Turbomeca ARRIEL-2B1

Service difficulty reports · 757

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 = 'ARRIEL2B1'
  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 M7K2008F00141Freq Adapter · crackedDURING ROUTINE INSP A CRACK IN THE YELLOW BLADES FREQUENCY ADAPTER WAS FOUND TO EXCEED THE MM 10MM LIMITATION, CRACK WAS FOUND ON THE T/E SIDE OF THE ADAPTER. (K)Apr 14, 2008 · N807MH · Urocop EC130B4 · Main Rotor HeadSDR HCM2008F00000Engine · making metalAPPROX 45 MINUTES INTO A TOUR FLIGHT, THE (ENGINE CHIP) WARNING LIGHT ILLUMINATED. PILOT PERFORMED A PRECAUTIONARY LANDING. MAINT DISPATCHED (ON SIGHT) INSP. REVEALED MANY METAL CHIPS ON THE MODULE 1 AND OIL TANK MAG PLUGS AND FULL FLOW ELECTRICAL CHIP DETEApr 11, 2008 · N11QL · Urocop EC130B4 · Engine (Turbine/Turboprop)SDR M7K2008F00052Chip Detector · contaminatedENGINE CHIP WARNING LIGHT ILLUMINATED. AN UNEVENTFUL PRECAUTIONARY LANDING TO FIRST SUITABLE SPOT PERFORMED. ALL ENGINE CHIP DETECTORS WERE INSPECTED FOR ABNORMAL METAL. ONE, NOT RECOVERABLE, HAIRLIKE SLIVER, FOUND ON THE ELECTRICITY WIRED DETECTOR WAS REMOApr 10, 2008 · N822MH · Urocop EC130B4 · Engine Indicating SystemSDR M7K2008F00102Potentiometer · defectivePILOT REPORTS HAVING AN AMBER GOVERNOR LIGHT IN FLIGHT. UPON AC SHUTDOWN, A FAILURE CODE WAS GENERATED INDICATING THE COLLECTIVE POTENTIOMETER WAS DEFECTIVE. A NEW PART WAS INSTALLED WITH NO FURTHER DEFECT REPORTED. THIS IS A RECURRING PROBLEM FOR THIS PARTMar 28, 2008 · N850MH · Urocop EC130B4 · Rotorcraft Flight ControlSDR M7K2008F00054Hinge · crackedDURING ROUTINE INSPECTION A CRACK WAS FOUND IN THE HINGE MOUNTING FLANGE RADIATING FROM THE OUTERMOST LT ATTACHMENT SCREW BORE. THIS IS A VERY COMMON FAILURE FOR THIS PART. (K)Mar 24, 2008 · N817MH · Urocop EC130B4 · Fuselage, Door HingeSDR M7K2008F00090Hinge · crackedDURING ROUTINE INSPECTION A CRACK WAS FOUND IN THE HINGE MOUNTING FLANGE RADIATING FROM THE OUTERMOST LT ATTACHMENT SCREW BORE. REMOVAL OF ATTACHMENT SCREW REVEALED THE FLANGE CORNER HAD SEPARATED FROM THE REST OF THE HINGE. THIS IS A VERY COMMON FAILURE FORMar 24, 2008 · N821MH · Urocop EC130B4 · Fuselage, Door HingeSDR M7K2008F00091Hinge · crackedDURING ROUTINE INSPECTION, A CRACK WAS FOUND IN THE HINGE MOUNTING FLANGE RADIATING FROM THE OUTERMOST LT ATTACHMENT SCREW BORE. REMOVAL OF ATTACHMENT SCREW REVEALED THE FLANGE CORNER HAD SEPARATED FROM THE REST OF THE HINGE. (K)Mar 24, 2008 · N822MH · Urocop EC130B4 · Fuselage, Door HingeSDR M7K2008F00092Tuning Unit · crackedROUTINE 100 HOUR INSPECTION REVEALED THAT HAMMER BLADE HAD CRACKED. AS THIS BLADE IS NORMALLY UNDER A 1200 FLEX PER MINUTE OPERATION IT IS EXPECTED TO WORK HARDEN OR FATIGUE OVER TIME. SUSPECT A METAL DEFECT OF SOME NATURE AS MOST OF THESE BLADES LAST MUCH LMar 24, 2008 · N848MH · Urocop EC130B4 · Main Rotor BladesSDR M7K2008F00093Blade · crackedPREFLIGHT