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 M7K2008F00146Windscreen · damagedACFT STRUCK BIRD WITH LOSS OF PILOTS AND CENTER WINDSCREENS. ACFT LANDED AT FIRST PRACTICAL LANDING SPOT. A MAJOR REPAIR OF LT CANOPY FRAME AND LT CENTER FRAME HAS BEEN COMPLETED BY MFG SUBSIDIARY. PILOTS WINDSCREEN FOUND INADEQUATE TO PREVENT BIRDS PENETRANov 5, 2007 · N808MH · Urocop EC130B4 · Flight Compartment WindowsSDR 363011032007Servo · failedAIRCRAFT WAS IN STRAIGHT AND LEVEL FLIGHT 10 MINUTES FROM T/O AT 7000 FT AGL. CYCLIC STICK JUMPED TO THE STOP AT THE 3 O’CLOCK POSITION. A/C ENTERED A RT BANK (APPROX. 10 DEGREES). IMMEDIATE RECOVERY WAS MADE. FELT CONTINUOUS FEEDBACK IN THE RT QUADRANT. SLOWNov 3, 2007 · N902CF · Snias AS350B3 · Rotorcraft Servo SystemSDR M7K2008F00056Light · inoperativeSTROBE FLASH BECAME WEAKER AS THE DAYS PASSED UNTIL UNIT WOULD NO LONGER PASS STROBE INTENSITY REQUIREMENTS AND WAS REPLACED IAW A FIELD APPROVED 337BY THE INSTALLATION OF A WHEEL FLASHING LED ANTI COLLISION LIGHT ASSEMBLY AND ADAPTER BRACKET. THESE MONOBLOCK Oct 30, 2007 · N808MH · Urocop EC130B4 · Exterior LightingSDR M7K2008F00057Fitting · failedPART FOUND CRACKED DURING ROUTINE INSPECTION IAW AD2004-01-14, REQUIREMENTS AT THE 110 HOUR INTERVAL INSPECTION. A NEW PART OF THE OLD PN WAS INSTALLED. SUGGEST MFG MAKE AVAILABLE THE NEW PN IMPROVED FITTINGS THAT DO NOT HAVE THE AD REQUIREMENT TO AL EC 130B4Oct 30, 2007 · N808MH · Urocop EC130B4 · Rotorcraft Tail BoomSDR M7K2008F00058Fan · failedFAN ASSY HAD 3 BLADES MISSING CORNERS WITH 1 BLADE MISSING 40 PERCENT OF ITS DIMENSIONS. NEW FAN ASSY INSTALLED. INITIAL BLADE FAILURE SEEMED TO BE A MATERIAL FAILURE NOT CAUSED BY AN IMPACT. THIS TYPE DEFECT IS PRETTY RARE. (K)Oct 30, 2007 · N814MH · Urocop EC130B4 · Engine Oil CoolerSDR M7K2008F00059Tensioner · crackedDURING COMPRESSOR REPLACEMENT THE COMPRESSOR TENSIONING BRACKET WAS FOUND TO HAVE CRACKED ON ONE OF THE 2 ARMS AND SERVICEABLE REPLACEMENT PART INSTALLED. CLOSE EXAMINATION REVEALED THAT THE PARTS ARM SLOTS HAD BEEN WATER JETTED DURING MFG WHICH LEAVES A ROUGOct 30, 2007 · N803MH · Urocop EC130B4 · Cabin Cooling SystemSDR M7K2008F00125Support · looseDURING ROUTINE INSPECTION IT WAS NOTED THAT THE TOP OF THE FLAP DOOR WAS EXCESSIVELY LOOSE. CLOSER INSPECTION REVEALED THAT THE DOOR’S ATTACHMENT HARDWARE HAD LOOSENED ALLOWING THE FITTING TO WEAR AROUND THE SCREW AND ULTIMATELY BREAK THROUGH THE METAL FLANGEOct 30, 2007 · N812MH · Urocop EC130B4 · DoorsSDR