# Service difficulty reports: Honeywell LTS101-700D-2 A list on [Honeywell LTS101-700D-2](https://openairdocs.org/engine/honeywell-lts101-700d-2.md). Newest first. General aviation reporting is voluntary. Page 1 of 3 · 118 reports - [SDR 2022FA0000456](https://openairdocs.org/sdr/2022FA0000456.md): Housing · worn · Aug 18, 2022 · Engine Oil Indicating System > LTS101-700D-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 TH - [SDR CA190626013](https://openairdocs.org/sdr/CA190626013.md): Lock · broken · Jun 23, 2019 · Snias AS350B2 · Main Rotor Gearbox > (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) - [SDR 2019F00114](https://openairdocs.org/sdr/2019F00114.md): Display · malfunctioned · Jun 15, 2019 · N752CH · Snias AS350B2 · Central Display > EEMS(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 - [SDR CA190312016](https://openairdocs.org/sdr/CA190312016.md): Bearing · making metal · Mar 11, 2019 · Snias AS350BA · Tail Rotor Gearbox > (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. - [SDR CA190307005](https://openairdocs.org/sdr/CA190307005.md): Leaf Spring · cracked · Mar 6, 2019 · Snias AS350BA · Standard Practices/Structures > (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 CRACKE - [SDR CA190220031](https://openairdocs.org/sdr/CA190220031.md): Line · leaking · Jul 29, 2018 · Snias AS350B2 · Hydraulic System, Main > (CAN) HYDRAULIC LINE FOUND LEAKING THROUGH THE BRAID (TC# 20190220031) - [SDR EVCA2017111400001](https://openairdocs.org/sdr/EVCA2017111400001.md): Line · leaking · Nov 12, 2017 · N406EM · Snias AS350B2 · Aircraft Fuel Distribution System > FLIGHT CREW REPORTED A FUEL ODOR IN THE CABIN. DURING MAINTENANCE INVESTIGATION THE FUEL FILTER LINE ON THE ENGINE WAS NOTED TO BE DRIPPING FUEL. - [SDR 2017FA0000395](https://openairdocs.org/sdr/2017FA0000395.md): Turbine Wheel · failed · Jan 20, 2017 · N920EM · Snias AS350B2 · Turbine Section > DURING 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. - [SDR CA160224009](https://openairdocs.org/sdr/CA160224009.md): Gearbox · making metal · Feb 12, 2016 · Snias AS350B2 · Main Rotor Gearbox > (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. - [SDR CA151105002](https://openairdocs.org/sdr/CA151105002.md): O-Ring · cut · Nov 4, 2015 · Snias AS350BA · Engine Oil Distribution (Airframe Furnished) > (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 - [SDR CA151202011](https://openairdocs.org/sdr/CA151202011.md): Transducer · faulty · Nov 2, 2015 · Snias AS350B2 · Engine Indicating System > (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. - [SDR CA151214015](https://openairdocs.org/sdr/CA151214015.md): Bracket · cracked · Oct 28, 2015 · Snias AS350B2 · Rotorcraft Tail Boom > (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. - [SDR CA150925012](https://openairdocs.org/sdr/CA150925012.md): Hydraulic Line · leaking · Sep 22, 2015 · Snias AS350BA · Hydraulic System, Main > (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 THE - [SDR CA150925006](https://openairdocs.org/sdr/CA150925006.md): Fuel Control · faulty · Sep 21, 2015 · Snias AS350BA · Fuel Control/Turbine Engines > (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 APPROXI - [SDR CA151202012](https://openairdocs.org/sdr/CA151202012.md): Gear · failed · Sep 15, 2015 · Snias AS350B2 · Main Rotor Gearbox > (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. - [SDR CA150902007](https://openairdocs.org/sdr/CA150902007.md): Drive Shaft · damaged · Sep 2, 2015 · Snias AS350B2 · Starter-Generator > (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. - [SDR