Turbomeca ARRIEL-1E2

Service difficulty reports · 163

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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 engine_model_key = 'ARRIEL1E2'
  ORDER BY difficulty_date DESC"

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SDR O84A2014101400161Unknown · odorON LEVEL OFF AND INTO CRUISE FLIGHT, MED CREW DETECTED A STRONG FUEL ODOR IN CABIN. ODOR THEN SPREAD TO COCKPIT. FLIGHT ABORTED AND RETURNED TO PAD. ACFT INSPECTED FOR FUEL LEAKS NONE FOUND. TOOK TWO ATTEMPTS TO START NR 2 ENGINE AND ODOR IS BELIEVED TO BEOct 14, 2014 · N140SF · Bolkms BK117C2 · Air Distribution SystemSDR HDNA2014092600160Actuator · failedDUPLEX CYCLIC TRIM ACTUATOR FAILED INFLIGHT CAUSING UNWANTED FORCE TO CONTROLS.Sep 25, 2014 · N474LF · Bolkms BK117C2 · Rotorcraft Flight ControlSDR QMLA2014091014108Shaft · damagedUPON REMOVAL OF TAIL ROTOR SHAFT FROM GEAR BOX, FOUND METAL PARTICLES INSIDE CASING & EXCESSIVE WEAR ON END SHAFT SPLINES. EROSION IS APPROX .090 FORM END INWARD & .030 DEEP.Sep 10, 2014 · N145HN · Bolkms BK117C2 · Tail Rotor GearboxSDR QMLA2014090414105Gearbox · crackedPILOT REPORTED OIL RESIDUE ON TAIL ROTOR GEARBOX & SCRATCH ON LEADING SIDE NEAR LT BOLT AFTER FLIGHT. MECHANIC INSPECTED & FOUND CRACK AFT OF LT AFT BOLT & TAIL ROTOR GEARBOX 1/4 QT LOW ON OIL.Sep 4, 2014 · N145HN · Bolkms BK117C2 · Tail Rotor GearboxSDR O84A2014082700149Engine · power lossBRIEFLY BEFORE ENTERING CRUISE FLIGHT, BOTH ENGINE CAD DISPLAYS SHOWED ENG PA DIS. ALSO ROTOR RPM DROPPED TO THE POINT OF WP LIGHT AND HORN. PILOT LOWERD POWER AND ATTEMPTED TO BEEP UP RPM. LOWERING POWER BROUGHT UP ROTOR RPM. AFTER CONSULTING CHECKLIST FOAug 24, 2014 · N440SF · Bolkms BK117C2 · Engine (Turbine/Turboprop)SDR QMLA2014043014048Transmitter · defectiveDURING TAKEOFF FROM LANDING ZONE THE NR 1 SYS MGB OIL PRESS DROPPED TO .4 BAR, BELOW NORMAL RANGE. THERE WERE NO CHIPS DETECTED OR TEMP RISE ASSOCIATED WITH THIS INDICATION. SYS NR 2 PRESS REMAINED WITHIN NORMAL LIMITS. THE FLIGHT WAS ABORTED & CONTINUED TApr 30, 2014 · N101VU · Bolkms BK117C2 · Main Rotor GearboxSDR QMLA2014042914045Actuator · leakingTHE TAIL ROTOR ACTUATOR WAS FOUND SEEPING. THIS ACTUATOR WAS IN SERVICE FOR 146 HOURS, ABOUT THE AVERAGE TIME FOR REPLACEMENT EXPERIENCED AT THIS FACILITY WITH THIS ACFT. THE LEAKAGE RATE EXCEEDS THE LIMITS SPECIFIED IN THE MBB BK117C-2 AMM IAW CH 67-34-00, Apr 29, 2014 · N145HH · Bolkms BK117C2 · Rotorcraft Servo SystemSDR 3GMA20140212002Unknown · malfunctionedTEN MINUTES INTO 1 LEG OF FLIGHT, NOTICED NR 1 & NR 2 OIL PRESS SLIGHTLY OFF. NOTED DECREASE IN OIL PRESS OF THE NR 2 ENG. AFTER 10 MINUTES PILOT ELECTED TO DIVERT FOR RUN ON LANDING. PILOT