Eci IO-360

Service difficulty reports · 86

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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 = 'IO360'
  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 2023FA0000622Cylinder · crackedPILOT REPORTED LOSS OF ENGINE POWER. BEGAN TO RUN ROUGH. MADE A PRECAUTIONARY NORMAL LANDING. MECHANIC REMOVED COWLING AND FOUND A CRACKED NR 4 CYLINDER. LB STATED NEW CYLINDERS WERE INSTALLED AT ENGINE OVERHAUL AT 1481.6 HOURS AGO. THE CYLINDER WAS REPLACED Oct 20, 2023 · N174GF · Cessna 172R · Reciprocating Engine Cylinder SectionSDR 2021FA0000407None · looseDURING R/H AILERON BELLCRANK CABLES DISCONNECTION FOR CLEANING / INSPECTION / LUBE, FOUND BELLCRANK ASSY P/N 47350-2 CONSTITUTED OF PIVOT BALL BEARING HOUSING P/N MS20218-1 SECURED TO BELLCRANK PLATE P/N 47349-2 EXHIBITING ONE (1) EACH OUT OF THREE (3) EACH LDec 16, 2021 · N1420J · Gulstm 112A · Aileron Control SystemSDR 4RPA201307010001Pump · failedLEFT ENGINE FUEL FLOW DROPPED FROM 25 GALLONS AN HOUR AT TOP OF CLIMB TO 7 GALLONS AN HOUR AT ALL POWER SETTINGS. ELECTRIC FUEL PUMP SWITCH ALSO FAILED. PILOT USED ENGINE PRIMER BUTTON TO KEEP ENGINE RUNNING. USE OF PRIMER BUTTON INCREASED FUEL FLOW TO 25 GJun 28, 2013 · N9450C · Piper PA34200T · Engine Fuel PumpSDR 2012FA0000727Power Supply · failedLEFT STROBE INOPERATIVE. TESTED FLASH TUBE WITH ANOTHER POWER SUPPLY - FUNCTION CHECK OK. PULLED THE POWER SUPPLY AND OPENED - EVIDENCE OF CAPACITOR EXPLOSION AND ELECTROLYTE SPILLAGE.Oct 25, 2012 · N2075T · Cirrus SR20 · Exterior LightingSDR 2012FA0000517Cowl Door · departedDURING DESCENT THROUGH 7,000 FT, TOP COWL ASSEMBLY DEPARTED THE ACFT AND STRUCK THE LEFT WINDSCREEN CAUSING A LARGE HOLE. FURTHER INSPECTION REVEALED THAT THE RIGHT SIDE BOTTOM COWL PLATE ASSY WAS ELONGATED FROM WEAR WITH THE TOP COWL ENGAGEMENT PIN, AND THE Jul 9, 2012 · N4428T · Piper PA28R200 · Engine Cowling SystemSDR 2012FA0000343Case · crackedDURRING PRE FLIGHT FOUND OIL ON COWLING. INVESTIGATION FOUND A CRACK IN THE RT FWD TOP OF THE ENGINE CASE.May 29, 2012 · N579RC · Cirrus SR20 · Reciprocating Engine Power SectionSDR 2011FA0000544Bolt · looseWHILE COMPLYING WITH AD 11-07-13 LT AND RT ELEVATOR SPAR, IT WAS NOTED THAT THE HORIZONTAL STAB WAS LOOSE AT BOTH THE FRONT AND REAR MOUNTING POINTS. MOVEMENT WAS MOST NOTED AT THE FWD PORTION OF THE STAB WITH A ROCKING MOVEMENT SIDE TO SIDE. UPON INVESTIGATAug 22, 2011 · N1148J · Gulstm 112A · Horizontal Stabilizer, Attach FittingsSDR 2011FA0000373Filter Element · splitDURING ROUTINE INSPECTION, AIR FILTER WAS FOUND SPLIT OPEN AT THE SEAM. IT IS A CYLINDRICAL SHAPE AND IT WRAPS AROUND A METAL SCREEN. THE SPLIT AREA COMPRISED SEVERAL SQ INCHES OF UNFILTERED