CA150727023](https://openairdocs.org/sdr/CA150727023.md): Hose · leaking · Jul 25, 2015 · Snias AS350B2 · Hydraulic System, Main > (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. - [SDR CA150813003](https://openairdocs.org/sdr/CA150813003.md): Flex Coupling · cracked · Jul 22, 2015 · Snias AS350B2 · Engine/Transmission Coupling > (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. - [SDR CA150617002](https://openairdocs.org/sdr/CA150617002.md): Hydraulic Line · blown · Jun 15, 2015 · Snias AS350B2 · Hydraulic System, Main > (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 FOLLOWING - [SDR CA150616025](https://openairdocs.org/sdr/CA150616025.md): Pump · leaking · May 25, 2015 · Snias AS350B2 · Fuel Boost Pump > (CAN) FUEL PUMP FOUND LEAKING EXCESSIVELY FROM OVERBOARD DRAIN TUBE. REQUIRED REPLACEMENT, PUMP HAD ONLY 44.8 HRS SINCE 600 HR INSPECTION. - [SDR CA150520014](https://openairdocs.org/sdr/CA150520014.md): Flex Coupling · cracked · May 19, 2015 · Snias AS350B2 · Tail Rotor Drive Shaft > (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 - [SDR CA150430006](https://openairdocs.org/sdr/CA150430006.md): Line · leaking · Apr 29, 2015 · Snias AS350B2 · Hydraulic System, Main > (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 LEAK - [SDR CA150413005](https://openairdocs.org/sdr/CA150413005.md): Shaft · sheared · Apr 11, 2015 · Snias AS350B2 · Starter-Generator > (CAN) STARTER GENERATOR SHEARED SHAFT ON INITIATION OF START. - [SDR CA150316008](https://openairdocs.org/sdr/CA150316008.md): Governor · malfunctioned · Mar 2, 2015 · Snias AS350B2 · Turbine Governor > (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 REMAINI - [SDR CA150210007](https://openairdocs.org/sdr/CA150210007.md): Encoder · failed · Feb 9, 2015 · Snias AS350B2 · Altimeter, Barometric/Encoder > (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. DURIN - [SDR CA150210006](https://openairdocs.org/sdr/CA150210006.md): Blade · delaminated · Feb 5, 2015 · Snias AS350B2 · Tail Rotor Blades > (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 INSPECTED - [SDR CA141208014](https://openairdocs.org/sdr/CA141208014.md): Angle · cracked · Dec 4, 2014 · Snias AS350B2 · Rotorcraft Tail Boom > (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. - [SDR 7EMA20140930007](https://openairdocs.org/sdr/7EMA20140930007.md): Fuel Control · leaking · Sep 28, 2014 · N406EM · Urocop AS365N3 · Fuel Control/Turbine Engines > ON 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 D - [SDR CA140818006](https://openairdocs.org/sdr/CA140818006.md): Shaft · seized · Aug 17, 2014 · Snias AS350B2 · Turbine Governor > (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 - [SDR CA140808009](https://openairdocs.org/sdr/CA140808009.md): Engine · power loss · Aug 6, 2014 · Snias AS350BA · Engine (Turbine/Turboprop) > (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 EX - [SDR CA140423013](https://openairdocs.org/sdr/CA140423013.md): Shaft · broken · Apr 22, 2014 · Snias AS350B2 · Starter-Generator > (CAN) THE STARTER GENERATOR DRIVESHAFT, BROKE INFLIGHT ILLUMINATING GENERATOR FAIL LIGHT ON CAUTION PANEL. - [SDR CA140214005](https://openairdocs.org/sdr/CA140214005.md): Starflex · debonded · Feb 14, 2014 · Snias AS350B2 · Main Rotor Head > (CAN) FOUND THE STARFLEX DEBONDED BETWEEN THE BUSHING AND THE SPINDLE. - [SDR CA131101003](https://openairdocs.org/sdr/CA131101003.md): Blade · loose · Oct 31, 2013 · Snias AS350B2 · Turbine Section > (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". - [SDR CA131023011](https://openairdocs.org/sdr/CA131023011.md): Bushing · damaged · Oct 