BROUGHT NR 2 ENG TO IDLE & SET UP FOR RUN ON LANDING.Feb 12, 2014 · N483LF · Bolkms BK117C2 · Engine Oil PressureSDR 3GMA20140212001Connector · dirtyEXPERIENCED LOSS OF OIL PRESS INDICATION ON NR 2 ENG IN-FLIGHT. FOLLOWED RFM FOR LOSS OF OIL PRESS INDICATION SINGLE ENG ID, SINGLE ENG EMERGENCY SHUTDOWN PERFORMED, LANDED AS SOON AS PRACTICAL AT NEAREST IMPROVED AREA FOR RUN ON LANDING. NO LIMITS EXCEEDED,Feb 11, 2014 · N483LF · Bolkms BK117C2 · Engine Indicating System WiringSDR QMLA2013101013141Valve · failedFOUND FUEL PRESSURIZING VALVE ON NR 2 ENGINE INOPERATIVE, ALLOWING TOO MUCH FUEL TO ENTER ENGINE AT START. RAW FUEL WAS BEING PUSHED THROUGH THE ENGINE ON START AND FLOWING INTO THE COWLINGS OF ACFT. IN FLIGHT THE TRAPPED FUEL WAS SEEPING OUT OF THE COWLINGSOct 10, 2013 · N145SM · Bolkms BK117C2 · Fuel Controlling SystemSDR 3GMA20130706006Gearbox · chippedTAIL ROTOR CHIP LIGHT IN FLIGHT. MADE A PRECAUTIONARY LANDING IN BASEBALL FIELD. ENROUTE TO MEDICAL SCENE CALL AND HAD TO ABORT.Jul 6, 2013 · N482LF · Bolkms BK117C2 · Tail Rotor GearboxSDR QMLA2013070513093Engine · making metalDURING A SCHEDULED ZONE INSPECTION, THE MECHANIC FOUND THE CHIP DETECTORS FOR THE NR 2 ENGINE WITH SMALL AMOUNTS OF METAL CHIPS ON ALL DETECTORS. HE THEN REMOVED THE OIL FILTER TO FIND METAL CHIPS AS WELL. AN OIL SAMPLE AND CHIPS WERE SENT TO LAB FOR TESTINGJul 5, 2013 · N854UH · Bolkms BK117C2 · Engine (Turbine/Turboprop)SDR GVNA201306180001Drain Valve · failedSTART DRAIN VALVE FAILED INTERNALLY ALLOWING FUEL TO FLOW INTO THE COMPRESSOR THROUGH THE P2 AIR LINE. FUEL BLEW OUT OF THE COMPRESSOR CASE SPLIT LINE AND IGNITED ON TOP OF THE ENGINE CAUSING THE FIRE WARNING LIGHT TO FLICKER ON AND OFF SEVERAL TIMES. PILOT Jun 14, 2013 · N452MH · Bolkms BK117C2 · Fuel Controlling SystemSDR 3GMA20130515004Tachometer · inoperativeDURING SYSTEM CHECK, AFTER STARTING NR 1 ENGINE, NO ROTOR TACH WAS INDICATED WITH ROTORS TURNING.May 15, 2013 · N481LF · Bolkms BK117C2 · Engine RPM Indicating SystemSDR QMLA2013032313042O-Ring · leakingAN ODOR OF FUEL IN THE NR 2 ENGINE COMPARTMENT, AND NOTICED THE ENGINE DECK HAD FUEL ON IT. DRIP FROM THE STARTING DRAIN VALVE DRAIN LINE. FOUND LEAK COMING FROM THE UNION BETWEEN THE STARTING DRAIN VALVE, AND IGNITION SOLENOID VALVE. FOUND O-RING HAD NOMar 23, 2013 · N145HN · Bolkms BK117C2 · Fuel Controlling SystemSDR 2013FA0000127Bolt · crackedDURING A 100HR ANNUAL INSPECTION, IT WAS NOTED ON THE VEMD THAT THERE WERE MAST MOMENT EXCEEDANCES TRAPPED. DURING A DIE PENETRANT INSPECTION OF THE SECONDARY BOLTS 3 OF 4 INSTALLED SECONDARY BOLTS HAD CRACKING IN THE THREADED PORTION OF THE BOLT.Feb 26, 2013 · N186LA · Bolkms BK117C2 · Main Rotor HeadSDR 