Moravan Z242L

Service difficulty reports · 189

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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 aircraft_model_key = 'Z242L'
  ORDER BY difficulty_date DESC"

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SDR CA070703002Rotor Shaft · sheared(CAN) A STUDENT PILOT NOTICED THAT THE ENGINE WOULD NOT RUN WHEN THE RT MAGNETO WAS SELECTED. MAINT WAS CALLED AND THE RT MAGNETO WAS REMOVED FROM THE ENGINE AND DISSASSEMBLED. THE ROTOR WAS FOUND SHEARED AT THE CAM ROTOR SLOT. (TC NR 20070703002)May 9, 2007 · Moravn Z242L · Magneto/DistributorSDR CA060628001Distributor Gear · broken(CAN) DURING POST REMOVAL TEARDOWN INSPECTION OF MAGNETO ELECTRODE FINGER FOUND BROKEN OFF OF THE DISTRIBUTER GEAR.Apr 11, 2006 · Moravn Z242L · Magneto/DistributorSDR CA051130006Impulse Coupling · missingAS A RESULT OF PREVIOUS MAGNETO FAILURES, IMPLEMENTED A 100 HR INSPECTION OF ALL IMPULSE COUPLED MAGNETOS ON ALL ZLIN 242L AIRCRAFT. DURING ONE OF THESE INSPECTIONS ONE OF THE IMPULSE COUPLING PAWLS HAD A SPRING MISSING. THIS SPRING ALLOWS THE PAWL TO ENGAGENov 30, 2005 · Moravn Z242L · Magneto/DistributorSDR CA050804008Control Cable · frayed(CAN) DURING A 100 HR INSPECTION THE CENTER FLAP CABLE WAS FOUND TO BE FRAYED AT THE PULLEY AREA. THE CABLE WAS REPLACED NEW. THIS IS A COMMON AREA FOR WEAR ON THESE CABLES.Jul 26, 2005 · Moravn Z242L · Trailing Edge Flap Control SystemSDR CA050804006Control Cable · frayed(CAN) DURING A 100 HR INSPECTION THE FLAP CONTROL SYSTEM CENTER CABLE WAS DISCOVERED TO BE FRAYED AT THE AREA OF THE PULLEY. THE CABLE WAS REPLACED NEW.Jun 23, 2005 · Moravn Z242L · Trailing Edge Flap Control SystemSDR CA050804005Control Cable · frayed(CAN) DURING A 100 HR INSPECTION THE FLAP CONTROL SYSTEM CENTER CABLE WAS DISCOVERED TO BE FRAYED AT THE AREA OF THE PULLEY. THE CABLE WAS REPLACED NEW.Jun 23, 2005 · Moravn Z242L · Trailing Edge Flap Control SystemSDR CA050624006Control Cable · frayedDUE TO PREVIOUS ELEVATOR TRIM CABLE FAILURES A 3000 HR REPLACEMENT INTERVAL WAS PUT INTO PLACE. THIS CABLE WAS BEING REMOVED FOR REPLACEMENT WHEN THE DEFECTS WERE FOUND. THE 3000HR INTERVAL WILL CONTINUE.Jun 16, 2005 · Moravn Z242L · Elevator Tab Control SystemSDR CA050624005Control Cable · frayedDUE TO PREVIOUS TRIM CABLE FAILURES A 3000 HR REPLACEMENT INTERVAL WAS INTRODUCED. THIS CABLE WAS BEING REMOVED FOR REPLACEMENT WHEN IT WAS FOUND TO BE FRAYED AT THE CONTROL STOP. THE 3000 HR REPLACEMENT INTERVAL WILL CONTINUE.Jun 7, 2005 · Moravn Z242L · Elevator Tab Control SystemSDR CA041215006Shaft · sheared(CAN) DURING A 100 HR INSPECTION, THE ELEVATOR TRIM CONTROL CABLE DRUM WAS NOTICED TO BE OFFSET ON AN ANGLE. FURTHER INSPECTION REVEALED THE SHAFT THAT THE DRUM IS ATTACHED TO HAD THE LT END SHEARED OFF.THE LT AND RT ENDS ARE SUPPORTED BY THE LT AND RT