Honeywell LTS101-700D-2

Service difficulty reports · 118

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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 = 'LTS101700D2'
  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 2022FA0000456Housing · wornLTS101-700D-2 ENGINE SN LE49043C WAS SMOKING SLIGHTLY FOR SOME TIME (POST HSI AT AIRWORK ON WO-123264), THIS WAS COMMUNICATED TO US BY THE CUSTOMER (SYDNEY HELICOPTERS). THE CUSTOMER HAS NOW FLOWN 427.4 HOURS. A FIELD JOB WAS ARRANGED (WO-127965) TO RECTIFY THAug 18, 2022 · Engine Oil Indicating SystemSDR CA190626013Lock · broken(CAN) AFTER TAKE OFF MGB CHIP LIGHT ILLUMINATED, PILOT RETURNED TO LANDING PAD, CHIP PLUGS WERE INSPECTED, MAST CHIP DETECTOR WAS BROKEN OFF. (TC# 20190626013)Jun 23, 2019 · Snias AS350B2 · Main Rotor GearboxSDR 2019F00114Display · malfunctionedEEMS(ELECTRONIC ENGINE MANAGEMENT SCREEN) FROZE ON START AT 12% NG, SCREENS GO INTO REVERSONARY MODE (FAILURE MODE) AND WILL NOT COME OUT OR FUNCTION. THIS CONTINUES ON SUBSEQUENT START ATTEMPTS. SYSTEM OPERATING SYSTEM MUST BE REFORMATTED AND LOADED MANUALLY Jun 15, 2019 · N752CH · Snias AS350B2 · Central DisplaySDR CA190312016Bearing · making metal(CAN) GEARBOX GENERATING METAL FLAKE. GEARBOX REPAIRED BY ORIGINAL EQUIPMENT MANUFACTURER WITHIN 8 HOURS. GEARBOX REMOVED AND RETURNED TO ORIGINAL EQUIPMENT MANUFACTURER COMPONENT SHOP FOR FURTHER INVESTIGATION AND REPAIR.Mar 11, 2019 · Snias AS350BA · Tail Rotor GearboxSDR CA190307005Leaf Spring · cracked(CAN) WHILE CREW WAS LOWERING FORWARD BELLY COWLING, INSIDE THE HANGAR, A LOUD BANG OCCURRED AND THE COWLING WAS PULLED OUT OF THEIR HANDS. THE RIGHT HAND ANTI-VIBRATION WEIGHT ASSEMBLY FELL ON THE FLOOR. UPON FURTHER INSPECTION A LEAF WAS FOUND TO HAVE CRACKEMar 6, 2019 · Snias AS350BA · Standard Practices/StructuresSDR CA190220031Line · leaking(CAN) HYDRAULIC LINE FOUND LEAKING THROUGH THE BRAID (TC# 20190220031)Jul 29, 2018 · Snias AS350B2 · Hydraulic System, MainSDR EVCA2017111400001Line · leakingFLIGHT CREW REPORTED A FUEL ODOR IN THE CABIN. DURING MAINTENANCE INVESTIGATION THE FUEL FILTER LINE ON THE ENGINE WAS NOTED TO BE DRIPPING FUEL.Nov 12, 2017 · N406EM · Snias AS350B2 · Aircraft Fuel Distribution SystemSDR 2017FA0000395Turbine Wheel · failedDURING THE PRE PURCHASE INSPECTION, AN ISSUE WITH THE ENGINE WAS FOUND. DURING THE INSPECTION, IT WAS DISCOVERED THAT THE PT ROTOR HAD FOUR RIVETS THAT HAD FAILED AT THE BASE OF THE BLADE SHANK.Jan 20, 2017 · N920EM · Snias AS350B2 · Turbine SectionSDR