AIRPATH.Jun 9, 2011 · N41AT · Piper PA28R200 · Engine Air Intake SystemSDR 2011FA0000334Spar · corrodedDURING REPAIR OF LT WING THE AFT SPAR ATTACH FITTING WAS REMOVED. SEVERE CORROSION WAS FOUND UNDER THE FITTING. PROBABLE CAUSE IS TRAPPED MOISTURE, LACK OF PREVENTATIVE TREATMENT AND LACK OF PROPER INSPECTION OF AREA.May 18, 2011 · N41WA · Piper PA28R180 · Wing SparSDR NX4R000013Mount · crackedDURING ROUNTINE MX, THE TECH WAS PERFORMING A PRELIMINARY/HIDDEN DAMAGE INSP OF THE AREA SURROUNDING THE AREA WHERE WORK WAS TO BE PERFORMED. NOTICED THE SMALL TUBE THAT IS WELDED TO THE LOWER ENGINE MOUNT TUBE THAT THE LOWER COWL IS MOUNTED TO, WAS MOVING SLIApr 28, 2011 · N701ER · Piper PA28R201 · Engine Mount SectionSDR NX4R000011Attach Fitting · brokenDURING TAKEOFF, THE PILOT RETRACTED THE LANDING GEAR. THE GEAR "UNSAFE LIGHT" REMAINED ILLUMINATED. ALSO THE ATC TOWER CONTROLLER ADVISED THE CREW THAT THEIR NLG APPEARED TO REMAIN IN THE DOWN POSITION. AN UNEVENTFUL LANDING WAS MADE AND THE LANDING GEAR INSApr 20, 2011 · N716ER · Piper PA28R201 · Fuselage Main, Attach FittingsSDR 2011FA0000054Shaft · failedMAG SHAFT COMPLETELY SEPARATED FROM THE MAG AS THE SHAFT EXITED THE MAG. CAUSING INOPERATIVE SYS, LOSS OF 1/2 ENGINE IGNITION AND ASSOCIATED WARNING LIGHTS IN THE COCKPIT.Jan 28, 2011 · N705CM · Amtr RV7 · Magneto/DistributorSDR 2010FA0001258Distributor Blk · meltedDURING A 500 HOUR INSP, COMPLIANCE OF M/N 6314 MAGNETOS, LT MAGNETO SHOWED SIGNS OF EXTREAM HIGH HEAT INTERNALLY. SB SB3-08A ADDRESSES PROBLEM CAUSED BY "SOFT" CARBON BRUSHES PACKAGED FROM SEPT 1, 2004 THROUGH AUGUST 14, 2008. TT OF MAGNETO WAS DOCUMENTED AS Dec 20, 2010 · N710MD · Cirrus SR20 · Magneto/DistributorSDR 2010FA0001132Spring · brokenON LANDING TAILSPRING BROKE. ACFT GROUND LOOPED CAUSING SUBSTANTIAL DAMAGE TO AIRCRAFT. INVESTIGATION OF BROKEN TAILSPRING REVEALED 2 EXISTING LOW CYCLE FATIGUE FRACTURES AND 1 OVERSTRESS POINT. MFG SUGGESTS REPLACING WITH A BOLT IN REDESIGNED UNIT.Aug 21, 2010 · N123TA · Amtr DR107 · Nose/Tail Landing GearSDR ZB0R20100002Master Switch · burned((ZB0R)) PILOT REPORTED BURNING SMELL AND FAILURE OF AVIONICS BUSS NR 2 ON RUN-UP. ACFT REPORTED TO MX. TROUBLESHOOTING REVEALED AVIONICS MASTER SWITCH RT SIDE (BUSS 2) ARCING INTERNALLY. REPLACED AVIONICS SWITCH AND OPS CK OK.May 31, 2010 · N963AC · Cessna 172S · DC Power Distribution SystemSDR 2010FA0000425Guide · broken(HE8S) PILOT`S SEAT HARNESS GUIDE BROKE AT SHOULDER HARNESS MOUNT TUBE. SUGGEST MAKING THIS PART WITH MORE DURABLE MATERIAL OR HAVING A REINFORCEMENT AT AREA OF BREAKAGE. THE BROKEN PART HAS A STRESS AREA WHERE IT WAS BROKEN DUE TO THE HOLE WHERE HEAD REST MApr 19, 2010 · N55SV · Cessna 172S · Flight Compartment EquipmentSDR 