M7K2008F00129Magnetic Seal · leakingSEAL LEAKAGE WAS NOTED TO BE INCREASING OVER TIME AND SEAL WAS CHANGED WHEN OIL BEGAN ACCUMULATING ON THE ENGINE DECK FOLLOWING A DAYS WORTH OF FLIGHTS. THIS SEAL WAS A HISTORY OF LEAK DEVELOPMENT AND USUALLY WILL BE CHANGED SEVERAL TIMES BEFORE ENGINE REACHEOct 30, 2007 · N814MH · Urocop EC130B4 · Turbine Engine Oil SystemSDR M7K2008F00138Cover · crackedTHIS PART WAS FOUND CRACKED DURING ROUTINE INSPECTION. THE CRACK ALWAYS OCCURS IN THE RADIUS OF THE LOWER IB CORNER FLANGE ALMOST ALL OF THESE SPRING COVERS WILL REQUIRE REPLACEMENT MULTIPLE TIMES WITHIN THE FIRST FEW THOUSAND FLIGHT HOURS OF THE AIRCRAFT. Oct 30, 2007 · N812MH · Urocop EC130B4 · Main Rotor SystemSDR M7K2008F00143Fitting · crackedPART FOUND CRACKED DURING ROUTINE INSP IAW AD2004-01-14/SB53A004 REQUIREMENTS AT THE 110 HOURS INTERVAL INSPECTION. A NEW PART OF THE OLD PN WAS INSTALLED. SUGGEST MFG MAKE AVAILABLE THE NEW PN IMPROVED FITTING THAT DO NOT HAVE THE AD REQUIREMENT TO ALL EC13Oct 30, 2007 · N804MH · Urocop EC130B4 · Standard Practices/StructuresSDR M7K2008F00055Switch · failedAT END OF FLIGHT, PILOT SELECTED IDLE POSITION AND ENGINE REMAINED IN THE FLIGHT POSITION AND WAS SHUTDOWN FROM FLIGHT POSITION. A FAULT CODE WAS GENERATED THA THE START STOP SWITCH WAS DEFECTIVE IN SOME MANNER. A NEW ENGINE START STOP/ON OFF SWITCH WAS INSTOct 10, 2007 · N805MH · Urocop EC130B4 · Ignition SystemSDR M7K2008F00060Potentiometer · defectiveA FAULT CODE WAS GENERATED AT ENGINE SHUTDOWN INDICATING A DEFECT WITH THE COLLECTIVE POTENTIOMETER. A NEW POTENTIOMETER WAS INSTALLED. THIS HAS BECOME A VERY COMMON PROBLEM WITH THE LATEST REPLACEMENT PARTS THAT THEY LAST MUCH LESS THAN THE 2000 HOUR SERVICOct 10, 2007 · N813MH · Urocop EC130B4 · Power LeverSDR M7K2008F00076Potentiometer · 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 HASOct 10, 2007 · N804MH · Urocop EC130B4 · Central WarningSDR M7K2008F00085Freq Adapter · failedDURING A PREFLIGHT INSPECTION PILOT, DISCOVERED ONE FREQUENCY ADAPTER WITH A 20MM CRACK IN THE ELASTOMER. MM LIMITATION IS 10MM. THIS IS A COMMON FAILURE WHICH OCCURS AT HALF LIFE OR LESS FOR THIS PART WITH A 3000 HOUR SERVICE LIFE LIMIT. THE OLDER PN ELASTOct 10, 2007 · N816MH · Urocop EC130B4 · Main Rotor HeadSDR M7K2008F00086Freq Adapter · crackedDURING SCHEDULED MAINT ONE ADAPTER OF SET OF 3 FOUND TO HAVE INTERNAL/EXTERNAL ELASTOMER CRACK EXCEEDING MM LIMITATIONS OF 10MM. THIS IS A VERY COMMON FAILURE THAT OCCURS AT HALF OR LESS OF