# Honeywell LTS101-700D-2 - Type: Engine model (FAA registry) - Registry code: 33825 - Manufacturer (registry): HONEYWELL - Model: LTS101-700D-2 - Engine type: Turbo-shaft - Power: 732 hp - Data sheet: [TCDS E5NE](https://openairdocs.org/tcds/E5NE) (OpenAirDocs) - Holder: Intermountain Turbine Services Inc. - Installed in: 8 registered aircraft - Page: https://openairdocs.org/engine/honeywell-lts101-700d-2 Model codes come from the FAA registry's reference file. ## ADs that may apply (OpenAirDocs) Matched to this engine model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. - [AD 2011-23-13](https://openairdocs.org/ad/2011-23-13): Power turbine governors (PTG) · Honeywell International LTS101-600A-2, LTS101-600A-3, LTS101-600A-3A and 1 more. Effective Nov 29, 2011 - [AD 2011-08-06](https://openairdocs.org/ad/2011-08-06): Power turbine rotors · Honeywell International LTP 101-600A-1A, LTP 101-700A-1A, LTS101-600A-2 and 10 more. Effective May 17, 2011 - [AD 2002-03-09 R1](https://openairdocs.org/ad/2002-03-09-R1): Impellers · Honeywell International LTP 101-600, LTP 101-600A, LTP 101-600A-1A and 14 more. Effective Mar 27, 2002 - [AD 2001-22-07](https://openairdocs.org/ad/2001-22-07): Rigid Tube Fuel Manifold Assemblies · Honeywell International LTP 101-600, LTP 101-600A, LTP 101-600A-1A and 14 more. Effective Nov 30, 2001 - [AD 96-12-05](https://openairdocs.org/ad/96-12-05): Turbine rotors · Honeywell International LTP 101-600, LTP 101-600A, LTP 101-600A-1A and 14 more. Effective Aug 12, 1996 ## Registered aircraft (8) - [N204CH](https://openairdocs.org/aircraft/N204CH): [Coastal Helicopters](https://openairdocs.org/faa-owner/COASTAL%20HELICOPTERS), [Juneau, AK](https://openairdocs.org/faa-place/AK/Juneau), built 1981, S/N 2054 - [N350HD](https://openairdocs.org/aircraft/N350HD): [T Scott Dunn Construction Inc](https://openairdocs.org/faa-owner/T%20SCOTT%20DUNN%20CONSTRUCTION%20INC), [Phoenix, OR](https://openairdocs.org/faa-place/OR/Phoenix), built 2007, S/N 4343 - [N350SH](https://openairdocs.org/aircraft/N350SH): [Jc Aircraft Leasing LLC](https://openairdocs.org/faa-owner/JC%20AIRCRAFT%20LEASING%20LLC), [Wasilla, AK](https://openairdocs.org/faa-place/AK/Wasilla), built 1998, S/N 3073 - [N3598D](https://openairdocs.org/aircraft/N3598D): [Pope James Dean](https://openairdocs.org/faa-owner/POPE%20JAMES%20DEAN), [Lewiston, ID](https://openairdocs.org/faa-place/ID/Lewiston), built 1979, S/N 1152 - [N668MM](https://openairdocs.org/aircraft/N668MM): [Colorado Highland Holdings LLC](https://openairdocs.org/faa-owner/COLORADO%20HIGHLAND%20HOLDINGS%20LLC), [Durango, CO](https://openairdocs.org/faa-place/CO/Durango), built 1991, S/N 2580 - [N752CH](https://openairdocs.org/aircraft/N752CH): [Csc Delaware Trust Co Trustee](https://openairdocs.org/faa-owner/CSC%20DELAWARE%20TRUST%20CO%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 1986, S/N 1906 - [N79FX](https://openairdocs.org/aircraft/N79FX): [Southern Helicopters Inc](https://openairdocs.org/faa-owner/SOUTHERN%20HELICOPTERS%20INC), [Sunshine, LA](https://openairdocs.org/faa-place/LA/Sunshine), built 1979, S/N 1204 - [N966FS](https://openairdocs.org/aircraft/N966FS): [Tumbleweed Leasing Co Inc](https://openairdocs.org/faa-owner/TUMBLEWEED%20LEASING%20CO%20INC), [West Jordan, UT](https://openairdocs.org/faa-place/UT/West%20Jordan), built 1989, S/N 2301 ## NTSB investigations (6) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB ANC22LA015](https://openairdocs.org/ntsb/ANC22LA015), Dec 25, 2021: Eurocopter France AS350B2 (N752CH), Kahului, HI, substantial damage. Probable cause: The pilot’s abrupt flight control inputs to correct for dynamic rollover, resulting in a hard landing. - [NTSB ANC20LA083](https://openairdocs.org/ntsb/ANC20LA083), Aug 25, 2020: Eurocopter