CA160224009Gearbox · making metal(CAN) METAL CONTAMINATION ON CHIP PLUG, ONLY 181.6 HRS SINCE O/H, GEARBOX ALMOST SEIZED ON WARM. NOTE: OIL PUMP IS PART OF THE MGB WHICH WAS O/H AT THE SAME TIME AS THE GEARBOX. THE MGB WILL BE SENT FOR A COMPLETE TEAR DOWN FOR A COMPLETED REPORT ANALYSIS. Feb 12, 2016 · Snias AS350B2 · Main Rotor GearboxSDR CA151105002O-Ring · cut(CAN) ACFT HAD A CHIP INDICATION IN FLIGHT, THE PILOTS LANDED AT THE COMPANY BASE. THE ENGINEERS INVESTIGATED AND FOUND MINOR FUZZ ON THE ADC SCAVENGE OIL FILTER CHIP PLUG. THE CHIP PLUG WAS CLEANED AND THE ACFT RETURNED TO SERVICE IAW MM. THE ACFT WENT OUT Nov 4, 2015 · Snias AS350BA · Engine Oil Distribution (Airframe Furnished)SDR CA151202011Transducer · faulty(CAN) NEW PRESSURE TRANSDUCER INDICATED 4 BARS AT INSTALLATION WITH ACFT POWER ON, ACFT NOT RUNNING. REJECTED PART INSTALLED ANOTHER NEW PART SYS FUNCTION TESTED SERVICEABLE.Nov 2, 2015 · Snias AS350B2 · Engine Indicating SystemSDR CA151214015Bracket · cracked(CAN) CRACK ON TAILBOOM FROM TAIL ROTOR GEARBOX COWLING BRACKET. CRACK STARTED FROM 1 OF THE RIVET HOLES THAT HOLDS THE BRACKET ONTO THE TAILBOOM.Oct 28, 2015 · Snias AS350B2 · Rotorcraft Tail BoomSDR CA150925012Hydraulic Line · leaking(CAN) PILOT NOTICED THE LINE WAS LEAKING AT THE LOWER END, THE ENGINEER ORIGINALLY SUSPECTED THE B-NUT AND TIGHTENED THE LINE. THIS DID NOT STOP THE LEAK SO THE ENGINEER HAD A MORE DETAILED LOOK AT THE LINE AND FOUND THE HYDRAULIC FLUID WAS COMING OUT OF THESep 22, 2015 · Snias AS350BA · Hydraulic System, MainSDR CA150925006Fuel Control · faulty(CAN) ACFT WAS STARTED FOR A COMPANY FLIGHT. DURING RUN UP CHECKS, THE EOS, ELECTRONIC OVERSPEED SENSOR, CHECK WAS COMPLETED SATISFACTORILY. HOWEVER, UPON RETURNING THE EOS SWITCH TO THE OFF, NORMAL, POSITION, THE ENGINE AND NR SPEEDS RAPIDLY SURGED TO APPROXISep 21, 2015 · Snias AS350BA · Fuel Control/Turbine EnginesSDR CA151202012Gear · failed(CAN) ACFT ENCOUNTERED CHIP LIGHT, LANDED CLEANED CHIP PLUG IAW AMM GROUND RUN AND TEST FLIGHT C/O CHIP LIGHT ILLUMINATED AGAIN. ACFT LANDED TRANSMISSION SENT FOR REPAIR. UPON REPAIR FOUND EPICYCLIC TO HAVE LARGE AMOUNTS OF DAMAGE. PARTS SCRAPPED.Sep 15, 2015 · Snias AS350B2 · Main Rotor GearboxSDR CA150902007Drive Shaft · damaged(CAN) STARTER WAS SENT IN FOR 900 HR O/H WITH THE DRIVESHAFT FAILING NDT FOR FLAWS AT THE SHEAR POINT. THIS ACFT IS MODIFIED IAW STC SR01647SE TO INSTALL ENGINE.Sep 2, 2015 · Snias AS350B2 · Starter-GeneratorSDR CA150727023Hose · leaking(CAN) DURING LAST FLIGHT OF