THIS PARTS SERVICE LIFE LIMIT OF 3000 HOURS. THE OLDER PN ADAPTERS UOct 10, 2007 · N812MH · Urocop EC130B4 · Main Rotor HeadSDR M7K2008F00087Wire · damagedPILOT REPORTED NO LOW ROTOR RPM WARNING HORN (HEADSET BEEP) NR GAUGE INDICATIONS WAS NORMAL. SENSOR IS DUAL ELEMENT WITH ONE PORTION PROVIDING EACH SIGNAL FOR WARNING HORN AND NR INDICATION. INTERNAL WIRES ARE SO FINE THIS UNIT IS FAILURE PRONE, SUGGEST OPTIOct 10, 2007 · N809MH · Urocop EC130B4 · Main Rotor SystemSDR M7K2008F00089Tensioner · crackedDURING ROUTINE COMPRESSOR REMOVAL TO FACILITATE OTHER MAINTENANCE THE CRACKED TENSIONING ARM WAS DISCOVERED AND A NEW REPLACEMENT PART INSTALLED. SUSPECT METAL FATIGUE BUT THE SECOND TENSIONING ARM MAINTAINED UNIT FUNCTIONALITY HAD NO APPARENT DEFECT DEVELOPIOct 10, 2007 · N803MH · Urocop EC130B4 · Cabin Cooling SystemSDR M7K2008F00137Chip Detector · brokenFOLLOWING ENGINE INSTALLATION A GROUND RUN WAS ABORTED WHEN AN ENGINE CHIP LIGHT ILLUMINATED IN A DIM FLICKERING MANNER ON THE CWP. INVESTIGATION REVEALED THE DETECTOR END HAD BROKEN LOOSE BUT REMAINED ATTACHED BY ITS INTERNAL WIRING. CLOSE EXAMINATION REVEAOct 10, 2007 · N806MH · Urocop EC130B4 · Engine Indicating SystemSDR M7K2008F00140Potentiometer · failedA FAULT CODE WAS GENERATED AT ENGINE SHUTDOWN INDICATING A DEFECT WITH THE COLLECTIVE POTENTIOMETER. A NEW POTENTIOMETER WAS INSTALLED. THIS HAS BECOME A VERY COMMON PROBLEM WITH THE LATEST REPLACEMENT PART THAT THEY LAST MUCH LESS THAN THE 2000 HOUR SERVICEOct 10, 2007 · N805MH · Urocop EC130B4 · Rotorcraft Flight ControlSDR M7K2008F00142Freq Adapter · crackedDURING ROUTINE INSP AT THE 30 HOUR INTERVAL, A CRACK IN THE BLUE BLADE FREQ ADAPTER T/E SIDE WAS FOUND TO EXCEED THE MM LIMITATION OF 10 MM FOR CRACKS IN THE ELASTOMER. IAW MFG REQUIREMENTS ALL 3 ADAPTERS RENEWED. THIS IS A VERY COMMON FAILURE FOR A PART THAOct 10, 2007 · N803MH · Urocop EC130B4 · Main Rotor HeadSDR HCM2007F00001Unknown · unknownAT APPROX 8000 FT ALTITUDE AT CRUISE FLT, NOTICED 2 MINOR KICKS & SLIGHT YAWS APPROX 30 SECONDS APART, REVIEWED INSTRUMENTS AND GAUGES, NOTHING ABNORMAL DETECTED. FLT CONTINUED, AT 1 HOUR INTO CRUISE FLT, APPROX 100 KNOTS AIRSPEED, AC EXPERIENCED A SUBSTANTIASep 28, 2007 · N11QG · Urocop EC130B4 · Engine Fuel and ControlSDR M7K2008F00049Angle · crackedFITTING FOUND CRACKED DURING INSP. A NEW FITTING INSTALLED. (K)Sep 19, 2007 · N805MH · Urocop EC130B4 · Standard Practices/StructuresSDR M7K2008F00050Fitting · crackedFITTING FOUND CRACKED