AS350 (N160SH), Ninilchik, AK, substantial damage. Probable cause: A loss of engine power for an undetermined reason. - [NTSB GAA19CA139](https://openairdocs.org/ntsb/GAA19CA139), Feb 18, 2019: Airbus A350 (N350ST), Eureka, AK, substantial damage. Probable cause: The pilot's selection of unsuitable terrain for landing on snow-covered mountainous terrain with steep rocks above, which resulted in loose rocks damaging the main rotor blades and the subsequent… - [NTSB ANC17LA025](https://openairdocs.org/ntsb/ANC17LA025), May 23, 2017: Airbus AS350 (N207CH), Juneau, AK, substantial damage. Probable cause: The pilot's decision to depart into an area of degraded visual meteorological and flat light conditions, which resulted in a loss of visual references and subsequent controlled flight into terrain. - [NTSB WPR17LA014](https://openairdocs.org/ntsb/WPR17LA014), Oct 28, 2016: Aerospatiale AS350 (N369BD), Starbuck, WA, substantial damage. Probable cause: A total loss of engine power due to fuel exhaustion, which resulted from the pilot’s reliance on the fuel gauge that was displaying an incorrect fuel amount due to the separation of the fuel… - [NTSB WPR09IA140](https://openairdocs.org/ntsb/WPR09IA140), Mar 3, 2009: Eurocopter AS 350 B2 (N197AE), Peach Springs, AZ, incident, minor damage. Probable cause: A loss of engine power due to the failure of the number three engine bearing as a result of oil starvation due to coked oil obstructing the oil passages. ## FAA accident and incident reports (10) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Accident 20211225020589A](https://openairdocs.org/incident/20211225020589A), Dec 25, 2021: Eurocopter France AS350B2 (N752CH), Kahului, HI, Substantial damage. On December 25, 2021 at maui heliport, Kahului hi, while attempting to lift the aircraft (N752CH) to a hover to taxi across the ramp the PIC noted the aircraft… - [Accident 20200825012599A](https://openairdocs.org/incident/20200825012599A), Aug 25, 2020: Eurocopter France AS350B2 (N160SH), Mount Iliamna, AK, Substantial damage. As aircraft approached the helipad (approximately 25 feet away horizontally) with very low forward airspeed, slightly above the level of the pad the engine… - [Accident 20190218010359A](https://openairdocs.org/incident/20190218010359A), Feb 18, 2019: Eurocopter France AS350B2 (N350ST), Glacier View, AK, Substantial damage. AS-350 was conducting heliski operations and unloading skiers during toe-in maneuver on ~20 degree slope at approx. 5500 foot level. Slope was direct lighted… - [Accident 20170522005739A](https://openairdocs.org/incident/20170522005739A), May 22, 2017: Eurocopter France AS350B2 (N207CH), Juneau, AK, Destroyed. Aircraft departed dogsled camp following the right side down the glacier maintaining visual reference with the rock wall. Approximately 3/4 of a mile down the… - [Incident 20141221023539I](https://openairdocs.org/incident/20141221023539I), Dec 21, 2014: Eurocopter AS 350 B2 (N9511), Honolulu, HI, Minor damage. On December 21, 2014, N9511 an AS350B2 helicopter operated by schuman aviation company inc., had just landed at Honolulu International Airport (phnl) after… - [Incident 20140228003319I](https://openairdocs.org/incident/20140228003319I), Feb 28, 2014: Aerospatiale AS350B2 (N204CH), Haines, AK, Minor damage. Helicopter struck known object with main rotor blade. Landed at airport without further incident. - [Incident 20120513007649I](https://openairdocs.org/incident/20120513007649I), May 13, 2012: Eurocopter AS 350 B2 (N9511), Honolulu, HI, No damage. Trash on taxiway was ingested into the tail rotor of the helicopter. Pilot aborted take off and completed an emergency landing. Upon shut down the pilot… - [Incident 20110704019349I](https://openairdocs.org/incident/20110704019349I), Jul 