2010FA0000228Mount · brokenHAVE HAD MULTIPLE PROBLEMS WITH THE MOUNTING KIT FOR THE ALTERNATOR THROUGH STC SA334SW. A NEW ALTERNATOR WAS INSTALLED ON 9/8/2006. AFTER 64 FLIGHT HOURS, THE ALUMINUM MOUNTING BLOCK BROKE DURING FLIGHT ON 6/5/07, AND WAS REPLACED ON 6/13/07. AFTER 127 FLIMar 12, 2010 · N35LA · Mooney M20F · DC Generator-AlternatorSDR 2010FA0000196Solenoid · sticksBURNED ODOR OF ELECTRICAL COMPONENTS AFTER ENGINE START UP. SELECTED ACFT MASTER SWITCH OFF AND SHUTDOWN ENGINE. INSP REVEALED STARTER MOTOR HAD OVERHEATED. FURTHER EXAMINATION REVEALED STARTER SOLENOID HAD STUCK IN THE CLOSED POSITION DURING ENGINE START AMar 3, 2010 · N7884N · Cessna 172E · Engine StarterSDR 2010FA0000045Track · brokenPN 1513055-1 CAM TRACK ASSY BROKE UPON GEAR RETRACTION. NOSE GEAR THEN WOULD NOT RETRACT PROPERLY OR EXTEND AND LOCK PROPERLY. PUMP MOTOR C/B CONTINUED TO TRIP DURING THE FLIGHT. ACFT WAS LANDED WITHOUT INCIDENT. IT WAS NOTICED THAT THE NOSE GEAR WAS COCKEJan 15, 2010 · N1871M · Cessna 337G · Landing Gear Retraction/Extension SystemSDR 2009FA0000986Shaft · fracturedROTOR SHAFT FRACTURED AT THE BOTTOM OF THE RUBBING BROOK SLOT. (K)Nov 20, 2009 · N96EV · Amtr RV6A · Magneto/DistributorSDR 2009FA0000873Nut · crackedWHEN REMOVING PROPELLER FOR RESEAL, FOUND 2 MOUNTING NUTS CRACKED. THE PROP HAS 93.5 HRS SINCE INSTALLATION. THE PROPELLER PREVIOUSLY HAD THE BLADES REPLACED DUE TO PROP STRIKE.Oct 22, 2009 · N722PA · Diamon DA40 · Propeller SystemSDR 2009FA0000921Screen · crackedREPAIR STATION IS HOLDER OF STC SA03674AT FOR THE INSTALATION OF R-134 COOLANT AIR CONDITIONER SYS IN THIS ACFT. IAW THIS STC INSTALLATION, A CONDENSER HOUSING IS MOUNTED ON THE BOTTOM OF THE ACFT FUSELAGE. IT HAS BEEN DISCOVERED THAT THE SCREEN WHICH COVERSAug 14, 2009 · N908DS · Diamon DA40 · Engine Air Intake SystemSDR 2009FA0000922Screen · crackedREPAIR STATION IS HOLDER OF STC SA03674AT FOR THE INSTALATION OF R-134 COOLANT AIR CONDITIONER SYS IN THIS ACFT. IAW THIS STC INSTALLATION, A CONDENSER HOUSING IS MOUNTED ON THE BOTTOM OF THE ACFT FUSELAGE. IT HAS BEEN DISCOVERED THAT THE SCREEN WHICH COVERSAug 14, 2009 · N385DS · Diamon DA40 · Cabin Cooling SystemSDR 2009FA0000510Air Filter · defectiveUPON RECEIVING INSP OF NEW MFG AIR FILTERS PN P107336 IT WAS FOUND THAT 3 OUT OF 4 NEW FILTERS HAD A DEFECTIVE SEALING SURFACE CAUSING THE SEALING/MATING SURFACE TO CRACK AND CRUMBLE. THIS DEFECTIVE SEALING SURFACE COULD POTENTIALY ENTER THE ENGINE INLET. THE Jun 9, 2009 · N1244S · Cessna 337H · Engine Fuel and ControlSDR 2009FA0000449Control Cable · brokenAN INSP OF RT WING FLAP CABLE REVEALED BROKEN STRANDS WHERE THE CABLE THIMBLE AND SHACKLE TO THE FLAP BELLCRANK INSIDE THE WING. THERE IS INSUFFICIENT