3GMA20130215001Blade · damagedON APPROACH, ROTOR TIP IMPACTED FLAG & FLAG HOLDER MOUNTED ON INDUSTRIAL CRANE. CREW FELT MINOR LOW FREQUENCY VIBRATION. PILOT LANDED ACFT IMMEDIATELY. ON PRELIMINARY INSPECTION, MINOR DAMAGE TO ONE MAIN ROTOR BLADE END CAP WAS DISCOVERED. PILOT NOTED NO LFeb 14, 2013 · N481LF · Bolkms BK117C2 · Main Rotor BladesSDR QMLA2013012613013Unknown · unknownPILOT REPORTED AFTER TAKEOFF, GOING THROUGH TRANSITIONAL LIFT, TRIM (YAW) TRIED TO MAKE NOSE YAW RIGHT, PILOT HAD TO EXCESSIVELY FIGHT TRIM. MECHANICS HAVE CHECKED THE TAIL ROTOR CONTROL SYS, INSPECTED AND CLEANED T/R BLADE GRIPS AND PERFORMED AUTOPILOT CHECKJan 26, 2013 · N184WK · Bolkms BK117C2 · Main Rotor SystemSDR QMLA2013012413010O-Ring · pinchedPILOT REPORTED FUEL SEEPING FROM ENGINE NR 2 COWLING AND MIGRATING BACK TO RT CLAMSHELL DOOR: UPON TROUBLESHOOTING, FOUND DAMAGED O-RING AT ENGINE 2 DRAIN VALVE. THE MECHANIC R & R THE O-RING AND PERFORMED LEAK CHECK WITH NO DISCREPANCIES NOTED. THE ACFT WAJan 24, 2013 · N811LV · Bolkms BK117C1 · Engine Fuel and ControlSDR 2013FA0000076Mount Bracket · crackedON VISUAL INSPECTION FOUND CRACKED MOUNTING BRACKET.Jan 18, 2013 · N483LF · Bolkms BK117C2 · Fuselage Main, Attach FittingsSDR QMLA2013011013004Fan · shortedCREW AND PILOT SMELLED ELECTRICAL BURNING ODOR DURING FLIGHT. NORMAL LANDING COMPLETED WITHOUT INCIDENT, AND WITHOUT ANY FURTHER EMERGENCY ACTION TAKEN. MX INSPECTED ACFT, FOUND COCKPIT VENTILATION FAN SHORTING.Jan 10, 2013 · N854EC · Bolkms BK117C2 · Air Distribution FanSDR QMLA2012121012189Switch · shortedDURING TAKEOFF, SMELLED ELECTRICAL BURNING, NO SMOKE IN AIRCRAFT. RETURNED TO BASE. FOUND ODOR TO BE COMING FROM SWITCH FOR CONTROLLABLE IR SEARCHLIGHT. SWITCH IS MOUNTED IN COLLECTIVE.Dec 10, 2012 · N145DU · Bolkms BK117C2 · Exterior LightingSDR QMLA2012112612187Structure · crackedTWO CRACKS NOTED DURING PREFLIGHT INSPECTION ON THE LT HORIZONTAL STABILIZER LOWER SIDE. NO OTHER VISUAL INDICATION OF DAMAGE.Nov 26, 2012 · N911MK · Bolkms BK117C2 · Rotorcraft Tail BoomSDR QMLA2012111212180Blade · crackedAFTER REMOVAL OF BLADE FITTINGS FOR NDT, CRACK DETECTED IN GRIP AREA.Nov 12, 2012 · N779LF · Bolkms BK117C2 · Main Rotor BladesSDR QMLA2012111212181Blade · crackedAFTER REMOVAL OF BLADE FITTINGS FOR NDT, CRACK DETECTED IN GRIP AREA.Nov 12, 2012 · N779LF · Bolkms BK117C2 · Main Rotor BladesSDR QMLA2012111212182Blade · crackedAFTER REMOVAL OF BLADE FITTINGS FOR NDT, CRACK DETECTED IN GRIP AREA. TNov 12, 2012 · N779LF · Bolkms BK117C2 · Main Rotor BladesSDR QMLA2012100912170Attach Fitting · cracked90 DEG, TAIL ROTOR GEAR BOX ATTACHMENT FITTING, CRACKED ABOUT 1 CM AT OTBD TOP MOUNTING BOLT.Oct 9, 2012 · N159LM · Bolkms BK117C1 · Rotorcraft Tail BoomSDR QMLA2012100112160Belt · brokenIN FLIGHT, PILOT AND PASSENGERS DETECTED THE ODOR OF SMOKE. NO SMOKE OR EVIDENCE OF FIRE WAS VISIBLE INSIDE OR OUTSIDE THE ACFT. PILOT SHUTOFF BOTH GENERATORS AND AIR CONDITIONER IAW CHECKLIST. ACFT MADE A PRECAUTIONARY LANDING AND PERFORMED AN EMERGENCY SHUOct 1, 2012 · N145SJ · Bolkms BK117C2 · Cabin Cooling SystemSDR QMLA2012092012157Frame · crackedDURING PREFLIGHT, FOUND A CRACK APPROX ONE INCH LONG IN THE LT FRAME OF THE TAIL FIN NEAR THE CAMLOCK FASTENER RECEPTACLE BELOW THE SERVO MOUNT.Sep 20, 2012 · N145SU · Bolkms BK117C2 · Rotorcraft Tail BoomSDR QMLA2012083012143Starter Gen · malfunctionedGENERATOR DISCONNECT LIGHT CAME ON FOR THE NR 1 GENERATOR. LANDED WITHOUT INCIDENT UNDER POWER FROM BOTH ENGINES. SWAPED STARTER/GENERATOR FROM SIDE TO SIDE. FOUND ISSUED FOLLOWED GENERATOR.Aug 30, 2012 · N779LF · Bolkms BK117C2 · Starter-GeneratorSDR QMLA2012081112132Engine · making metal20 MINUTES INTO FLIGHT, THE NR 2 ENGINE CHIP LIGHT ILLUMINATED. ACTIVATED THE FUZZ BURNER FOR APPROX 1 SECOND AND THE LIGHT EXTINGUISHED. APPROX 1 SECOND LATER THE CHIP LIGHT ILLUMINATED AGAIN. ACTIVATED THE FUZZ BURNER AGAIN AND LIGHT EXTINGUISHED. APPROAug 11, 2012 · N779LF · Bolkms BK117C2 · Engine (Turbine/Turboprop)SDR QMLA2012081012128Unknown · odorIN LEVEL FLIGHT, CREW DETECTED ODOR IN AFT CABIN SPREADING FORWARD TO COCKPIT. NOT ELECTRICAL, BUT MORE OF SOMETHING GETTING VERY HOT BUT NOT QUITE BURNING. AIR CONDITIONING UNIT WAS SHUTOFF AND THE ODOR DISSIPATED. ACFT RETURNED TO BASE. MECHANIC NOTHINAug 10, 2012 · N146DU · Bolkms BK117C2 · Air Distribution SystemSDR QMLA2012070112110Chip Detector · dirtyDURING CRUISE FLIGHT, 4 MINUTES AFTER DEPARTURE TAIL ROTOR CHIP CAUTION SEGMENT ILLUMINATED. PILOT PERFORMED EMERGENCY PROCEDURE IAW FMS 9.2-15-5. TAIL ROTOR CHIP REMAINED ILLUMINATED. PILOT LANDED WITHOUT FURTHER INCIDENT, ACFT SHUTDOWN. MECHANIC REMOVED Jul 1, 2012 · N102VU · Bolkms BK117C2 · Tail Rotor GearboxSDR QMLA2012060512090Disk · damagedWHILE PERFORMING TU360 UPGRADE TO ENGINE SN 18789 FOUND THE SECOND STAGE TURBINE DISK BLADE LOCKS DISPLACED LEADING TO BLADE SHIFT. R & R MODULE 3.Jun 5, 2012 · N145SJ · Bolkms BK117C2 · Turbine SectionSDR QMLA2012060112092Fcu · out of tolerancePERFORMED ENGINE ZONE 8 INSPECTION, RUN UP AND LEAK CHECKED, AND STARTED POWER CHECK PROCEDURE. N1, N2 AND TORQUE FLUCTUATING, 1-2 PERCENT ON N1, 2-3 PERCENT ON THE TORQUE. INSPECTED P2 LINE, PERFORMED LEAK CHECKS, AS DIRECTED BY THE TECH REP AND RAN UP AGAJun 1, 2012 · N587MH · Bolkms BK117C2 · Fuel Control/Turbine EnginesSDR QMLA2012051812083Fcu · unserviceableFUEL LEAKING FROM OVERBOARD DRAIN DETECTED AFTER