INBOARDec 15, 2004 · Moravn Z242L · Elevator Tab Control SystemSDR CA040831009Spring · broken(CAN) DURING TAXI A STUDENT PILOT NOTICED THAT THE AIRCRAFT WAS DIFFICULT TO STEER. IT WAS ALSO NOTICED THAT THE RUDDER PEDALS FELT DIFFERENT. MAINTENANCE WAS NOTIFIED AND IT WAS FOUND THAT THE RT STEERING SPRING WAS BROKEN. THE SPRING WAS REPLACED IAW THE Aug 31, 2004 · Moravn Z242L · Landing Gear Steering SystemSDR CA040408013Tee Fitting · separated(CAN) DURING AN ENGINE REMOVAL THE OIL DRAIN TEE FITTING WAS FOUND TO HAVE THE PICK UP TUBE LOOSE IN THE TEE FITTING. THIS PROBLEM WAS PREVIOUSLY REPORTED IN AN SDR. A MANDATORY SB WAS ISSUED FROM THE MANUFACTURER (MSBZ242L/42A) AND THE FITTINGS WERE REPAIREApr 8, 2004 · Moravn Z242L · Reciprocating Engine Oil SystemSDR CA040406005Baffle · broken(CAN) DUE TO PREVIOUS DISCOVERIES OF BROKEN INTERNAL BAFFLES INSIDE THE NR 1 EXHAUST SILENCER ON OTHER AIRCRAFT IN OUR FLEET, AN INTERNAL INSPECTION HAS BEEN CALLED UP EVERY 100 HOURS TO COINCIDE WITH A 100 HR INSPECTION. THIS PARTICULAR BAFFLE WAS FOUND BROKEApr 5, 2004 · Moravn Z242L · Engine Noise SuppressorSDR CA040319001Control Cable · frayed(CAN) DURING A 100 HOUR INSPECTION, IT WAS NOTICED THAT THE AFT TRIM CABLE HAD A BROKEN STRAND FORWARD OF THE RT PULLEY NEAR THE TRIM DRUM. THROUGH EXPERIENCE IT WAS FOUND THAT CONDITION WOULD LEAD TO A TOTAL FAILURE OF THE CABLE IN THE NEAR FUTURE. THE CABLMar 12, 2004 · Moravn Z242L · Elevator Tab Control SystemSDR CA040126007Spring · broken(CAN) DURING TAXI A STUDENT PILOT NOTICED THAT THE AIRCRAFT WOULD NOT STEER PROPERLY. MAINTENANCE NOTICED THAT THE RT STEERING SPRING WAS BROKEN. THIS HAS BEEN AN ON GOING PROBLEM WITH STUDENTS WHEN THEY TRY TO STEER THE AIRCRAFT WITHOUT GETTING THE AIRCRAFT RJan 26, 2004 · Moravn Z242L · Landing Gear Steering SystemSDR CA031201009Spring · broken(CAN) DURING A ROUTINE INSPECTION THE LT FLAP CONTROL LEVER UPLOCK SPRING WAS FOUND TO BE BROKEN. THIS SPRING KEEPS PRESSURE ON THE UPLOCK HOOK THAT HOLDS THE FLAP I N THE UP POSITION. THERE ARE ALSO SPRINGS THAT ASSIST IN KEEPING THE FLAP IN THE UP POSITIONNov 26, 2003 · Moravn Z242L · Trailing Edge Flap Control SystemSDR CA031009001Impulse Coupling · loose(CAN) DUE TO PREVIOUS IMPULSE COUPLING FAILURES, THE MAGNETO IMPULSE COUPLING IS INSPECTED EVERY 100 HOURS OF OPERATION.THIS MAGNETO WAS REMOVED FOR A 500 HOUR INSPECTION AND THE HUB WAS FOUND TO BE VERY LOOSE.THIS COUPLING HAD ONLY 93.1 HOURS TSN.Oct 6, 2003 · Moravn Z242L · Magneto/DistributorSDR CA030730005Cable · broken(CAN) AS A RESULT OF PREVIOUS FRAYED CABLES, SPECIAL ATTENTION IS PAID TO AREAS WHERE THE ELEVATOR TRIM CABLE PASSES THROUGH PULLEYS, CABLE DRUMS. THIS CABLE HAD BROKEN STRANDS WHERE IT PASSED THOUGH THE LT AFT PULLEY. A REPLACEMENT INTERVAL OF THESE CABLES Jul 29, 2003 · Moravn Z242L · Elevator Tab Control