INSPECTION REVEALED THAT HAMMER BLADE HAD CRACKED IN TWO AND THE WEIGHTS AND BLADE WERE CAPTURED BY THE CONTAINMENT BOX ASSY. AS THIS BLADE IS NORMALLY UNDER A 1200 FLEX PER MINUTE OPERATION IT IS EXPECTED TO WORK HARDEN OR FATIGUE OVER TIME. THIS Mar 24, 2008 · N848MH · Urocop EC130B4 · Main Rotor BladesSDR M7K2008F00094Bracket · crackedBRACKET FOUND CRACKED DURING ROUTINE 100 HOUR INSPECTION. (K)Mar 24, 2008 · N813MH · Urocop EC130B4 · Fuselage Main, Attach FittingsSDR M7K2008F00095Bracket · crackedFOUND CRACKED DURING ROUTINE 100 HOUR INSPECTION. THIS IS A VERY COMMON PROBLEM FOR THIS PART. SUGGEST A MORE ROBUST MATERIAL SUCH AS SS BE UTILIZED TO REDUCE THE CRACKING OR PERHAPS A MACHINED PART. (K)Mar 24, 2008 · N812MH · Urocop EC130B4 · Engine Starting SystemSDR M7K2008F00110Potentiometer · defectiveFAILURE CODE AT SHUTDOWN INDICATED A FAULT WITH THE COLLECTIVE POTENTIOMETER. INSTALLED NEW POTENTIOMETER AND NO FURTHER PROBLEM NOTED. THIS IS A VERY COMMON FAULT FOR THIS PART THAT EFFECTS THE DISPATCH RELIABILITY FOR THIS MODEL AIRCRAFT. (K)Mar 24, 2008 · N806MH · Urocop EC130B4 · Rotorcraft Flight ControlSDR M7K2008F00111Potentiometer · defectiveFAILURE CODE AT SHUTDOWN INDICATED A FAULT WITH THE COLLECTIVE POTENTIOMETER. INSTALLED NEW POTENTIOMETER AND NO FURTHER PROBLEM NOTED. THIS IS A VERY COMMON FAULT FOR THIS PART THAT EFFECTS THE DISPATCH RELIABILITY FOR THIS MODEL AIRCRAFT. (K)Mar 24, 2008 · N846MH · Urocop EC130B4 · Rotorcraft Flight ControlSDR M7K2008F00071Potentiometer · defectivePILOT REPORTS AMBER GOVERNOR LIGHT ILLUMINATED DURING FLIGHT. A FAULT CODE WAS GENERATED INDICATING THE POTENTIOMETER AS THE LIKELY DEFECTIVE UNIT. A NEW PART WAS INSTALLED AND NO FURTHER DEFECTS WERE NOTED. THIS IS A RECURRING PROBLEM FOR THIS PART THAT HASMar 3, 2008 · N847MH · Urocop EC130B4 · Central WarningSDR M7K2008F00072Potentiometer · defectivePILOT REPORTS AMBER GOVERNOR LIGHT ILLUMINATED DURING FLIGHT. A FAULT CODE WAS GENERATED INDICATING THE POTENTIOMETER AS THE LIKELY DEFECTIVE UNIT. A NEW PART WAS INSTALLED AND NO FURTHER DEFECTS WERE NOTED. THIS IS A RECURRING PROBLEM FOR THIS PART THAT HASMar 3, 2008 · N804MH · Urocop EC130B4 · Central WarningSDR M7K2008F00074Potentiometer · defectivePILOT REPORTS AMBER GOVERNOR LIGHT ILLUMINATED DURING FLIGHT. A FAULT CODE WAS GENERATED INDICATING THE POTENTIOMETER AS THE LIKELY DEFECTIVE UNIT. A NEW PART WAS INSTALLED AND NO FURTHER DEFECTS WERE NOTED. THIS IS A RECURRING PROBLEM FOR THIS PART THAT HASMar 3, 2008 · N808MH · Urocop EC130B4 · Central WarningSDR M7K2008F00075Potentiometer · defectivePILOT REPORTS AMBER GOVERNOR LIGHT ILLUMINATED DURING FLIGHT. A FAULT CODE WAS GENERATED INDICATING THE POTENTIOMETER AS THE LIKELY DEFECTIVE UNIT. A NEW PART WAS INSTALLED AND NO FURTHER DEFECTS WERE NOTED. THIS IS A RECURRING PROBLEM FOR THIS PART THAT HASMar 3, 2008 · N850MH · Urocop EC130B4 · Rotorcraft Flight ControlSDR M7K2008F00077Fitting · crackedCRACK FOUND DURING ROUTINE INSPECTION RADIATING FROM A SCREW HOLE TO THE EDGE OF THE MACHINED FLANGE AND ACROSS THE ENTIRE FLANGE. PART WAS REMOVED IN TWO PIECES. A NEW FITTING WAS MATCH DRILLED AND INSTALLED. (K)Mar 3, 2008 · N816MH · Urocop EC130B4 · Rotorcraft Tail BoomSDR M7K2008F00078Fitting · crackedCRACK FOUND DURING ROUTINE INSPECTION RADIATING FROM A SCREW HOLE TO THE EDGE OF THE MACHINED FLANGE. A NEW FITTING WAS MATCH DRILLED AND INSTALLED. (K)Mar 3, 2008 · N812MH · Urocop EC130B4 · Rotorcraft Tail BoomSDR M7K2008F00097Potentiometer · intermittentAT FULL BRIGHTNESS ADJUSTMENT ALL CONTROLLED LIGHTING FLICKERS ON AND OFF INTERMITTENTLY. REPLACEMENT WITH NEW PART CORRECTED THE DEFECT. (K)Mar 3, 2008 · N807MH · Urocop EC130B4 · Lighting SystemSDR M7K2008F00108Potentiometer · defectivePILOT REPORTED THAT WHEN ADJUSTING POWER FOR CRUISE FLIGHT THE ENGINE HAD FLUCTUATIONS WHEN PASSING THROUGH A CERTAIN COLLECTIVE POSITION THAT WERE REPEATABLE IF SELECTING THE POSITION IN QUESTION. UPON SHUTDOWN A FAULT CODE WAS GENERATED INDICATING THE COLLEMar 3, 2008 · N810MH · Urocop EC130B4 · Rotorcraft Flight ControlSDR M7K2008F00117Hinge · crackedDURING ROUTINE 100 HR INSPECTION A CRACK WAS FOUND RADIATING HORIZONTALLY FROM THE SECOND HOLE FROM THE ONE END AND ACROSS THE CORNER OF THE FIRST HOLE ON THE OPPOSITE HINGE END WITH A TOTAL SEPARATION OF THE HINGE CORNER METAL. (K)Mar 3, 2008 · N818MH · Urocop EC130B4 · Fuselage, Door HingeSDR M7K2008F00120Transmitter · intermittentPILOT REPORTED THAT THE MAIN GEARBOX LOW OIL PRESSURE WARNING LIGHT ILLUMINATED INTERMITTENTLY AT IDLE. A NEW OIL PRESSURE TRANSMITTER WAS INSTALLED AND NO FURTHER FALSE INDICATIONS NOTED. THIS SWITCH HAS A MODERATE FAILURE RATE USUALLY BY LOSING ITS LOW ENDMar 3, 2008 · N813MH · Urocop EC130B4 · Main Rotor GearboxSDR M7K2008F00121Transmitter · intermittentPILOT REPORTED THAT THE MAIN GEARBOX LOW OIL PRESSURE WARNING LIGHT ILLUMINATED INTERMITTENTLY AT IDLE. A NEW OIL PRESSURE TRANSMITTER WAS INSTALLED AND NO FURTHER FALSE INDICATIONS NOTED. THIS SWITCH HAS A MODERATE FAILURE RATE USUALLY BY LOSING ITS LOW ENDMar 3, 2008 · N807MH · Urocop EC130B4 · Main Rotor GearboxSDR M7K2008F00131Fitting · crackedDURING ROUTINE 100 HOUR INSPECTION, A CRACK WAS FOUND RADIATING ACROSS THE CORNER OF THE FIRST HOLE ON THE HINGE END WITH A TOTAL SEPARATION OF THE HINGE CORNER METAL ON THE FAIRING ATTACHMENT FLANGE. A NEW PART WAS INSTALLED IAW THE REQUIREMENTS OF AD2004-01Mar 3, 2008 · N807MH · Urocop EC130B4 · Aerodynamic FairingsSDR M7K2008F00000Latch · failedTHIS PART CALLED A SHOCK ABSORBER DEVICE BY THE MFG IS USED TO SEQUENCE THE DOOR LATCHING MECHANISM TO PREVENT DOOR CLOSURE WITH LATCH PINS EXTENDED AND IMPACTS WITH THE DOOR FRAME. IT IS MFG OF A VERY BRITTLE BRONZE TYPE MATERIAL