ENGINE SHUTDOWN FROM GROUND RUN LEAK CHECK FOR PERFORMED MX NOT ASSOCIATED WITH THIS FAILURE. TROUBLESHOOTING IAW MM REVEALED THAT THE FCU HAD FAILED, LEAKING FUEL AT A RATE WELL ABOVE THAT ALLOTED BY MFG. CONFEMay 18, 2012 · N854UH · Bolkms BK117C2 · Fuel Control/Turbine EnginesSDR QMLA2012051412081Fcu · leakingCREW MEMBER SMELLED FUEL. COULD SEE LIQUID ON THE RT REAR CLAM SHELL GLASS WINDOW. CONTINUED FLIGHT AND LANDED WITHOUT INCIDENT. AFTER LANDING, FOUND THE FUEL CAP SECURE, BUT FUEL ON NR 1 ENGINE DECK AND ON THE ACFT SKIN BELOW AND AFT OF THE ENGINE DECK. May 14, 2012 · N101VU · Bolkms BK117C2 · Fuel Control/Turbine EnginesSDR QMLA2012041212059Throttle · roughPILOT WAS PERFORMING PRE-START CHECKLIST FOR 2ND FLIGHT OF THE DAY. WHILE OPERATING NR 2 TWIST GRIP FROM "0" TO "F" NOTICED EXTREME FRICTION FROM BETWEEN "30" AND "F". MADE SEVERAL ATTEMPTS TO GO TO "F" BUT WAS CONCERNED THAT SOMETHING MAY BREAK. ACFT REMOVApr 12, 2012 · N854UH · Bolkms BK117C2 · Power LeverSDR QMLA2012032112034Engine · malfunctionedINBOUND TO THE MAIN HELIPAD WHEN THE LOW ROTOR HORN ACTIVATED WHILE AIRSPEED WAS ABOVE 55 KNOTS. DUE TO THE DECREASING AIRSPEED DURING APPROACH AND AFT CYCLIC STICK APPLICATION, AIRSPEED DROPPED BELOW 55 KNOTS & ROTOR RPM INSCREASED TO 101 PERCENT. ABORTED Mar 21, 2012 · N102VU · Bolkms BK117C2 · Engine (Turbine/Turboprop)SDR QMLA2012030312023Unknown · odorTHE PILOT DETECTED THE ODOR OF FUEL IN THE CABIN AND COCKPIT, APPROXIMATELY FOUR MINUTES INTO FLIGHT. RETURNED TO BASE. MX INSPECTED ACFT IAW THE MM 60. NO DEFECTS WERE NOTED. A MX CHECK FLIGHT WAS PERFORMED WITH NO ODOR DUPLICATED. THE ACFT WAS RETURNED Mar 3, 2012 · N811LV · Bolkms BK117C1 · Air Distribution SystemSDR QMLA2012012712014Fuel Control · leakingAFTER TAKEOFF, NOTICED FLUID ON THE HELIPAD WHERE THE HELICOPTER WAS SITTING. WHILE SETTING UP FOR FINAL APPROACH BACK TO BASE, RECEIVED COMMUNICATION THAT FLUID WAS IDENTIFIED AS JET FUEL. AFTER LANDING, NOTED FLUID COMING OUT OF NR 2 ENGINE DRAIN PORT. Jan 27, 2012 · N587M · Bolkms BK117C2 · Fuel Control/Turbine EnginesSDR QMLA2012010412001O-Ring · tornTHE PILOT REPORTED AFTER LANDING, THE NURSE IN THE AFT CABIN STATED HE SMELLED GAS FUMES. AS THE CREW WAS EXITING THE ACFT, THEY VISUALLY CONFIRMED FUEL LEAKING FROM THE NR 1 ENGINE COWLING. THE PILOT IMMEDIATELY COMPLIED WITH AN EMERGENCY SHUTDOWN OF THE ENJan 4, 2012 · N103VU · Bolkms BK117C2 · Aircraft Fuel Filter/StrainerSDR QMLA2011101811102Fuel Tank · leakingTHE MEDICAL CREW REPORTED TO THE PILOT THAT THEY SMELLED FUEL IN THE CABIN SHORTLY AFTER TAKEOFF. THE PILOT IMMEDIATELY RETURNED TO THE HELIPAD. THE MECHANIC PERFORMED AN INPSECTION OF THE FUEL SYS AND FOUND THAT THE