THE DAY INSPECTION FOUND HYDRAULIC FLUID ON TRANSMISSION DECK. FAULT HOSE FOUND TO BE CAUSE, REPLACED HOSE WITH SERVICEABLE LINE.Jul 25, 2015 · Snias AS350B2 · Hydraulic System, MainSDR CA150813003Flex Coupling · cracked(CAN) DURING SHUTDOWN, ROTORS TURNING LOUD CLICKING HEARD FROM COUPLING WHILE ROTORS WERE SLOWING DOWN. COUPLING FOUND CRACKED IN 3 PLACES ALL AROUND, AND GOING THROUGH THE CRIMPED BUSHINGS OF THE OUTER DISK.Jul 22, 2015 · Snias AS350B2 · Engine/Transmission CouplingSDR CA150617002Hydraulic Line · blown(CAN) MECHANIC FOUND DURING HELICOPTER TURN AROUND THAT THERE WAS HYD FLUID ON TAIL BOOM. AFTER INVESTIGATION FOUND HYD HOSE PN 704A34-412-271A WAS BLEW UP & THAT THE HYD TANK WAS ALMOST EMPTY, WHICH WILL HAVE CERTAINLY LEAD TO AN HYD FAILURE ON THE FOLLOWINGJun 15, 2015 · Snias AS350B2 · Hydraulic System, MainSDR CA150616025Pump · leaking(CAN) FUEL PUMP FOUND LEAKING EXCESSIVELY FROM OVERBOARD DRAIN TUBE. REQUIRED REPLACEMENT, PUMP HAD ONLY 44.8 HRS SINCE 600 HR INSPECTION.May 25, 2015 · Snias AS350B2 · Fuel Boost PumpSDR CA150520014Flex Coupling · cracked(CAN) DURING POST FLIGHT INSPECTION, FOUND FWD FLEX COUPLING BETWEEN ENGINE AND TRANSMISSION CRACKED ON DRIVE SHAFT SIDE OF COUPLING, WHILE REMOVING FLEX COUPLING, THE 3 BOLTS THAT ATTACH THE COUPLING TO THE BELT DRIVE PULLEY WERE FOUND SLIGHTLY LOOSE. DRIVE May 19, 2015 · Snias AS350B2 · Tail Rotor Drive ShaftSDR CA150430006Line · leaking(CAN) ACFT JUST CAME OUT OF INSPECTION. IT HAD ALL HYDRAULIC LINES REPLACED FOR 6 YEAR REPLACEMENT. ACFT WAS GROUND RUN AND LEAK CHECKED SERVICEABLE. ACFT DEPARTED A DAY LATER, AFTER ARRIVING PILOT DID A POST FLIGHT INSPECTION AND FOUND HYDRAULIC FLUID LEAKApr 29, 2015 · Snias AS350B2 · Hydraulic System, MainSDR CA150413005Shaft · sheared(CAN) STARTER GENERATOR SHEARED SHAFT ON INITIATION OF START.Apr 11, 2015 · Snias AS350B2 · Starter-GeneratorSDR CA150316008Governor · malfunctioned(CAN) ENGINE CYCLED WHILE IN FLIGHT, MOMENTARELY LOST POWER. WHILE HOVERING, NG SPOOLED BACK UP 40 FT ABOVE TREES, LANDED IN CLEAR AREA. GOVERNOR WAS REPLACED AS A PRECAUTIONARY MEASURE, STIFFER THAN NORMAL LEVEL TRAVEL, PN 4-301-289-05 WITH LOW TIME REMAINIMar 2, 2015 · Snias AS350B2 · Turbine GovernorSDR CA150210007Encoder · failed(CAN) DURING FLIGHT A BURNING ODOR WAS NOTICED WITH NO VISUAL SMOKE. THE PILOT DECIDED TO RETURN TO BASE FOR INVESTIGATION ON THE WAY THE TRANSPONDER/ENCODER CIRCUIT BREAKER TRIPPED THE PILOT CHOSE NOT TO RESET THE BREAKER AND LANDED SAFELY AT THE BASE. DURINFeb 9, 