CLEARANCE BETWEEN THE CABLE AS IT WRAPS AROUND THE THIMBLE AND THE BELLCRANK AND IT WAS GETTING PINCHED WHENMay 12, 2009 · N62045 · Maule M5210C · Trailing Edge Flap Control SystemSDR 2009FA0000396Plunger · damagedPLUNGER P/N 210332 INSPECTED IAW SB 33571C AND FAILED.May 11, 2009 · N286DS · Diamon DA40 · Propeller GovernorSDR 2008FA0000841Latch · disengagedAT 10500 FT IN CRUISE FLIGHT, GOT AN AUDIBLE "DING" ON THE G1000 WARNING AND THEN A LIGHT SAYING THAT A DOOR WAS OPEN. BACK DOOR HAD COME OPEN IN FLIGHT. THE DOOR HAD BEEN SHUT AND THERE HAD BEEN NO WARNING DURING PRE-FLIGHT CHECK AND RUN-UP. WAS IN THE RT SNov 24, 2008 · N661DS · Diamon DA40 · Passenger/Crew DoorsSDR 2008FA0000880Sensor · defectiveSENSOR PRODUCED A FALSE HIGH OIL PRESSURE INDICATION DURING ACFT APPROACH TO AIRPORT. PROBABLE CAUSE WAS INTERNAL FAILURE, RECOMMENDATIONS TO PREVENT RECURRENCE ARE UNAVAILABLE, AS THE FREQUENCY OF THIS TYPE OF OCCURRENCE HAS BEEN VERY LOW.Nov 22, 2008 · N212LV · Cirrus SR20 · Engine Oil PressureSDR 2010FA0000758Wire · chafed(NU7R) PILOT REPORTED AVIONICS INTERMITTENT TO COME ON WITH AVIONICS SWITCH. MFG DWG PAGE 24-50-01, PAGE 1 SHOWS AVIONICS RELAY NR 1 WITH WIRE CSVA661-14 LEAVING THE RELAY GOING TO THE AVIONICS ESSENTIAL BUSS. THIS WIRE WAS CHAFING ON THE BOTTOM HINGE ATTACHNov 7, 2008 · N893CD · Cirrus SR20 · Electrical Power System WiringSDR CA081009009Wire · broken(CAN) A+ TERMINAL MELTED OFF ALTERNATOR AND LOOSE. PROBLEM CAUSED BY BROKEN TERMINAL ON A+ WIRE GOING TO ALTERNATOR. WIRE WAS ORIGINALLY VERY TIGHT CAUSING THE BREAKAGE, THEN IT ARCED CAUSING HEAT AND EVENTUAL FAILURE.Sep 27, 2008 · Diamon DA40 · Electrical Power System WiringSDR 2008FA0000661Casting · brokenCUSTOMER ATTEMPTED TO START ENGINE. WHILE CRANKING ENGINE, CUSTOMER REPORTED A LOUD "CLUNK" AND THE PROPELLER STOPPED ROTATING. INVESTIGATED PROBLEM AND FOUND THE STARTER DRIVE CASTING BROKE FROM STARTER MOTOR. THE CASTING INCLUDED A BEARING FOR THE STARTER DRSep 17, 2008 · N273DS · Diamon DA40 · Engine StarterSDR 2008FA0000505Connector · damagedON JUNE 28TH, 2008, DURING CLIMB OUT, PASSING THROUGH 4000 FEET THE ENGINE SUDDENLY WENT INTO AN OVER SPEED CONDITION OF OVER 3100 RPM. THE AIRCRAFT REMAINED UNDER CONTROL AND WAS LANDED SAFELY AT AIRPORT AFTER AN EMERGENCY WAS DECLARED. UPON DISASSEMBLY OF TJul 22, 2008 · N412PJ · Diamon DA40 · Propeller/Propulsor System WiringSDR 2008FA0000278Valve · looseTHE ALTERNATE AIR VALVE IS VIBRATING AND CAUSING FRETTING BETWEEN THE INLET RING, PN D41-7166-20-31 AND FLANGE, PN D41-7166-20-33. THE "DUST" IS BEING INGESTED INTO THE FUEL CONTROL SERVO AND ENGINE. THERE NEEDS TO BE A TIGHTER FIT BETWEEN THESE PARTS.Apr 15, 2008 · N105UV · Diamon DA40 · Air Conditioning SystemSDR 