DURING POST FLIGHT INSP. A NEW FITTING MATCH DRILLED AND INSTALLED. THIS IS A COMMON DEFECT FOR THIS PART AND OCCURS MULTIPLE TIMES ON SOME AC AND NEVER ON OTHERS FOR REASONS UNKNOWN. SOME SHIMMING IS SOMETIMES REQUIRED AND IF DONE POOSep 19, 2007 · N803MH · Urocop EC130B4 · Rotorcraft Tail BoomSDR M7K2008F00051Fitting · crackedFITTING FOUND CRACKED DURING POST FLIGHT INSP. A NEW FITTING MATCH DRILLED AND INSTALLED. THIS IS A COMMON DEFECT FOR THIS PART AND OCCURS MULTIPLE TIMES ON SOME AC AND NEVER ON OTHERS FOR REASONS UNKNOWN. SOME SHIMMING IS SOMETIMES REQUIRED AND IF DONE POOSep 19, 2007 · N805MH · Urocop EC130B4 · Rotorcraft Tail BoomSDR M7K2008F00053Bearing · seizedPILOT WAS IN A HOVER TAXI WHEN AN UNUSUAL HIGH FREQUENCY VIBRATION WAS FELT IN THE AC AND PARTIAL POWER LOSS BECAME APPARENT AND AC WAS LANDED WITH A CHIP LIGHT ILLUMINATING WITHIN SECONDS OF GROUND CONTACT AND ENGINE WAS SHUTDOWN. A VERY RAPID DECAY OF NG SPESep 19, 2007 · N804MH · Urocop EC130B4 · Turbine Engine Compressor SectionSDR M7K2008F00080Blower Motor · seizedPILOT REPORTED BLOWER VERY NOISY/GROWLS IN OPERATION. CLOSER EXAMINATION REVEALED VERY ROUGH SHAFT BEARING. A NEW REPLACEMENT MOTOR WAS INSTALLED. THIS BLOWER MOTOR IS USUALLY VERY RELIABLE IF A BIT NOISY IN NORMAL OPERATION. LIKELY CAUSE IS POOR QUALITY OSep 19, 2007 · N817MH · Urocop EC130B4 · Rotorcraft Cooling Fan SystemSDR M7K2008F00088Oil Tank · leakingOIL LEAK FOUND ON DECK DURING POST FLIGHT INSP. CRACK FOUND AT OIL TANK FILLER NECK EXTERNAL WELD. THIS SIS A COMMON PROBLEM THAT OCCURS TO THIS COMPONENT AND IS AGGRAVATED BY CAP BEING INSTALLED TOO AGGRESSIVELY DURING OIL SERVICING. SUGGEST MFG IMPROVE EXSep 19, 2007 · N813MH · Urocop EC130B4 · Main Rotor GearboxSDR M7K2008F00112Potentiometer · intermittentTHIS PART IS THE POSITION INDICATOR FOR BOTH COLLECTIVE AND TAIL ROTOR FADEC CONTROL ACTIONS. IT ALMOST NEVER FAILS TOTALLY BUT GENERATES A FAILURE CODE THAT REQUIRES THEY BE REPLACED. THESE PARTS CAN LAST THOUSANDS OF HOURS OR LESS THAN FIFTY. ONLY RECENTLSep 19, 2007 · N816MH · Urocop EC130B4 · Rotorcraft Flight ControlSDR M7K2008F00113Potentiometer · intermittentTHIS PART IS THE POSITION INDICATOR FOR BOTH COLLECTIVE AND TAIL ROTOR FADEC CONTROL ACTIONS. IT ALMOST NEVER FAILS TOTALLY BUT GENERATES A FAILURE CODE THAT REQUIRES THEY BE REPLACED. THESE PARTS CAN LAST THOUSANDS OF HOURS OR LESS THAN FIFTY. ONLY RECENTLSep 19, 2007 · N813MH · Urocop EC130B4 · Rotorcraft Flight ControlSDR M7K2008F00114Potentiometer · intermittentTHIS PART IS THE POSITION INDICATOR FOR BOTH COLLECTIVE AND TAIL ROTOR FADEC CONTROL ACTIONS. IT ALMOST NEVER FAILS TOTALLY BUT GENERATES A FAILURE CODE THAT REQUIRES THEY BE REPLACED. THESE PARTS CAN LAST THOUSANDS OF HOURS OR LESS THAN FIFTY. ONLY RECENTLSep 19, 2007 · N804MH · Urocop EC130B4 · Rotorcraft Flight ControlSDR M7K2008F00115Potentiometer · intermittentTHIS PART IS THE POSITION INDICATOR FOR BOTH COLLECTIVE AND TAIL ROTOR FADEC CONTROL ACTIONS. IT ALMOST NEVER FAILS TOTALLY BUT GENERATES A FAILURE CODE THAT REQUIRES THEY BE REPLACED. THESE PARTS CAN LAST THOUSANDS OF HOURS OR LESS THAN FIFTY. ONLY RECENTLSep 19, 2007 · N804MH · Urocop EC130B4 · Rotorcraft Flight ControlSDR M7K2008F00116Hinge · crackedCRACK’S DEVELOP IN HINGE 1ST SEGMENT OF LEADING EDGE DURING NORMAL OPERATIONS, REQUIRING REPAIR OR REPLACEMENT EVERY 100 HOURS. TYPICALLY AT MINIMUM A STOP DRILL IS REQUIRED. HINGE MATERIAL IS THIN ALUMINUM AND PERHAPS A CHANGE TO THICKER GAUGE OR ALTERNATE Sep 19, 2007 · N801MH · Urocop EC130B4 · Fuselage, Door HingeSDR M7K2008F00134Bracket · crackedFOUND CRACKED DURING AIRFRAME 100/200/500 HOUR INSPECTION, BRACKET SUPPORTS, AIR INLET COOLING DUCT WHICH IS SUBJECT TO RAM AIR AND LIKELY VIBRATES CAUSING METAL OF BRACKET TO COLD WORK. THIS IS A COMMON PROBLEM WHICH OCCURS EVERY 200-300 HOURS FOR THIS COMPOSep 19, 2007 · N823MH · Urocop EC130B4 · Starter-GeneratorSDR M7K2008F00135Blade · failedIB SURFACE ADJACENT TO PITCH HORN WORN BEYOND LIMITS DUE TO "TT" STRAP FAILURE, OB LAMINATE OF 20/21 PLATES BREAKS. THIS PROBLEM OCCURS WHEN STRAPS BREAK INTO 2 PIECES AND BROKEN ENDS VIBRATES LIKE A REED, BEYOND THE HEAT SHRINK. SUGGEST MFG THICKENS OB PLATESep 19, 2007 · N814MH · Urocop EC130B4 · Tail Rotor BladesSDR M7K2008F00136Wire · brokenNR (ROTOR RPM) MAGNETIC SENSING PICKUP LOOP BROKEN CAUSING INTERMITTENT NR INDICATION FLUCTUATIONS DURING FLIGHT. PROBABLE CAUSE IS THAT WIRE AND FRAGILE COIL WIRE IS HAIR THIN. SUGGEST A STRONGER WIRE HARNESS BE USED. (K)Sep 19, 2007 · N810MH · Urocop EC130B4 · Main Rotor System WiringSDR M7K2008F00145Combustion Liner · crackedDURING ROUTINE MONITORING OF EXISTING CRACKS WHICH HAD, TO THIS TIME, REMAINED WITHIN MM LIMITATIONS FOR A REDUCED INTERVAL INSP, NO TO EXCEED 150 FLIGHT HOURS. PARALLEL CRACKS HAVE INTERSECTED WITH THE POSSIBILITY FOR A PIECE TO BREAK FREE AND BE INGESTED BYSep 19, 2007 · N816MH · Urocop EC130B4 · Turbine Engine Combustion SectionSDR M7K2008F00096Light · unknownTHIS