2015 · Snias AS350B2 · Altimeter, Barometric/EncoderSDR CA150210006Blade · delaminated(CAN) AFTER 7 DAYS OF SITTING OUTSIDE IN THE RAIN THE ACFT WAS STARTED UP FOR REPOSITIONING. ONCE THE ACFT WAS AT FLIGHT IDLE, A AIRFRAME VIBRATION WAS FELT & THE TAKEOFF WAS ABORTED & THE ENG WAS SHUT DOWN. UPON INSPECTION THE TAIL ROTOR BLADE WAS INSPECTEDFeb 5, 2015 · Snias AS350B2 · Tail Rotor BladesSDR CA141208014Angle · cracked(CAN) INSPECTION BEING CARRIED OUT IAW EASB: 05.00.70 CRACKS WERE NOTED RADIATING FROM THE NR 7 BOLT HOLE IN REINFORCEMENT BRACKET. ANGLE TO BE REPLACED.Dec 4, 2014 · Snias AS350B2 · Rotorcraft Tail BoomSDR 7EMA20140930007Fuel Control · leakingON DAILY INSPECTION TECHNICIAN NOTICED FUEL PUMP LEAKING AT ENG MATING. UPON PUMP REMOVAL DISCOVERED FUEL CONTROL DRIVE BEARING BLUE GREASE LUBRICATION EXCESSIVELY WASHED OUT OF DRIVE. MM STATES IN 72-00-00 PAGE 7 OVERBOARD FUEL PUMP LEAKAGE MAY BE UP TO 4 DSep 28, 2014 · N406EM · Urocop AS365N3 · Fuel Control/Turbine EnginesSDR CA140818006Shaft · seized(CAN) ENGINE FLAME OUT ON TAKEOFF. INVESTIGATION OF THE PROBLEM WAS DONE AND FOUND THAT THE GOVERNOR SHAFT IS SEIZED. THE BEARING WAS REPLACE ON THIS UNIT 335 HRS. THIS UNIT HAD SOME REPAIR DONE TO IT AT TSO 1338.8 HRS, BACK IN OCTOBER 23 2013 . TIME SINCE Aug 17, 2014 · Snias AS350B2 · Turbine GovernorSDR CA140808009Engine · power loss(CAN) ON DEPARTURE, AT AN ELEVATION OF 900FT AGL PILOT NOTICED LOSS OF POWER AND SUBSEQUENT LOW ROTOR HORN ALARM. PILOT ENTERED AUTO-ROTATION, A/C LANDED WITH MINOR DAMAGE AND NO INJURY TO THE PILOT. PLUMES OF WHITE SMOKE WERE SEEN BY WITNESSES COMING FROM EXAug 6, 2014 · Snias AS350BA · Engine (Turbine/Turboprop)SDR CA140423013Shaft · broken(CAN) THE STARTER GENERATOR DRIVESHAFT, BROKE INFLIGHT ILLUMINATING GENERATOR FAIL LIGHT ON CAUTION PANEL.Apr 22, 2014 · Snias AS350B2 · Starter-GeneratorSDR CA140214005Starflex · debonded(CAN) FOUND THE STARFLEX DEBONDED BETWEEN THE BUSHING AND THE SPINDLE.Feb 14, 2014 · Snias AS350B2 · Main Rotor HeadSDR CA131101003Blade · loose(CAN) DURING AN 1800 HRS INSPECTION, PT ROTOR BLADE RETAINING RIVETS WERE FOUND LOOSE IN EXCESS OF PRESCRIBED LIMITS. LIMIT IS 0.010" AND A NUMBER WERE FOUND AT .011".Oct 31, 2013 · Snias AS350B2 · Turbine SectionSDR CA131023011Bushing · damaged(CAN) DURING A 100 HRS SCHEDULED INSPECTION, 1 OF THE TAIL ROTOR DRIVESHAFT, REAR SECTION OUTER BEARING BUSHING WAS FOUND WITH OVERHEAT DAMAGED CAUSED BY THE HOT ENGINE GASES, TO THE POINT WERE THE RUBBER MELTED AGAINST THE DRIVE SHAFT