2008FA0000234Valve · brokenTHE ENG AUTOMATIC ALTERNATE INDUCTION AIR VALVE THAT IS PARTIALLY LOCATED INSIDE THE CYLINDRICAL PAPER INDUCTION AIR FILTER CAME APART AND SOME OF ITS PART (2 INCH LONG, .2500 INCH DIAMETER BOLT. 2 INCH LONG SPIRAL SPRING WASHER, AND COTTER PIN) WERE INGESTEDMar 7, 2008 · N51430 · Maule M4210C · Engine Air Intake SystemSDR 2008FA0000254Servo · damagedWHILE PERFORMING A 100 HR INSP, THE TECH DISCOVERED FINE METAL PARTICLES COVERING THE THROAT AND VALVE OF THE FUEL INJECTION SERVO (2576568-1, SN 70B10709). THE SERVO WAS SENT TO A REPAIR FACILITY TO DETERMINE WHETHER OR NOT ANY OF THE METAL PARTICLES ENTEREDMar 5, 2008 · N103UV · Diamon DA40 · Engine Fuel DistributionSDR 2008FA0000238Bushing · incorrectSTATIC SYSTEM FAILED LEAK CHECK DURING 2 YEAR STATIC SYS IFR CERTIFICATION, LEAKS WERE CAUSED BY REDUCED BUSHING FAILING TO SEAL STATIC LINE SUMP. (ON BOTH SIDES, PILOT AND COPILOT). TO REPAIR THE LEAKAGE, PIPE THREAD TAPE (TEFLON TAPE) WAS USED ON THE REDUCFeb 27, 2008 · N362HE · Cirrus SR20 · Pitot/Static SystemSDR 2007FA0000711Resistor · damagedMFG FABRICATED AN IN-LINE RESISTOR FROM THE ALTERNATOR TO THE VOLTAGE REGULATOR. THE RESISTOR WAS LOCATED APPROXIMATELY 2 INCHES FROM AUX TERMINAL ON ALTERNATOR. IT WAS STRENGTHENED WITH MULTIPLE LAYERS OF HEAT-SHRINK AND TERMINAL WAS CRIMPED ON THE SOLID WIJul 10, 2007 · N187DS · Diamon DA40 · Electrical Power System WiringSDR 2007FA0000554Antenna · disconnectedWHILE IN CRUISE FLIGHT THE NR 1 GPS STOPPED RECEIVING A SIGNAL. AFTER LANDING, REMOVED THE MFD AND FOUND THE GLUE HOLDING THE VELCRO TO THE GPS ANTENNA HAD COME UNDONE. BOTH GPS ANTENNAS ARE HELD IN PLACE WITH VELCRO STRIPS AND IN THE HEAT OF SUMMER, THE GLUE Jun 28, 2007 · N5959A · Cirrus SR20 · Global Positioning SystemSDR 2007FA0000533Strut · crackedNOSE LANDING GEAR STRUT HAS A CRACK AT THE TOP. THE STRUT COMES UP TO A Y FOR MOUNT. AT THE YOKE OF THE Y IS A WELDED REINFORCEMENT, AND THE CRACK IS AT THE TOP WHERE THIS REINFORCEMENT MEETS THE LEGS OF THE Y.Jun 22, 2007 · N217JH · Cirrus SR20 · Nose/Tail Landing Gear Strut/AxleSDR AW42007F00000Nut · looseDURING THE PERFORMANCE OF A 100 HOUR INSPECTION, SLIGHT MOVEMENT OF THE HORIZONTAL STABILIZER WAS NOTED RELATIVE TO THE RT SIDE OF THE FUSELAGE. INVESTIGATION FOUND THAT THE RT FWD ATTACH BOLT NUT APPEARED TO BE SLIGHTLY LOOSE OR UNDER-TORQUED. REMOVED ATTACJun 8, 2007 · N784WW · Cessna 172R · Horizontal Stabilizer StructureSDR 2007FA0000571Bracket · failedTHE PILOT STATED NOSE GEAR COLLAPSED ON LANDING. AFTER AIRCRAFT REMOVED FROM RUNWAY AND PUT ON JACKS. THE NOSE GEAR WOULD NOT EXTEND OR RETRACT. THE GEAR WAS EXTENDED BY EMERGENCY EXTENSION. THE NOSE GEAR ALIGNER BRACKET FELL OFF THE GEAR. AGAIN