATELY 30 MINUTES BEFORE TAKEOFF, WITH NO SMOKE OR SMELL OBSERVED. THE HEATER WAS TURNED OFF, AND THE SMOKE DDec 18, 2006 · N870JA · Beech 58 · Heating SystemSDR 2007FA0000010Battery · leakingDURING ANNUAL INSPECTION, FOUND BATTERY COMPARTMENT CONTAMINATED BY LEAKAGE FROM D CELLS AND BATTERY TERMINALS CORRODED. BATTERIES FOUND DEAD. BATTERIES WERE INSTALLED MARCH 2004 AND HAVE A EXPIRATION DATE OF MARCH 2008. THE MODEL ELT IS CERTIFIED BY THE MFDec 18, 2006 · N910JR · Cirrus SR22 · Emergency Locator BeaconSDR 2007FA0000734Volt Regulator · failedTHE INABILITY OF THE VOLTAGE REGULATOR (PN 800397-501, SN 0165) TO CONTROLTHE OUTPUT OF THE ALTERNATOR WHEN THE BATTERY SWITCH WAS TOGGLED BETWEEN THE NR1 AND NR 2 BATTERY, IN FLIGHT. (K)Jul 24, 2006 · N999JW · Mooney M20R · AC RegulatorSDR N8142GFirewall · crackedWHILE UNDERGOING AN ANNUAL INSPECTION THE ENGINE FIREWALL WAS FOUND TO BE CRACKED WHERE THE EXHAUST HANGER BRACKETS ATTACH ON THE LT SIDE. ADDITIONAL CRACKING WAS ALSO FOUND ON THE INNER BULKHEAD.Jun 27, 2006 · N8142G · Cessna 210K · Fuselage Main, BulkheadSDR FAA0607001Firewall · crackedWHILE UNDERGOING AN ANNUAL INSPECTION THE ENGINE FIREWALL WAS FOUND TO BE CRACKED WHERE THE EXHAUST HANGER BRACKETS ATTACH ON THE LT SIDE. ADDITIONAL CRACKING WAS ALSO FOUND ON THE INNER BULKHEAD.Jun 27, 2006 · N8142G · Cessna 210K · Fuselage Main, BulkheadSDR FAA0607002Firewall · crackedWHILE UNDERGOING AN ANNUAL INSPECTION THE ENGINE FIREWALL WAS FOUND TO BE CRACKED WHERE THE EXHAUST HANGER BRACKETS ATTACH ON THE LT SIDE. ADDITIONAL CRACKING WAS ALSO FOUND ON THE INNER BULKHEAD.Jun 27, 2006 · N8142G · Cessna 210K · Fuselage Main, BulkheadSDR 2006FA0000576Nut · splitTHRU STUD NUT SPLIT ON NR 4 CYLINDER TOP THRU STUD. (K)Jun 6, 2006 · N746C · Cirrus SR22 · Reciprocating Engine Power SectionSDR 2006FA0000580Connecting Rod · unknown50 MILES OUT OF HOME BASE, PILOT HEARD A (POP) CAME FROM LEFT ENGINE, THEN NOTICED OIL PRESSURE START THE FALL. FEATHERED PROP AND SECURED ENGINE. MADE A UNEVENTFUL LANDING. INSP FOUND NR 4 CYLINDER ON L/E DDEPARTED FROM ENGINE AND NR 4 ROD BROKEN. SUSPECMay 8, 2006 · N106GA · Beech 58 · Reciprocating Engine Power SectionSDR 2006FA0000412Thru Bolt · brokenTHE ENGINE CRANKCASE THRU-BOLT BROKE. THIS THRU-BOLT IS LOCATED UNDER THE TOP OF THE OIL COOLER ADAPTER PLATE THRU TO THE NR 6 CYL TOP FRONT. IT BROKE OFF FLUSH AT THE CYL BASE WHILE IN FLIGHT. THE BOLT END WHICH BROKE OFF WITH THE CYL BASE NUT