SystemSDR CA030619006Cable · broken(CAN) WHILE TAXIING AN AIRCRAFT THE STUDENT PILOT NOTICED THAT THE NOSE WHEEL STEERING WAS NOT RESPONDING WITH TURNS TO THE RT. MAINTENANCE WAS NOTIFIED AND IT WAS FOUND THAT THE RT NOSE GEAR STEERING CABLE WAS BROKEN AT THE AFT END OF THE CABLE WHERE THE ATTJun 16, 2003 · Moravn Z242L · Landing Gear Steering SystemSDR CA030626006Camshaft · worn(CAN) THE ENGINE WAS SENT IN FOR CAMSHAFT CHANGE DUE TO CAMSHAFT FAILURE. THE CAMSHAFT WAS FOUND TO HAVE SEVERE WEAR ON THE NR 1 & 2 INTAKE LOBE. REPLACED WITH A FACTORY NEW CAMSHAFT.Jun 13, 2003 · Moravn Z242L · Reciprocating Engine Power SectionSDR CA030626003Camshaft · spalled(CAN) THE ENGINE WAS SENT IN FOR A PROP STRIKE INSPECTION. AFTER DISASSEMBLY THE CAMSHAFT WAS FOUND TO HAVE AN UNACCEPTABLE AMOUNT OF SPALLING ON THE NR 1 EXHAUST LOBE AND ON BOTH INTAKE LOBES. THE CAM AND LIFTERS WERE REPLACED WITH A MFG FACTORY NEW KIT.Jun 13, 2003 · Moravn Z242L · Reciprocating Engine Power SectionSDR CA030626005Camshaft · spalled(CAN) THE ENGINE WAS SENT FOR INSPECTION DUE TO METAL CONTAMINATION. AFTER DISASSEMBLY THE CAMSHAFT WAS FOUND TO HAVE SPALLING ON ALL THE LOBES, THE INTAKE LOBES BEING THE WORST. THIS SPALLING WAS THE CAUSE OF THE METAL CONTAMINATION. THE CAMSHAFT WAS REPLACEDJun 12, 2003 · Moravn Z242L · Reciprocating Engine Power SectionSDR CA030626007Camshaft · spalled(CAN) THE ENGINE WAS SENT IN FOR INSPECTION DUE TO METAL CONTAMINATION. TWO PROBLEMS WERE DISCOVERED. FIRST, THE CONNETING ROD CAPS WERE CONTACTING THE OPPOSING PISTON SKIRTS, THE CAPS WERE FOUND TO BE APPROXIMATELY .020 THICKER THAN SEVERAL OTHERS MEASURED. TJun 12, 2003 · Moravn Z242L · Reciprocating Engine Power SectionSDR CA030526001Baffle · broken(CAN) DUE TO FINDING A BROKEN INTERNAL BAFFLE INSIDE THE NR 1 EXHAUST SILENCER, WE INITIATED AN INTERNAL INSPECTION OF THE SILENCER EVERY 100 HR INSPECTION INTERVAL. THIS BAFFLE WAS FOUND TO BE COMPLETELY BROKEN. THE EXHAUST SILENCER WAS REPLACED WITH A REPAIMay 23, 2003 · Moravn Z242L · Engine Noise SuppressorSDR CA030521001Rivet · loose(CAN) DURING A 100 HR INSPECTION, AND DUE TO PREVIOUS IMPULSE COUPLING FAILURES, THE LT MAGNETO IS REMOVED AND THE IMPULSE COUPLING IS INSPECTED EVERY 100 HOURS. THIS IMPULSE COUPLING HAD A LOOSE RIVET ON ONE OF THE LATCHING PAWLS AND THE POSSIBILITY OF THE RMay 15, 2003 · Moravn Z242L · Magneto/DistributorSDR CA030508004Rivet · loose(CAN) DUE TO OTHER IMPULSE COUPLING FAILURES, AT EVERY 100 HR INSPECTION, THE LT MAGNETO IS REMOVED AND THE IMPULSE COUPLING IS INSPECTED. THIS IMPULSE COUPLING HAD A LOOSE RIVET THAT HOLDS ONE OF THE PAWLS IN PLACE. HAD THE RIVET FAILED THE PAWL WOULD CONTAMMay 8, 2003 · Moravn Z242L · Magneto/DistributorSDR CA030325005Rivet · loose(CAN) DUE TO PREVIOUS IMPULSE COUPLING FAILURES, WE HAVE IMPLEMENTED AN INSPECTION OF THE IMPULSE