FAIRING. PART WAS REPLAOct 23, 2013 · Snias AS350B2 · Tail Rotor Drive ShaftSDR CA131007026Power Supply · failed(CAN) THE STROBE LIGHT WAS NOTED AS BEING INTERMITTENT BY THE PILOT. UPON INVESTIGATION THE STROBE POWER SUPPLY HAD FAILED INTERNALLY. THE CIRCUIT BOARD APPEARS TO HAVE CAUGHT IN FIRE. THE WIRING TO THE STROBE LIGHT WAS INSPECTED FOR DAMAGE AND A NEW POWEOct 2, 2013 · Snias AS350BA · Exterior LightingSDR C3OR201309270001Combust Chamber · damagedCUSTOMER REPORTED VIBRATION, CLUTCH SLIPPING AND OIL IN TAIL PIPE. INCOMING DELTA P JUST BELOW LIMIT 21.7 PERCENT, 2.6 PSI. R & R, NO FAULT FOUND, PERFORMED ANOTHER DELTA P, FOUND ABNORMALLY LOW, 40 PERCENT NORMAL FOR DRY RBSH, WITH ANOTHER GAGE SET 3.7 PSISep 27, 2013 · Turbine Engine Combustion SectionSDR CA130816003Pump · leaking(CAN) DURING AFTER LAST FLIGHT INSPECTION, FUEL IS FOUND LEAKING BELOW THE FUEL TANK. INSPECTION SHOWS THAT THE RT FUEL PUMP IS LEAKING AT THE IMPELLER AREA, DRAIN HOLE, PUMP REPLACED.Aug 14, 2013 · Snias AS350B2 · Fuel Boost PumpSDR CA130816002Shaft · broken(CAN) WHEN THE PILOT PRESSED THE START BUTTON, THE NG STAYED AT ZERO, BUT THE STARTER WAS TURNING. SHAFT DISCOVERED BROKEN AT THE SHEAR POINT.Aug 13, 2013 · Snias AS350B2 · Starter-GeneratorSDR CA130814002Transmitter · intermittent(CAN) ENGINE OIL PRESSURE GAUGE WAS INTERMITTENT. RESISTANCE CHECK OF TRANSMITTER FOUND IT TO BE OPEN CIRCUIT. REMOVED TRANSMITTER CASE TO FIND THAT INTERNAL WIRE WAS MISROUTED CAUSING IT TO BE PINCHED AND EVENTUALLY CUT THROUGH. TRANSMITTER REPLACED.Aug 12, 2013 · Snias AS350BA · Engine Oil PressureSDR CA130730003Pulley · failed(CAN) ON A DAILY INSPECTION AFTER A DAY OF FLYING THE ENGINEER ON THE MACHINE NOTICED SUBSTANTIAL PLAY ON THE HYDRAULIC PUMP DRIVE PULLEY. HE DISSASEMBLED THE UNIT TO FIND THAT THE INNER RACE OF THE BEARING HAD COMPLETELY WORN AWAY THE AREA OF THE PULLEY WHERJul 26, 2013 · Snias AS350B2 · Hydraulic Pump (Electric/Engine), MainSDR CA130624004Modulator · cracked(CAN) WHILE PERFORMING A 100 HRS INSPECTION, IT WAS NOTICED THAT THE BOTTOM ATTACHMENT ARM ON THE AIRFLOW MODULATOR WAS CRACKED. ONCE THE UNIT WAS REMOVED, THE ARM BROKE OFF WITH FINGER FORCE ONLY.Jun 21, 2013 · Snias AS350BA · Pneumatic Distribution SystemSDR CA130525002Starter Gen · failed(CAN) REPORTED UPON START UP A LOAD NOISE COMING FROM ENGINE AREA. START UP ABORTED. UPON INSPECTION IT WAS FOUND TO HAVE LOST THE COOLING FAN. NUT HAD BACKED OFF AND THE FAN HAD COME OFF AND DAMAGED THE SPLINES AND THREADS. A REPLACEMENT STARTER WAS