4, 2011: Eurocopter AS 350 BA (N250AH), Prosperity, PA, No damage. On July 4, 2011 at approximately 0845 eastern daylight savings time, aircraft N250AH, a Eurocopter AS-350-BA, operating under title 14 CFR part 133, operated… - [Incident 20090303003149I](https://openairdocs.org/incident/20090303003149I), Mar 3, 2009: Snias AS350B2 (N197AE), Peach Springs, AZ, Minor damage. (-23) Aircraft AS350B2, N197AE piloted by [privacy data omitted], while performing a sightseeing tour over the Grand Canyon the aircraft lost engine power the… - [Incident 20010907024869I](https://openairdocs.org/incident/20010907024869I), Sep 7, 2001: Snias AS350BA (N350SH), Grand Canyon, AZ, Minor damage. (-23) Aircraft struck a small hawk which caused a baseball sized hole in the nose of the aircraft. The pilot flew about one minute to a safe landing site. ## Service difficulty reports (118, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR 2022FA0000456](https://openairdocs.org/sdr/2022FA0000456), Aug 18, 2022: HOUSING. WORN. 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 HELI - [SDR CA190626013](https://openairdocs.org/sdr/CA190626013), Jun 23, 2019: LOCK. 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) - [SDR 2019F00114](https://openairdocs.org/sdr/2019F00114), Jun 15, 2019: DISPLAY. MALFUNCTIONED. 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 CONT - [SDR CA190312016](https://openairdocs.org/sdr/CA190312016), Mar 11, 2019: BEARING. MAKING METAL. (CAN) GEARBOX GENERATING METAL FLAKE. GEARBOX REPAIRED BY ORIGINAL EQUIPMENT MANUFACTURER WITHIN 8 HOURS. GEARBOX REMOVED AND RETURNED TO ORIGINAL EQUIPMENT MAN - [SDR CA190307005](https://openairdocs.org/sdr/CA190307005), Mar 6, 2019: LEAF 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- - [SDR CA190220031](https://openairdocs.org/sdr/CA190220031), Jul 29, 2018: LINE. LEAKING. (CAN) HYDRAULIC LINE FOUND LEAKING THROUGH THE BRAID (TC# 20190220031) - [SDR EVCA2017111400001](https://openairdocs.org/sdr/EVCA2017111400001), Nov 12, 2017: LINE. LEAKING. 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), Jan 20, 2017: TURBINE WHEEL. FAILED. 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 FAIL - [SDR CA160224009](https://openairdocs.org/sdr/CA160224009), Feb 12, 2016: GEARBOX. 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 TIM - [SDR CA151105002](https://openairdocs.org/sdr/CA151105002), Nov 4, 2015: O-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 FILTE - [SDR CA151202011](https://openairdocs.org/sdr/CA151202011), Nov 2, 2015: TRANSDUCER. 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 TESTE - [SDR CA151214015](https://openairdocs.org/sdr/CA151214015), Oct 28, 2015: BRACKET. 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. - [SDR CA150925012](https://openairdocs.org/sdr/CA150925012), Sep 22, 2015: HYDRAULIC 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 - [SDR CA150925006](https://openairdocs.org/sdr/CA150925006), Sep 21, 2015: FUEL 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 RETUR - [SDR CA151202012](https://openairdocs.org/sdr/CA151202012), Sep 15, 2015: GEAR. 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 F - [SDR CA150902007](https://openairdocs.org/sdr/CA150902007), Sep 2, 2015: DRIVE 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 - [SDR CA150727023](https://openairdocs.org/sdr/CA150727023), Jul 25, 2015: HOSE. 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. - [SDR CA150813003](https://openairdocs.org/sdr/CA150813003), Jul 22, 2015: FLEX 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 - [SDR CA150617002](https://openairdocs.org/sdr/CA150617002), Jun 15, 2015: HYDRAULIC 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 & TH - [SDR CA150616025](https://openairdocs.org/sdr/CA150616025), May 25, 2015: PUMP. LEAKING. (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), May 19, 2015: FLEX 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 COUPLI - [SDR CA150430006](https://openairdocs.org/sdr/CA150430006), Apr 29, 2015: LINE. 