COUPLING EVERY 100 HOURS. THIS IMPULSE COUPLING HAD A LOOSE RIVET ON ONE OF THE PAWLS. IF THE RIVET WAS TO SHEAR THERE WOULD BE SIGNIFICANT DAMAGE TO THE ENGINE.Mar 14, 2003 · Moravn Z242L · Magneto/DistributorSDR CA030305001Impulse Coupling · loose(CAN) AS A RESULT OF PREVIOUS IMPULSE COUPLING FAILURES, WE IMPLEMENTED AN IMPULSE COUPLING INSPECTION EVERY 100 HRS. UPON INSPECTION OF THIS IMPULSE COUPLING WE FOUND THE HUB VERY LOOSE, BOTH PAWL RIVETS LOOSE, AND THE PAWL GAPS EXCEEDED THE MAXIMUM ALLOWED BMar 4, 2003 · Moravn Z242L · Magneto/DistributorSDR CA030305002Impulse Coupling · loose(CAN) DUE TO PREVIOUS IMPULSE COUPLING FAILURES, WE IMPLEMENTED AN IMPULSE COUPLING INSPECTION EVERY 100 HRS. THIS IMPULSE COUPLING WAS FOUND TO HAVE A LOOSE PAWL RIVET. SLICK SB1-98 WAS CARRIED OUT AND THE PAWL GAPS WERE FOUND TO BE WITHIN LIMITS, AND THE T-Feb 27, 2003 · Moravn Z242L · Magneto/DistributorSDR CA030116004Seal · blown(CAN) FRONT CRANKSHAFT SEAL BLOWN OUT DUE TO FROZEN ENGINE VENT LINE CANISTER. VENT SYSTEM PURGED AND CLEANED CRANKSHAFT SEAL RESEATED. ENGINE RUN-UP AND OIL FILTERS SERVICEABLE (NO METAL).Dec 24, 2002 · Moravn Z242L · Reciprocating Engine Power SectionSDR 2002FA0001233Valve · erodedOIL DRAIN VALVE WAS REMOVED BECAUSE OF LEAK, UPON REMOVAL IT WAS DISCOVERED THAT SMALL NUT HOLDING SLUDGE VALVE ASSY TOGETHER WAS WORE TO MIN AMOUNT AND MISSING ONE HALF, IF NUT HAD COME OFF VALVE ASSY WOULD OPEN CAUSING ENGINE OIL TO COMPLETLY DRAIN.Oct 28, 2002 · N242MC · Moravn Z242L · Engine Oil Storage (Airframe Furnished)SDR CA020910007Control Cable · broken(CAN) ON TAXI THE AIRCRAFT WOULD ONLY TURN IN ONE DIRECTION. IT WAS FOUND THAT THE RT STEERING CABLE HAD BROKEN AT THE FWD END AT THE LOOP AROUND THE BOLT. THE CABLE WAS REPLACED AND THE STEERING SPRING GAP WAS SET. ALL OTHER CABLES ON THE FLEET OF Z242L Sep 9, 2002 · Moravn Z242L · Landing Gear Steering SystemSDR CA020904012Bearing · worn(CAN) T57006 PROPELLER REMOVED AT SCHEDULED 100 HOUR INSPECTION. DURING ROTATION OF PROP BY HAND AN OBJECT COULD BE HEARD TUMBLING AROUND INSIDE HUB. NOTE THAT JUST PRIOR TO REMOVAL OF THE PROP A REPORT WAS RECEIVED STATING THAT THE PROPELLER WOULD NOT RETAIN Aug 28, 2002 · Moravn Z242L · Propeller Hub SectionSDR CA020904011Rivet · loose(CAN) AFTER TWO COMPLETE IMPULSE COUPLING FAILURES WHICH RESULTED IN THE ENGINES BEING REMOVED FOR REPAIR, IT WAS DECIDED THAT AT EVERY 100 HOUR INSPECTION THE LT MAGNETO WOULD BE REMOVED AND THE IMPULSE COUPLING INSPECTED. ON THIS IMPULSE COUPLING ONE PAWL RAug 20, 2002 · Moravn Z242L · Magneto/DistributorSDR CA020830021Spring · broken(CAN) DURING TAXI, A STUDENT NOTICED PLAY IN THE NOSE WHEEL STEERING OF THE AIRCRAFT. MAINTENANCE WAS NOTIFIED AND THE LT STEERING SPRING WAS FOUND TO BE BROKEN. THE SPRING WAS REPLACED USING THE MINIMUM COIL DISTANCE SETTING ON