INSTAMay 24, 2013 · Snias AS350B2 · Starter-GeneratorSDR CA130521011Yoke · broken(CAN) DURING 100 HR INSPECTION, 1 OF THE 3 DROOP RING RETAINING YOKES FOUND BROKEN BUT STILL KEPT IN PLACE BY THE CLAMP. NO OTHER DAMAGE. PART REPLACED BY A NEW ONE.May 16, 2013 · Snias AS350B2 · Main Rotor HeadSDR CA130521020Transmitter · failed(CAN) LOSS OF ENGINE OIL PRESSURE ON ACFT ENGINE INSTRUMENTS IN FLIGHT. EACH INCIDENT WAS RECTIFIED BY REPLACEMENT OF OIL PRESSURE TRANSMITTER WHICH IS AN AIRFRAME PART SUPPLIED BY MFG. WE INSTALLED THE FIRST NEW TRANSMITTER IT LASTED 39.7 HRS, THE SECOND TRAMay 16, 2013 · Snias AS350B2 · Engine Oil PressureSDR CA130423001Servo · stiff(CAN) DURING ENGINE START THE PILOT IN COMMAND & MECHANIC OBSERVE THE TAIL ROTOR LT PEDAL MOVING TO FULL DEFLECTION WITHOUT INPUT. THE PIC DID RESTRICTED THE UNCOMMANDED MOVEMENT OF THE LT PEDAL BY APPLYING FORCE. THE PIC DID MENTIONED TO THE MECHANIC THAT TApr 21, 2013 · Snias AS350B2 · Rotorcraft Servo SystemSDR CA130321008Skin · deformed(CAN) FOUND A 2.5CM X 5CM SMOOTH DEFORMATION AT BS91 CM AT TOP LT OF TAILBOOM. SUSPECT HEAT DEFORMATION FROM ENGINE EXHAUST.Mar 13, 2013 · Snias AS350B2 · Rotorcraft Tail BoomSDR CA130306004Fuel Control · disconnected(CAN) FUEL LEVER WAS DISCONNECTED AT LINKAGE. LEVER POSITIONED IN OPEN POSITION DURING RIGGING REQUIREMENTS. LINKAGE RECONNECTED. AT NO TIME WAS THE FUEL SYSTEM FUEL LINES OPENED. THE NEXT ENGINE START ATTEMPT RESULTED IN FAILED START ATTEMPT. THE SYSTEM WAMar 4, 2013 · Snias AS350BA · Fuel Control/Turbine EnginesSDR CA130213001Mount · cracked(CAN) DURING A 12 YEARS AIFRAME INSPECTION, THE HYDRAULIC PUMP MOUNT WAS FOUND CRACKED TO ONE OF THE MOUNTING BOLT HOLE. PART WAS MFG IN 03/04.Feb 12, 2013 · Snias AS350B2 · Hydraulic Pump (Electric/Engine), MainSDR CA130208006Servo · seized(CAN) DURING START SEQUENCE THE TAIL ROTOR PEDAL MOVED AND SEIZED IN FULL LT CONFIGURATION. THE PILOT ACTUATED THE HYDRAULIC TEST SWITCH AND THE TAIL ROTOR PEDAL DID RETURN TO NEUTRAL POSITION. A MECHANIC WAS DISPACTH TO THE ACFT AND WITH THE HELP OF A REMOFeb 7, 2013 · Snias AS350B2 · Rotorcraft Servo SystemSDR CA130208003Hose · unserviceable(CAN) HYD FLUID LOSS WAS DISCOVERED ON DAILY INSPECTION. HYD FLUID WAS NOTICED COMING FROM THE HYD PRESSURE LINE, LT SERVO TO EPICYCLIC JUNCTION, WHERE THE BRAIDED PORTION OF THE LINE IS CRIMPED TO THE FITTING. FLUID LEAKING OBSERVED AT BOTH ENDS OF THE CRIMFeb 6, 2013 · Snias AS350B2 · Hydraulic System, Main
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