LIGHT ASSY HAS BEEN FAIRLY RELIABLE BUT IS A LITTLE DIFFICULT TO WORK ON REQUIRING PIN EXTRACTION TOOLING TO TROUBLESHOOT OR REPLACE. THE TYPICAL FAILURE IS INSIDE THE SEALED UNIT. THE QUALITY OF CONSTRUCTION IS EXCELLENT. (K)Sep 17, 2007 · N804MH · Urocop EC130B4 · Lighting SystemSDR M7K2008F00118Seal · leakingSEAL FOUND LEAKING FUEL OVERBOARD WITH FUEL BOOST PUMP PRESSURE APPLIED. FOLLOWING STARTUP AND SHUTDOWN OF THE FUEL BOOST PUMP FUEL LEAK SLOWED BUT CONTINUED AND WAS BEYOND ALLOWABLE LIMITS OF THE MM. THIS IS A VERY COMMON PROBLEM WITH ALMOST ALL CONTROLS RESep 17, 2007 · N801MH · Urocop EC130B4 · Fuel Controlling SystemSDR M7K2008F00119Seal · leakingSEAL FOUND LEAKING FUEL OVERBOARD WITH FUEL BOOST PUMP PRESSURE APPLIED. FOLLOWING STARTUP AND SHUTDOWN OF THE FUEL BOOST PUMP FUEL LEAK SLOWED BUT CONTINUED AND WAS BEYOND ALLOWABLE LIMITS OF THE MM. THIS IS A VERY COMMON PROBLEM WITH ALMOST ALL CONTROLS RESep 17, 2007 · N822MH · Urocop EC130B4 · Fuel Controlling SystemSDR M7K2008F00122Power Supply · inoperativeTHIS ANTICOLLISION LIGHT AND POWER SUPPLY ASSY HAS PROVEN TO BE OF LOW QUALITY AS MOST FAIL WITHIN THEIR FIRST 1000 HOURS OF SERVICE AND ARE NOT REPAIRABLE IAW MFG. AS THIS UNIT IS VERY EXPENSIVE TO REPLACE WE RECOMMEND THAT THE WHEN LED FLASHING ANTI COLLISISep 17, 2007 · N813MH · Urocop EC130B4 · Exterior LightingSDR M7K2008F00123Power Supply · inoperativeTHIS ANTI-COLLISION LIGHT AND POWER SUPPLY ASSY HAS PROVEN TO BE OF LOW QUALITY AS MOST FAIL WITHIN THEIR FIRST 1000 HOURS OF SERVICE AND ARE NOT REPAIRABLE IAW MFG. AS THIS UNIT IS VERY EXPENSIVE TO REPLACE WE RECOMMEND THAT THE WHEN LED FLASHING ANTI COLLISSep 17, 2007 · N815MH · Urocop EC130B4 · Exterior LightingSDR M7K2008F00133Switch · intermittentPILOT REPORTED THAT SEVERAL SELECTIONS TO THE ENGINE START POSITION WERE REQUIRED TO GET THE ENGINE TO START. UPON CLOSER INSP IT WAS DETERMINED THAT SELECTING THE ON OR START POSITION GENTLY WITHOUT SNAPPING THE LEVER INTO THE START POSITION COULD CAUSE THE Sep 17, 2007 · N807MH · Urocop EC130B4 · Engine Starting SystemSDR 350608222007Compressor · seizedAIR CONDITIONER BELT HAD BEEN REPLACE. AC RELEASED FOR FLIGHT. AT ABOUT THE SAME TIME WE WERE TONED FOR A SCENE CALL. ABOUT 30 SECONDS AFTER TAKEOFF, SMELLED SMOKE, AIR CONDITIONER WAS TURNED OFF BUT THE SMELL OF SMOKE GOT WORSE SO A 180 TURN WAS MADE AND RETUAug 22, 2007 · N130LN · Urocop EC130B4 · Cabin Compressor SystemSDR M7K2007F00000Frame · crackedDURING ROUTINE 100 HOUR