THE LT AND RT STEERING SPRINJul 30, 2002 · Moravn Z242L · Landing Gear Steering SystemSDR CA020731003Muffler · cracked(CAN) DURING A FIRST 100 HOUR INSPECTION ON A NEW AIRCRAFT, THE NR 3 CYLINDER EXHAUST PIPE WAS FOUND TO BE CRACKED WHERE IT IS WELDED TO THE MUFFLER. THE CRACK WAS APPROXIMATELY 1.5 INCHES LONG AROUND THE CIRCUMFERENCE OF THE PIPE. THIS PIPE HAS A STRUT ATTACHJul 23, 2002 · Moravn Z242L · Engine Noise SuppressorSDR CA020729007Impulse Coupling · loose(CAN) WHILE INSPECTING A MAGNETO, THE IMPULSE COUPLING WAS REMOVED, INSPECTED AND WAS FOUND TO HAVE A LOOSE FIT BETWEEN THE IMPULSE PAWL MOUNTING PLATES AND THE IMPULSE HUB. DUE TO TWO PREVIOUS CATASTROPHIC FAILURES OF IMPULSE COUPLINGS. THE IMPULSE COUPLINGJul 16, 2002 · Moravn Z242L · Magneto/DistributorSDR CA020626008Booster · failed(CAN) DURING A PRE-FLIGHT RUN-UP THE AIRCRAFT ENGINE LT MAGNETO DROP WAS 600 RPM. TROUBLESHOOTING SHOWED THAT THE CAUSE WAS A FAULT WITH THE SLICK-START MEGNETO BOOSTER. THE BOOSTER WAS REPLACED AND THE ENGINE GROUND RUN. THE MAGENTO DROPS WERE WITHIN LIMITS.Jun 19, 2002 · Moravn Z242L · Magneto/DistributorSDR CA020626006Control Cable · frayed(CAN) AS A RESULT OF THE DISCOVERY OF AN ALMOST COMPLETELY FAILED ELEVATOR TRIM CONTROL CABLE ON ANOTHER AIRCRAFT AND BROKEN WIRES IN A SECOND AIRCRAFT'S CABLE, THIS AIRCRAFT'S ELEVATOR TRIM CONTROL SYSTEM WAS INSPECTED TO DETEMINE THE CONDITION OF THE CABLES.Jun 19, 2002 · Moravn Z242L · Elevator Tab Control SystemSDR CA020626007Booster · failed(CAN) DURING A PRE-FLIGHT RUN-UP THE AIRCRAFT ENGINE LT MAGNETO DROP WAS 600 RPM. TROUBLESHOOTING SHOWED THAT THE CAUSE WAS A FAULT WITH THE SLICK-START MAGNETO BOOSTER. THE BOOSTER WAS REPLACED AND THE ENGINE GROUND RUN. THE MAGNETO DROPS WERE WITHIN LIMITS.Jun 18, 2002 · Moravn Z242L · Magneto/DistributorSDR CA020508004Spring · broken(CAN) UPON TAXI A STUDENT PILOT NOTICED AN EXCESSIVE AMOUNT OF PLAY IN THE NOSE STEERING SYSTEM. MAINTENANCE WAS NOTIFIED AND THE RT STEERING SPRING WAS FOUND TO BE BROKEN. THE SPRING WASREPLACED USING THE MINIMUM SPACING FOR PRELOAD TENSION. STUDENT REMINDED Apr 23, 2002 · Moravn Z242L · Landing Gear Steering SystemSDR CA020508003Spring · broken(CAN) UPON TAXI A STUDENT PILOT NOTICED AN EXCESSIVE AMOUNT OF PLAY IN THE NOSE STEERING SYSTEM. MAINTENANCE WAS NOTIFIED AND THE RT STEERING SPRING WAS FOUND TO BE BROKEN. THE SPRING WAS REPLACED USING THE MINIMUM SPACING FOR PRELOAD TENSION. STUDENT REMINDEDApr 22, 2002 · Moravn Z242L · Landing Gear Steering SystemSDR CA020507022Spring · broken(CAN) A STUDENT PILOT REPORTED TO MAINTENANCE THAT ON A GROUND RUN OF THE AIRCRAFT THAT THE PROPELLER WOULD NOT CYCLE WHEN THE CONTROL WAS PULLED OUT TO PUT THE PROP INTO COARSE PITCH. INVESTIGATION FOUND THAT THE PROP CONTROL FLAT SPRINGS THAT HOLD THE PROP CApr 21, 2002 · Moravn Z242L · Propeller