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 DEPAR - [SDR CA150413005](https://openairdocs.org/sdr/CA150413005), Apr 11, 2015: SHAFT. SHEARED. (CAN) STARTER GENERATOR SHEARED SHAFT ON INITIATION OF START. - [SDR CA150316008](https://openairdocs.org/sdr/CA150316008), Mar 2, 2015: GOVERNOR. 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 A - [SDR CA150210007](https://openairdocs.org/sdr/CA150210007), Feb 9, 2015: ENCODER. 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 CI - [SDR CA150210006](https://openairdocs.org/sdr/CA150210006), Feb 5, 2015: BLADE. 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 & T - [SDR CA141208014](https://openairdocs.org/sdr/CA141208014), Dec 4, 2014: ANGLE. 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. - [SDR 7EMA20140930007](https://openairdocs.org/sdr/7EMA20140930007), Sep 28, 2014: FUEL CONTROL. LEAKING. ON DAILY INSPECTION TECHNICIAN NOTICED FUEL PUMP LEAKING AT ENG MATING. UPON PUMP REMOVAL DISCOVERED FUEL CONTROL DRIVE BEARING BLUE GREASE LUBRICATION EXCESSIV - [SDR CA140818006](https://openairdocs.org/sdr/CA140818006), Aug 17, 2014: SHAFT. 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 H - [SDR CA140808009](https://openairdocs.org/sdr/CA140808009), Aug 6, 2014: ENGINE. 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 M - [SDR CA140423013](https://openairdocs.org/sdr/CA140423013), Apr 22, 2014: SHAFT. BROKEN. (CAN) THE STARTER GENERATOR DRIVESHAFT, BROKE INFLIGHT ILLUMINATING GENERATOR FAIL LIGHT ON CAUTION PANEL. - [SDR CA140214005](https://openairdocs.org/sdr/CA140214005), Feb 14, 2014: STARFLEX. DEBONDED. (CAN) FOUND THE STARFLEX DEBONDED BETWEEN THE BUSHING AND THE SPINDLE. - [SDR CA131101003](https://openairdocs.org/sdr/CA131101003), Oct 31, 2013: BLADE. 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 - [SDR CA131023011](https://openairdocs.org/sdr/CA131023011), Oct 23, 2013: BUSHING. 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 HO - [SDR CA131007026](https://openairdocs.org/sdr/CA131007026), Oct 2, 2013: POWER 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 - [SDR C3OR201309270001](https://openairdocs.org/sdr/C3OR201309270001), Sep 27, 2013: COMBUST CHAMBER. DAMAGED. 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 ANO - [SDR CA130816003](https://openairdocs.org/sdr/CA130816003), Aug 14, 2013: PUMP. 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, DR - [SDR CA130816002](https://openairdocs.org/sdr/CA130816002), Aug 13, 2013: SHAFT. 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. - [SDR CA130814002](https://openairdocs.org/sdr/CA130814002), Aug 12, 2013: TRANSMITTER. 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 WI - [SDR CA130730003](https://openairdocs.org/sdr/CA130730003), Jul 26, 2013: PULLEY. 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 U - [SDR CA130624004](https://openairdocs.org/sdr/CA130624004), Jun 21, 2013: MODULATOR. 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 - [SDR CA130525002](https://openairdocs.org/sdr/CA130525002), May 24, 2013: STARTER 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 O - [SDR CA130521011](https://openairdocs.org/sdr/CA130521011), May 16, 2013: YOKE. 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 - [SDR CA130521020](https://openairdocs.org/sdr/CA130521020), May 16, 2013: TRANSMITTER. 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 AIRFR - [SDR CA130423001](https://openairdocs.org/sdr/CA130423001), Apr 21, 2013: SERVO. 