INSPECTION THE CRACK WAS FOUND UTILIZING A BRIGHT LIGHT LOOKING AFT DOWN THE TAIL BOOM INTERIOR FROM THE TAILBOOM MOUNTED BATTER ACCESS DOOR. AS VIEWED FROM THE REAR, THE CRACK WAS LOCATED AT THE 9:00 POSITION OF THE TAIL BOOM FRAME, SAug 6, 2007 · N803MH · Urocop EC130B4 · Rotorcraft Tail BoomSDR M7K2007F00001Support Fitting · damagedDURING ROUTINE POSTFLIGHT INSPECTION THE CRACK WAS FOUND VISUALLY ON THE RT LOWER SUPPORT FITTING POSITION ON THE PARTS TRAILING EDGE FACE AND FOUND TO EXTEND ALMOST 2 INCHES OR ALMOST HALF WAY ACROSS THE PART. THIS IS A COMMON FAILURE FOR THIS PART. BELIEVEAug 6, 2007 · N808MH · Urocop EC130B4 · Fuselage Main, StructureSDR M7K2007F00003Freq Adapter · crackedDURING ROUTINE POSTFLIGHT INSPECTION THE CRACK WAS FOUND VISUALLY ON THE YELLOW BLADES FREQUENCY ADAPTER ELASTOMER SURFACE TRAILING EDGE SIDE JUST BEGINNING TO EXCEED THE M LIMITATION OF 10 MM OF LENGTH. THIS IS A VERY COMMON FAILURE THAT OCCURS USUALLY BEFORAug 6, 2007 · N808MH · Urocop EC130B4 · Main Rotor HeadSDR M7K2007F00002Casting · crackedDURING ROUTINE 500 HOUR INSPECTION IT WAS DISCOVERED THAT THE CASTING AT THE AFT MOST POSITION OF THE TAILBOOM, WHICH IS THE ATTACHMENT POINT FOR THE FENESTRON (DUCTED FAN TAIL ROTOR) HAD SEVERAL CRACKS EXCEEDING 1.5 INCHES RADIATING FROM ONE POINT AT THE 3:00Jul 26, 2007 · N806MH · Urocop EC130B4 · Rotorcraft Tail BoomSDR 070207Actuator · wrong partAIRCRAFT REQUIRED EXCESSIVE LT PEDAL IN A HOVER. CHANGED TAIL ROTOR SERVO. NOTE: UNDER MODEL THERE IS NOT THE OPTION FOR EC-135 T2 AND FOR THE ENGINE THERE IS NO OPTION FOR ARRIEL 2B2. UNDER MANUFACTURE NAME FOR THE PART THERE IS NOT A LISTING FOR THE COMPANY.Jul 2, 2007 · N308ME · Urocop EC135T1 · Tail Rotor Control SystemSDR AS350B3Gearbox · warning lightMGB CHIP LIGHT CAME ON IN FLIGHT. REMOVED CHIP PLUGS FROM THE MGB AND THE MAST FOUND PARTICLES ON THE MGB PLUG LESS THAN LIMITS CALLED OUT IN AEC AS350B3 SPM 20.08.01.601 NOTHING ON THE MAST PLUG. PERFORMED 10 MIN. HOVER AND RECHECKED CHIP PLUGS IAW AEC AS350Jun 28, 2007 · N808CP · Snias AS350B3 · Main Rotor GearboxSDR FAA070628001Gearbox · making metalMGB CHIP LIGHT CAME ON IN FLIGHT. REMOVED CHIP PLUGS FROM THE MGB AND THE MAST FOUND PARTICALS ON THE MGB PLUG LESS THAN LIMITS CALLED OUT IN AEC AS350B3 SPM 20.08.01.601 NOTHING ON THE MAST PLUG.PERFORMED 10 MIN. HOVER AND RECHECKED CHIP PLUGS AS PER AEC AS35Jun 28, 2007 · N808CP · Snias AS350B3 · Main Rotor Gearbox
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