Controlling SystemSDR CA020508005Spring · broken(CAN) UPON TAXI A STUDENT PILOT NOTICED AN EXCESSIVE AMOUNT OF PLAY IN THE NOSE STEERING SYSTEM. MAINTENANCE WAS NOTIFIED AND THE LT STEERING SPRING WAS FOUND TO BE BROKEN. THE SPRING WAS REPLACED USING THE MINIMUM SPACING FOR PRELOAD TENSION. STUDENTS WERE ONApr 19, 2002 · Moravn Z242L · Landing Gear Steering SystemSDR CA020502005Impulse Coupling · failed(CAN) THE LT MAGNETO FAILED DURING ENGINE START UP. MAGNETO IMPULSE COUPLING HAD COME APART AND LOOSE PIECES FROM COUPLING CAUSED MAJOR DAMAGE TO MAGNETO AND ENGINE. ENGINE REPLACED AND A/C RETURNED TO SERVICE.Apr 5, 2002 · Moravn Z242L · Magneto/DistributorSDR CA020501013Impulse Coupling · worn(CAN) AS A RESULT OF 2 RECENT CATASTROPHIC MAGNETO IMPULSE COUPLING FAILURES ON OTHER AIRCRAFT IN OUR FLEET THAT RESULTED IN ENGINES BEING REPLACED, THIS MAGNETO WAS REMOVED AND INSPECTED FOR CONDITION OF THE IMPULSE COUPLING. ONE OF THE TWO PAWLS AND IT'S ATTApr 1, 2002 · Moravn Z242L · Magneto/DistributorSDR CA020501014Impulse Coupling · broken(CAN) DURING AN ENGINE START, AN UNUSUAL NOISE WAS HEARD COMING FROM THE ENGINE. INVESTIGATION BY MAINTENANCE PERSONNEL REVEALED THAT THE LT MAGNETO HAD FAILED AND THAT IT'S IMPULSE COUPLING HAD COME APART. THE PARTS MISSING FROM THE IMPULSE COUPLING ENTERED IMar 28, 2002 · Moravn Z242L · Magneto/DistributorSDR CA020408009Strut · broken(CAN) DURING A 100 HOUR INSPECTION THE EXHAUST STAY STRUT WAS FOUND BROKEN AT THE THREADED PART OF THE EYE END. A NEW STRUT AND EYE END ASSEMBLY WAS INSTALLED AND POSITIONED FOR PROPER FIT. THIS EYE END IS SECURED BY THE UPPER RIGHT HAND NUT THAT ALSO SECURES Mar 19, 2002 · Moravn Z242L · Engine Collector/Tailpipe/NozzleSDR CA020408008Spring · broken(CAN) A STUDENT PILOT REPORTED EXCESSIVE MOVEMENT IN THE NOSE GEAR STEERING SYSTEM. A MAINTENANCE CHECK REVEALED THAT THE LT NOSE GEAR STEERING SPRING WAS BROKEN. THE SPRING WAS REPLACED USING THE MINIMUM COIL DISTANCE SETTING ON THE L/H & R/H SPRINGS. THE PROMar 18, 2002 · Moravn Z242L · Landing Gear Steering SystemSDR 2001FA0000608Support · brokenEYE SCREW, IS A SUPPORT STRUT WHICH ATTACHES TO THE EXHUST STACK AT ONE END AND THE FUEL SERVO TO ENGINE SUMP ATTACHMENT STUDS AT THE OTHER END. THE STRUT FELL BETWEEN THE THROTTLE ARM AND SUMP. THIS PREVENTED THE ENGINE FROM BEING ABLE TO REDUCE POWER BELOW 1Dec 6, 2001 · N147FS · Moravn Z242L · Aircraft Fuel Distribution SystemSDR CA011217018Camshaft · worn(CAN) DURING SCHEDULED 50 HOUR INSPECTION THAT CONTAINED TASKS REQUIRED TO COMPLY WITH THE ENGINE ON THE CONDITIONS PROGRAM ESTABLISHED FOR THE ENGINE BEING INSPECTED, A MODERATE AMOUNT OF VERY SMALL METAL PARTICLES WERE FOUND IN THE OIL FILTER ELEMENT DURING Nov 30, 2001 · Moravn Z242L · Reciprocating Engine Power Section
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