23, 2013 · Snias AS350B2 · Tail Rotor Drive Shaft > (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 REPLA - [SDR CA131007026](https://openairdocs.org/sdr/CA131007026.md): Power Supply · failed · Oct 2, 2013 · Snias AS350BA · Exterior Lighting > (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 POWE - [SDR C3OR201309270001](https://openairdocs.org/sdr/C3OR201309270001.md): Combust Chamber · damaged · Sep 27, 2013 · Turbine Engine Combustion Section > CUSTOMER 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 PSI - [SDR CA130816003](https://openairdocs.org/sdr/CA130816003.md): Pump · leaking · Aug 14, 2013 · Snias AS350B2 · Fuel Boost Pump > (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. - [SDR CA130816002](https://openairdocs.org/sdr/CA130816002.md): Shaft · broken · Aug 13, 2013 · Snias AS350B2 · Starter-Generator > (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. - [SDR CA130814002](https://openairdocs.org/sdr/CA130814002.md): Transmitter · intermittent · Aug 12, 2013 · Snias AS350BA · Engine Oil Pressure > (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. - [SDR CA130730003](https://openairdocs.org/sdr/CA130730003.md): Pulley · failed · Jul 26, 2013 · Snias AS350B2 · Hydraulic Pump (Electric/Engine), Main > (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 WHER - [SDR CA130624004](https://openairdocs.org/sdr/CA130624004.md): Modulator · cracked · Jun 21, 2013 · Snias AS350BA · Pneumatic Distribution System > (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. - [SDR CA130525002](https://openairdocs.org/sdr/CA130525002.md): Starter Gen · failed · May 24, 2013 · Snias AS350B2 · Starter-Generator > (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 INSTA - [SDR CA130521011](https://openairdocs.org/sdr/CA130521011.md): Yoke · broken · May 16, 2013 · Snias AS350B2 · Main Rotor Head > (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. - [SDR CA130521020](https://openairdocs.org/sdr/CA130521020.md): Transmitter · failed · May 16, 2013 · Snias AS350B2 · Engine Oil Pressure > (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 TRA - [SDR CA130423001](https://openairdocs.org/sdr/CA130423001.md): Servo · stiff · Apr 21, 2013 · Snias AS350B2 · Rotorcraft Servo System > (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 T - [SDR CA130321008](https://openairdocs.org/sdr/CA130321008.md): Skin · deformed · Mar 13, 2013 · Snias AS350B2 · Rotorcraft Tail Boom > (CAN) FOUND A 2.5CM X 5CM SMOOTH DEFORMATION AT BS91 CM AT TOP LT OF TAILBOOM. SUSPECT HEAT DEFORMATION FROM ENGINE EXHAUST. - [SDR CA130306004](https://openairdocs.org/sdr/CA130306004.md): Fuel Control · disconnected · Mar 4, 2013 · Snias AS350BA · Fuel Control/Turbine Engines > (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 WA - [SDR CA130213001](https://openairdocs.org/sdr/CA130213001.md): Mount · cracked · Feb 12, 2013 · Snias AS350B2 · Hydraulic Pump (Electric/Engine), Main > (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. - [SDR CA130208006](https://openairdocs.org/sdr/CA130208006.md): Servo · seized · Feb 7, 2013 · Snias AS350B2 · Rotorcraft Servo System > (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 REMO - [SDR CA130208003](https://openairdocs.org/sdr/CA130208003.md): Hose · unserviceable · Feb 6, 2013 · Snias AS350B2 · Hydraulic System, Main > (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 CRIM Next page: https://openairdocs.org/engine/honeywell-lts101-700d-2/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/engine/honeywell-lts101-700d-2/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.