THE NOSE May 31, 2007 · N56066 · Piper PA28R200 · Nose/Tail Landing GearSDR 2007FA0000577Downlock · brokenTHE LOWER LATCH HOOK WAS BROKEN OFF ALLOWING THE NOSE GEAR TO COLLAPSE. (K)May 12, 2007 · N5094S · Piper PA28R200 · Nose/Tail Landing GearSDR 2007FA0000349Spar · looseDURING AN ANNUAL INSPECTION, THE RT FLAP IB HINGE/CONTROL BRACKET WAS FOUND TO BE LOOSE. FURTHER INSPECTION REVEALED THAT THE FLAP SPAR WAS CRACKED AT THE UPPER RIVET ATTACH POINTS. THE CRACK IS 3.5 INCH LONG AND EXTENDS PAST THE RIVET HOLES IN BOTH DIRECTIOApr 1, 2007 · N9810M · Maule M4210C · Trailing Edge FlapsSDR 2007FA0000112Air Filter · twistedDURING REMOVAL OF THE AIR FILTER THE CENTER WIRE MESH SCREEN WAS FOUND TWISTED AND BENT. SOME OF THE WELDS WERE BROKEN. SCREEN DEFORMATION CAN LEAD TO UNFILTERED AIR AND FOD ENTERING THE ENGINE. APPARENT CAUSE IS EITHER OVERTORQUEING WING NUT AND/OR INSUFFIJan 8, 2007 · N758EJ · Cessna R172K · Engine Air Intake SystemSDR 2006FA0001020Line · chafedFUEL LINE CHAFED, LINE REPLACED.Oct 18, 2006 · N777ND · Cirrus SR20 · Aircraft Fuel Distribution SystemSDR 2006FA0000561Attach Bracket · crackedENGINE MOUNT ATTACHMENT BRACKET WITH CRACKS AT THE 12 AND 6 O`CLOCK POSITION. CRACKS ON IB AND OB SIDES OF THE AN960-616 WASHER. NORMAL FLIGHT CONDITIONS UNDER WHICH IT OCCURRED. POSSIBLE CAUSE AN960-616 WASHER TOO SMALL. LARGER AREA AND THICKER WASHER NEEMay 31, 2006 · N6622E · Cessna 175 · Fuselage, Powerplant Attach FittingsSDR 2006FA0000134Attach Bracket · brokenTHE AC EXPERIENCED A HARD LANDING. DURING THE LANDING THE 2 TOP ENGINE MOUNT ATTACH BRACKETS FAILED BEHIND THE FIREWALL, ALLOWING THE TOP HALF OF THE FIREWALL TO FAIL, PULLING FORWARD AND DOWN ABOUT 18 INCHES. PN 051313211 ENGINE MOUNT ATTACH BRACKET FITS ONJan 31, 2006 · N6612E · Cessna 175 · Engine Mount SectionSDR 10943282Frame · crackedFOUND CRACK APPROXIMATELY .3750 INCH IN LENGTH ON RT FRAME 20 WING ATTACH POINT.Jan 20, 2006 · N314X · Maule M5210C · Fuselage Main, StructureSDR 2005FA0001483Hinge · failedUPON INSTALLATION OF A NEW AFT CABIN DOOR SUPPORT STRUT, THE DOOR WAS CLOSED, AND THE AFT CABIN DOOR HINGE FAILED. UPON FURTHER INSPECTION, THE DOOR HINGE WAS FOUND TO HAVE BEEN DELAMINATED WHICH COULD NOT WITHSTAND THE PRESSURE OF THE NEW SUPPORT STUT. THE Oct 5, 2005 · N541DS · Diamon DA40 · Fuselage, Door HingeSDR 2005FA0001311Engine · stoppedDURING CRUISE CLIMB, PILOT REPORTED BOTH ENGINES QUIT RUNNING AND DEVERTED. DURING DECENT ENGINES CAME BACK TO LIFE. SUMPED 1 PINT EACH FROM FRONT, BACK FUEL STRAINERS, LT AND RT WING DRAINS. FUEL APPEARED NORMAL COLOR BLUE AND NO CONTAMINATES FOUND. (K)Sep 9, 2005 · N37E · Cessna P337H · Engine (Reciprocating)
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