FLEW OUT THE FRApr 24, 2006 · N4918R · Cessna A188B · Reciprocating Engine Power SectionSDR AVI000021Elevator · out of toleranceDURING SA 06-05 ELEVATOR GAP VISUAL INSPECTION IT WAS NOTED THAT THE GAP BETWEEN ELEVATOR TIP AND HORIZONTAL STABILIZER WAS LESS THEN 0.10 INCH, UPON FURTHER INVESTIGATION IT WAS NOTED THAT PN 11626-002 ELEVATOR HINGE, OB WAS RUBBING ON HORIZONTAL STABILIZER OApr 19, 2006 · N753CD · Cirrus SR22 · Elevator StructureSDR 2006FA0000454Cylinder · crackedNR 5 CYLINDER CRACKED AFT OF VALVES. (STILL HAD GOOD COMPRESSION BUT COULD HEAR AIR) (LT ENGINE) (K)Apr 18, 2006 · N3149P · Beech 58 · Reciprocating Engine Cylinder SectionSDR 2006FA0000455Cylinder · crackedNR 2 CYLINDER COMPLETELY CRACKED ALL THE WAY AROUND AFT OF VALVES. (LT ENGINE) (K)Apr 18, 2006 · N3149P · Beech 58 · Reciprocating Engine Cylinder SectionSDR 2006FA0000456Cylinder · crackedNR 6 CYLINDER CRACKED AFT OF VALVES. (STILL HAD GOOD COMPRESSION COULD HEAR AIR.) (LT ENGINE) (K)Apr 18, 2006 · N3149P · Beech 58 · Reciprocating Engine Cylinder SectionSDR 2006FA0000457Cylinder · crackedNR 4 CYLINDER CRACKED AFT OF VALVES. (STILL HAD GOOD COMPRESSION BUT COULD HEAR AIR) (LT ENGINE) (K)Apr 18, 2006 · N3149P · Beech 58 · Reciprocating Engine Cylinder SectionSDR 2006FA0000239Relief Valve · restrictedLOSS OF OIL PRESSURE, INSPECTED OIL PRESSURE RELIEF VAVLE AND FOUND TIP OF DRILL BIT LODGED IN RELIEF VALVE. REMOVED TIP OF DRILL BIT AND REASSEMBLED RELIEF VALVE. GROUND RAN, OPS CHECKED GOOD. (K)Mar 15, 2006 · N216N · Cirrus SR22 · Reciprocating Engine Oil SystemSDR 2006FA0000236Flight Dir · intermittentJUST GOT 2003 SR22 BACK FROM GETTING REVISION 6 COMPLETED. PUT ABOUT 10 HOURS ON THE AIRPLANE. TWICE DURING THIS TRIP, THE PFD DISPLAY ROTATED OR ROLLED LIKE THE OLD TELEVISION SETS DID. ONCE FOR ONLY 2 OR 3 SECONDS AND ANOTHER TIME FOR MAYBE 10 TO 20 SECONFeb 27, 2006 · N56FS · Cirrus SR22 · Flight Management Computing Hardware SystemSDR 2006FA0000389Actuator · failedMECHANICAL FAILURE OF THE RT MLG DOOR ACTUATOR, PREVENTED THE EXTENSION OF THIS AC LANDING GEAR EITHER BY NORMAL OF EMERGENCY PROCEDURES. THE FAILURE WAS THE ACTUATOR GLAND AND CIRCLIP COMING APART FROM THE ACTUATOR. THE RT MLG ACTUATOR WAS REMOVED AND RESEAJan 28, 2006 · N4FL · Cessna 210L · Landing Gear Door ActuatorSDR 2006FA0000096Transmitter · intermittentELT TRANSMITTER WAS REMOVED DURING ANNUAL FOR BATTERY REPLACEMENT AND TESTING. UPON TEST WITH BATTERIES REPLACED. THE