LOWER FITTING OF THE EXPANSION TANK WAS LOct 18, 2011 · N854EC · Bolkms BK117C2 · Fuel StorageSDR QMLA2011090711104Control Tube · crackedDURING AN AIRWORTHINESS CHECK, A CRACK WAS DISCOVERED IN THE MAIN ROTOR ROTATING CONTROL TUBE ATTACHED TO THE GREEN MAIN ROTOR BLADE. THE CRACK WAS LOCATED IN THE COLLAR OF THE TUBE POSITIONED NEAREST THE BLADE, AND WAS PARALLEL TO THE LENGTH OF THE TUBE. ONCSep 7, 2011 · N745TX · Bolkms BK117C2 · Main Rotor Mast/SwashplateSDR QMLA2011052411060Fuel Control · defectiveABOUT 4 MINUTES INTO FLIGHT STRAIGHT AND LEVEL NR 1 ENGINE ROLLED BACK TO 74 PERCENT N1 UNCOMMANDED. NR1 ENGINE LOW LIGHT ILLUMINATED. PILOT CONFIRMED PCL WAS IN FULL FORWARD FLY POSITION AND ATTEMPTED TO BEEP NR1 ENGINE UP USING ENGINE TRIM SWITCH, ENGINE REMay 24, 2011 · N117UP · Bolkms BK117C1 · Fuel Control/Turbine EnginesSDR QMLA2011050611054Blade · damagedDURING THE PILOTS PRE FLIGHT, FOUND THAT THE TRIMMING SURFACE ON THE YELLOW BLADE WAS MISSING. UPON INSPECTION FOUND THE TWO RIVET HOLES, WHERE THE RIVETS HELP HOLD THE TRIMMING SURFACE TO THE BLADE, WAS IN ALMOST PERFECT CONDITION. SENT MAIN ROTOR BLADE TO AMMay 6, 2011 · N779LF · Bolkms BK117C2 · Main Rotor BladesSDR QMLA2011033011042Bearing · making metalTHE NR 2 ENGINE CHIP LIGHT ILLUMINATED ENROUTE TO A SCENE CALL. THE PILOT IMMEDIATELY ABORTED THE FLIGHT AND RETURNED TO BASE LESS THAN 3 MILES AWAY. UPON ARRIVING AT THE BASE, THE MECHANIC INSPECTED THE CHIP PLUGS AND FOUND METAL ON THE M05 MAGNETIC PLUG ANMar 30, 2011 · N117UP · Bolkms BK117C1 · Engine (Turbine/Turboprop)SDR 7KFA775LWire · chafedELECTRICAL FIRE IN FLIGHT IN THE VICINITY OF SUCTION CONTROLS AND LIQUID OXYGEN GAUGE, FLAMES, SMOKE AND FUMES IN ACFT. WHEN DISCOVERED: IN FLIGHT, CAUSE OF INCIDENT COME FROM THE 120 VOLT AC OUTLET WIRE NR XMO10B12, PN M22759/16/12 WHICH IS LOCATED ON THE LTDec 4, 2010 · N271NE · Bolkms BK117C1 · Electrical Power System WiringSDR UIEA201000233Skin · puncturedDURING JACKING OF ACFT, MX PUNCTURED AN EXISTING REPAIR DOUBLER THROUGH THE UNDERLYING SKIN, LOCATED AT SECTION 48, BS 2594 ABOVE STRINGER 42R TAIL JACK PAD AREA. PUNCTURE MEASURING 5.0 IN. LENGTH X 1.750 WIDTH. DISPOSITION WAS MADE TO PERFORM PERMANENT REPAOct 10, 2010 · N415MC · Boeing 74747UF · Fuselage Main, Plate/SkinSDR QMLA2010091810061Chip Detector · contaminatedTHE TRANSMISSION CHIP LIGHT ILLUMINATED IN CRUISE FLIGHT ON RETURN FLIGHT TO BASE. THE MECHANIC INSPECTED THE CHIP PLUGS AND FILTERS, AND FOUND A SMALL PARTICLE ON THE PLUG, AND FUZZ ON BOTH THE FILTER HOUSING AND THE FILTERS. THE MECHANIC PROCEEDED TO DRAINSep 18, 2010 · N101VU · Bolkms BK117C2 · Main Rotor Gearbox
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