THAT WILL CRACK WITH JUST THFeb 4, 2008 · N821MH · Urocop EC130B4 · DoorsSDR M7K2008F00002Hinge · crackedDURING ROUTINE 100 HOUR INSP, A CRACK IN THE HINGE OF THE ENGINE FAIRING WAS FOUND RADIATING FROM THE 2ND HOLE FROM ONE END OF THE HINGE WITH THE CORNER HAVING SEPARATED FROM THE HINGE FROM CRACKS EMANATING FROM THE 1ST HOLE. THIS IS A COMMON FAILURE FOR THISFeb 4, 2008 · N817MH · Urocop EC130B4 · Fuselage, Door HingeSDR M7K2008F00048Fitting · crackedCRACK FOUND DURING ROUTINE INSP RADIATING FROM A SCREW HOLE ON MOUNTING FLANGE SURFACE AND ONTO REINFORCEMENT RIB SURFACE. A NEW FITTING HAS BEEN MATCH DRILLED AND INSTALLED. (K)Jan 8, 2008 · N812MH · Urocop EC130B4 · Rotorcraft Tail BoomSDR M7K2008F00061Potentiometer · inoperativePILOT REPORTS AMBER GOVERNOR LIGHT CAME ON IN FLIGHT. NO FAULT CODE WAS GENERATED INDICATING A POTENTIOMETER DEFECT HOWEVER CIRCUMSTANCES REPORTED POINTED TO THIS. A NEW POTENTIOMETER HAS BEEN INSTALLED. PROBLEM FIXED THIS PART HAS LASTED MUCH LONGER THAN TYPIJan 8, 2008 · N807MH · Urocop EC130B4 · Central WarningSDR M7K2008F00062Potentiometer · inoperativePILOT REPORTS AMBER GOVERNOR LIGHT CAME ON IN FLIGHT. NO FAULT CODE WAS GENERATED INDICATING A POTENTIOMETER DEFECT HOWEVER CIRCUMSTANCES REPORTED POINTED TO THIS. A NEW POTENTIOMETER HAS BEEN INSTALLED. PROBLEM FIXED THIS PART HAS LASTED MUCH LONGER THAN TYPIJan 8, 2008 · N815MH · Urocop EC130B4 · Central WarningSDR M7K2008F00063Potentiometer · inoperativePILOT REPORTS AMBER GOVERNOR LIGHT CAME ON IN FLIGHT. NO FAULT CODE WAS GENERATED INDICATING A POTENTIOMETER DEFECT HOWEVER CIRCUMSTANCES REPORTED POINTED TO THIS. A NEW POTENTIOMETER HAS BEEN INSTALLED. PROBLEM FIXED THIS PART HAS LASTED MUCH LONGER THAN TYPIJan 8, 2008 · N818MH · Urocop EC130B4 · Central WarningSDR M7K2008F00064Potentiometer · failedPILOT REPORTS AMBER GOVERNOR LIGHT CAME ON IN FLIGHT. NO FAULT CODE WAS GENERATED INDICATING A POTENTIOMETER DEFECT HOWEVER CIRCUMSTANCES REPORTED POINTED TO THIS. A NEW POTENTIOMETER HAS BEEN INSTALLED. PROBLEM FIXED THIS PART HAS LASTED MUCH LONGER THAN TYPIJan 8, 2008 · N818MH · Urocop EC130B4 · Central WarningSDR M7K2008F00065Potentiometer · failedPILOT REPORTS AMBER GOVERNOR LIGHT CAME ON IN FLIGHT. NO FAULT CODE WAS GENERATED INDICATING A POTENTIOMETER DEFECT HOWEVER CIRCUMSTANCES REPORTED POINTED TO THIS. A NEW POTENTIOMETER HAS BEEN INSTALLED. PROBLEM FIXED THIS PART HAS LASTED MUCH LONGER THAN TYPIJan 8, 2008 · N808MH · Urocop EC130B4 · Central WarningSDR M7K2008F00066Potentiometer · failedPILOT REPORTS AMBER GOVERNOR LIGHT CAME ON IN FLIGHT. NO FAULT CODE WAS GENERATED INDICATING A POTENTIOMETER DEFECT HOWEVER CIRCUMSTANCES REPORTED POINTED TO THIS. A NEW POTENTIOMETER HAS BEEN INSTALLED. PROBLEM FIXED THIS PART HAS LASTED MUCH LONGER THAN TYPIJan 8, 2008 · N812MH · Urocop EC130B4 · Central WarningSDR M7K2008F00067Potentiometer · failedPILOT REPORTS AMBER GOVERNOR LIGHT CAME ON IN FLIGHT. NO FAULT CODE WAS GENERATED INDICATING A POTENTIOMETER DEFECT HOWEVER CIRCUMSTANCES REPORTED POINTED TO THIS. A NEW POTENTIOMETER HAS BEEN INSTALLED. PROBLEM FIXED THIS PART HAS LASTED MUCH LONGER THAN TYPIJan 8, 2008 · N806MH · Urocop EC130B4 · Central WarningSDR M7K2008F00068Potentiometer · failedPILOT REPORTS AMBER GOVERNOR LIGHT CAME ON IN FLIGHT. NO FAULT CODE WAS GENERATED INDICATING A POTENTIOMETER DEFECT HOWEVER CIRCUMSTANCES REPORTED POINTED TO THIS. A NEW POTENTIOMETER HAS BEEN INSTALLED. PROBLEM FIXED THIS PART HAS LASTED MUCH LONGER THAN TYPIJan 8, 2008 · N810MH · Urocop EC130B4 · Central WarningSDR M7K2008F00069Potentiometer · malfunctionedPILOT REPORTS AMBER GOVERNOR LIGHT CAME ON IN FLIGHT. NO FAULT CODE WAS GENERATED INDICATING A POTENTIOMETER DEFECT HOWEVER CIRCUMSTANCES REPORTED POINTED TO THIS. A NEW POTENTIOMETER HAS BEEN INSTALLED. PROBLEM FIXED THIS PART HAS LASTED MUCH LONGER THAN TYPIJan 8, 2008 · N810MH · Urocop EC130B4 · Fuel Controlling SystemSDR M7K2008F00070Potentiometer · failedPILOT REPORTS AMBER GOVERNOR LIGHT CAME ON IN FLIGHT. NO FAULT CODE WAS GENERATED INDICATING A POTENTIOMETER DEFECT HOWEVER CIRCUMSTANCES REPORTED POINTED TO THIS. A NEW POTENTIOMETER HAS BEEN INSTALLED. PROBLEM FIXED THIS PART HAS LASTED MUCH LONGER THAN TYPIJan 8, 2008 · N806MH · Urocop EC130B4 · Central WarningSDR HCM2007F00002Chip Detector · faultyAPPROX 1 HR AFTER TAKEOFF ON A TOUR FLIGHT, THE ENGINE CHIP LIGHT ILLUMINATED. THE PILOT MADE A PRECAUTIONARY LANDING. UPON INSPECTION BY MAINT, NO METAL WAS FOUND ON THE ENGINE ELECTRICAL CHIP PLUGS OR ON THE ENGINE MAGNETIC PLUGS. SMALL CARBON DEPOSIT WASNov 16, 2007 · N11QM · Urocop EC130B4 · Turbine Engine Accessory DriveSDR 420611112007Fire Warning · false activationSECOND OCCURRENCE OF A FALSE ENGINE FIRE WARNING ON THIS AIRCRAFT IN THE LAST THREE DAYS. ONE FLIGHT OCCURRED BETWEEN THE TWO INCIDENTS. ARRIVED AT HOSPITAL TO PICK UP PATIENT TO TRANSPORT TO ANOTHER HOSPITAL. WHEN THE TWIST GRIP WAS PLACED IN THE IDLE POSITIONov 11, 2007 · N544AM · Snias AS350B3 · Fire DetectionSDR 350611102007Unknown · unknownUPON COMPLETION OF REFUELING, PILOT AND CREW PERFORMED WALK-AROUND AND NORMAL ENGINE START. AFTER CLEARANCE FROM TOWER DEPARTED FOR A SCENE FLIGHT. TWO MILES OUT OF AIRPORT, MGB PRESSURE LIGHT STARTED TO FLICKER WITH AUDIO WARNING (GONG). WARNING LIGHT THEN INov 10, 2007 · N130LN · Urocop EC130B4 · Central WarningSDR 420611092007Warning Light · false activationPERFORMED AIRCRAFT STOPPING ENGINE ITEMS AS OUTLINED IN CHECK LIST. WHEN TWIST GRIP WAS PLACED IN THE IDLE POSITION, THE (ENG FIRE) WARNING LIGHT ON THE CWP CAME ON. CREW MEMBER OUTSIDE THE AIRCRAFT WAS ASKED IF SMOKE OR FLAMES WERE PRESENT. HE ADVISED THEY WENov 9, 2007 · N544AM · Snias AS350B3 · Fire DetectionSDR M7K2008F00105Potentiometer · defectiveAMBER GOVERNOR LIGHT ILLUMINATED IN FLIGHT AND A FAULT CODE GENERATED INDICATING FAULT WITH COLLECTIVE LEVER VALUES BEING PROVIDED BY THE POTENTIOMETER. NEW POTENTIOMETER INSTALLED WITH NO FURTHER DEFECT NOTED. SUGGEST DIFFERENT MFG OR DESIGN BE CONSIDERED ANov 5, 2007 · N824MH · Urocop EC130B4 · Rotorcraft Flight ControlSDR M7K2008F00106Potentiometer · crackedAMBER GOVERNOR LIGHT ILLUMINATED IN FLIGHT AND A FAULT CODE GENERATED INDICATING FAULT WITH COLLECTIVE LEVER VALUES BEING PROVIDED BY THE POTENTIOMETER. NEW POTENTIOMETER INSTALLED WITH NO FURTHER DEFECT NOTED. SUGGEST DIFFERENT MFG OR DESIGN BE CONSIDERED ANov 5, 2007 · N824MH · Urocop EC130B4 · Rotorcraft Flight ControlSDR M7K2008F00109Potentiometer · defectiveAC HAD SOME SUDDEN YAWING WHEN PASSING THROUGH A SPECIFIC COLLECTIVE POWER SETTING THAT WAS REPEATABLE AND INDICATED A SUDDEN CHANGE OF ENGINE TORQUE SUCH AS ONE MAY EXPERIENCE WITH COMPRESSOR STALLS. NO FAULT CODES WERE GENERATED AD THE ENGINE HAD NO OBSERVANov 5, 2007 · N815MH · Urocop EC130B4 · Rotorcraft Flight ControlSDR M7K2008F00126Handle · brokenUPON LANDING PILOT FOUND HANDLE TO BE LIMP AND FLOPPING IN THE SLIPSTREAM. DOOR HAD TO BE OPENED UTILIZING THE INSIDE HANDLE. BELLCRANK LEVER WHICH CONNECTED OUTSIDE HANDLE TO THE DOOR LATCHING MECHANISM HAD BROKEN. A NEW DOOR HANDLE ASSY WAS INSTALLED. (KNov 5, 2007 · N807MH · Urocop EC130B4 · Passenger/Crew DoorsSDR M7K2008F00127B-Nut · leakingHOSE FOUND TO BE LEAKING NOT FROM THE B-NUT BUT A THE FITTING JUNCTION WITH THE HOSE MATERIAL. NEW REPLACEMENT HOSE INSTALLED AND NO FURTHER LEAKAGE NOTED. IN 55,000 FLIGHT HOURS THIS IS THE ONLY PROBLEM WE HAVE HAD WITH THIS HOSE. LEAK WAS CONSIDERED MINORNov 5, 2007 · N816MH · Urocop EC130B4 · Turbine Engine Oil SystemSDR M7K2008F00128Switch · failedAMBER GOVERNOR LIGHT ILLUMINATED IN FLIGHT. NO FAULT CODE WAS GENERATED THAT POINTED TO THE SWITCH AS THE PROBLEM AS WOULD NORMALLY OCCUR WITH THIS TYPE OF FAILURE. NO FURTHER PROBLEMS DEVELOPED FOLLOWING THE INSTALLATION OF A NEW SWITCH. (K)Nov 5, 2007 · N802MH · Urocop EC130B4 · Engine Starting SystemSDR M7K2008F00139Fitting · crackedDURING ROUTINE PERIODIC INSPECTION THE UPPER RT FITTING WAS FOUND WITH 25 INCH CRACK ON ITS BOTTOM ATTACHMENT FLANGE AND THROUGH ONE OF THE 4 REINFORCEMENT RIBS. A NEW FITTING WAS MATCH DRILLED AND INSTALLED. THIS IS A FAIRLY COMMON DEFECT THAT OFTEN REPEATSNov 5, 2007 · N818MH · Urocop EC130B4 · Rotorcraft Tail BoomSDR M7K2008F00144Fitting · crackedFITTING FOUND CRACKED DURING POST FLIGHT INSP AND A NEW FITTING MATCH DRILLED AND INSTALLED. THIS IS A COMMON DEFECT FOR THIS PART AND OCCURS MULTIPLE TIMES ON SOME AIRCRAFT AND NEVER ON OTHER AIRCRAFT FOR REASONS UNKNOWN. SOME SHIMMING CAN BE REQUIRED AND MNov 5, 2007 · N815MH · Urocop EC130B4 · Rotorcraft Tail Boom
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