UNIT ON/OFF WAS INTERMITTENT AND THE REMOTE OPERATION WAS INTERMITTENT. UNIT IS APPROXIMATELY 7 YEARS OLD. TREND OF FAILURES ON THIS MAKEJan 17, 2006 · N2164K · Mooney M20R · Emergency Locator BeaconSDR 2006FA0000123Mount · crackedDURING SCHEDULED INSPECTION FOUND THE FUEL FLOW TRANSDUCER MOUNT CRACKED COMPLETELY ACROSS ON ONE END. (K)Jan 13, 2006 · N8419Q · Cessna U206F · Aircraft Fuel SystemSDR 2006FA0000121Arm · wornTROUBLESHOT STIFF RUDDER PEDAL STEERING AND REPLACED PILOTS RT ARM ASSY. PN 002-524012-1 WITH NEW IAW MM. APPEARS ARM ASSY ROLLER BEARING WAS NEVER LUBED DURING BUILD OF AIRCRAFT. THE ROLLER BEARING WEAR CAUSED THE ARM TO SEIZE ON THE RUDDER PEDAL TORQUE TUJan 10, 2006 · N3224G · Beech A36 · Rudder Control SystemSDR 2006FA0000060Bushing · wornAILERON TRIM MADE POPPING NOISE AS CONTROL WAS ROTATED. FOUND BUSHING FOR CONTROL SHAFT IN PEDESTAL SEVERELY WORN ALLOWING U-JOINT TO CONTACT STRUCTURE AS CONTROL WAS ROTATED. TRIM CABLE TENSION WAS WITHIN LIMITS, NO REASON FOR ACCELERATED WEAR NOTED. BUSHIJan 5, 2006 · N376W · Beech 58 · Aileron TabsSDR 2006FA0000003Dipstick · brokenDURING PREFLIGHT WHILE CHECKING OIL LEVEL ON DIPSTICK, ENTIRE ROD PORTION OF DIPSTICK CAME APART IN MY HANDS UPON LIFTING IT OUT OF OIL FILLER TUBE. BARELY CAUGHT IT WITH MY HAND BEFORE IT WOULD'VE FALLEN DOWN INSIDE THE ENGINE CRANKCASE WITH POTENTIALLY CATAJan 4, 2006 · N5175L · Cirrus SR22 · Reciprocating Engine Oil SystemSDR 2006FA0000004Dipstick · brokenDURING PREFLIGHT WHILE CHECKING OIL LEVEL ON DIPSTICK, THE ENTIRE ROD PORTION OF THE DIPSTICK CAME APART IN MY HANDS UPON LIFTING IT OUT OF THE OIL FILLER TUBE. BARELY CAUGHT IT WITH MY HAND BEFORE IT WOULD'VE FALLEN DOWN INSIDE THE ENGINE CRANK CASE WITH POTEJan 4, 2006 · N5175L · Cirrus SR22 · Reciprocating Engine Oil SystemSDR AU510001653Vent Line · leakingRT FUEL VENT LEAKING. INVESTIGATION FOUND THAT THE SEALANT AROUND THE VENT TUBE IN THE RT WET WING FUEL TANK HAD DETERIORATED ALLOWING FUEL TO LEAK INTO THE VENT LINE.Dec 12, 2005 · Beech 58 · Aircraft Fuel Distribution SystemSDR 2006FA0000006Valve · out of rigTHE NEW VALVE RECEIVED FROM THE MFG WAS INTERNALLY CLOCKED INCORRECTLY. AFTER INSTALLATION, NO FUEL WAS AVAILABLE FROM EITHER THE ON OR CROSSFEED PORTS. AFTER MALVE REMOVAL, IT WAS CONFIRMED THAT THE VALVE REMAINED IN THE OFF POSITION REGARDLESS OF MOVMENT TDec 8, 2005 · N2347G · Beech 58 · Standard Practices/Structures
Back to Continental IO-550 series