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 UN - [SDR CA130321008](https://openairdocs.org/sdr/CA130321008), Mar 13, 2013: SKIN. DEFORMED. (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), Mar 4, 2013: FUEL 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 - [SDR CA130213001](https://openairdocs.org/sdr/CA130213001), Feb 12, 2013: MOUNT. 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. - [SDR CA130208006](https://openairdocs.org/sdr/CA130208006), Feb 7, 2013: SERVO. 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 PEDA - [SDR CA130208003](https://openairdocs.org/sdr/CA130208003), Feb 6, 2013: HOSE. 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 BRAI All 118: https://openairdocs.org/engine/honeywell-lts101-700d-2/reports.md ## PMA parts (OpenAirDocs) (17) Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this engine model on its data sheet, so check the FAA record before relying on it. Newest first. - [4-131-010-30](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192455809320241018160209.0001): Liner Assy, Combustion Chamber. Honeywell International Inc. · PMA PQ1222NM · Replaces 4-131-010-30 · Jul 2, 2024 - [4-111-015-19](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168494359020241018160209.0001): Disk – First Turbine Rotor. Honeywell International Inc. · PMA PQ1222NM · Replaces 4-111-015-19 · Jul 2, 2024 - [4-111-058-06](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID150699376320241018160209.0001): Blade, Turbine Rotor – Stage 1 – Low Flow. Honeywell International Inc. · PMA PQ1222NM · Replaces 4-111-058-06 · Jul 2, 2024 - [4-141-290-30](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135990764120241018160210.0001): Turbine Rotor. Honeywell International Inc. · PMA PQ1222NM · Replaces 4-141-290-30 · Jul 2, 2024 - [4-111-062-06](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132122400520241018160209.0001): Disk, Rotor – HP Turbine. Honeywell International Inc. · PMA PQ1222NM · Replaces 4-111-062-06 · Jul 2, 2024 - [4-131-070-04](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID130507704220241018160210.0001): Curl, Comb Chamber Assy. Honeywell International Inc. · PMA PQ1222NM · Replaces 4-131-070-04 · Jul 2, 2024 - [4-111-014-65](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID118223391920241018160208.0001): Blade, Turbine Rotor, Turbine Engine. Honeywell International Inc. · PMA PQ1222NM · Replaces 4-111-014-65 · Jul 2, 2024 - [2691794HT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID112924083920240802140701.0001): Bearing, Ball (Drive). HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2691794 · Apr 4, 2024 - [117110-01A2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID638107735520210623160059.0001): High Pressure Filter. Triumph Engine Control Systems, LLC · PMA PQ0108NE · Replaces 4-301-123-03 · Feb 1, 2021 - [117110-01A2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID476789967820210629213700.0001): High Pressure Filter. Triumph Engine Control Systems, LLC · PMA PQ0108NE · Replaces 4-301-123-03 · Feb 1, 2021 - [117100-01A2](https://drs.faa.gov/browse/excelExternalWindow/1536F74F8B34E14C86258631005436CD.0001): High Pressure Filter. Triumph Engine Control Systems, LLC · PMA PQ0108NE · Replaces 4-301-123-03 · Nov 29, 2020 - [2537678HT](https://drs.faa.gov/browse/excelExternalWindow/0B599622025D67ED86258550006342B5.0001): Screw. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2537678 · Apr 30, 2019 - [116115A6](https://drs.faa.gov/browse/excelExternalWindow/61251AE719378D7786258489004290ED.0001): PUMP ASSEMBLY COMPLETE. Triumph Engine Control Systems, LLC · PMA PQ0108NE · Replaces 4-301-377-10 · Mar 20, 2019 - [116115A7](https://drs.faa.gov/browse/excelExternalWindow/530C058E13EB78008625848900429103.0001): PUMP ASSEMBLY COMPLETE. Triumph Engine Control Systems, LLC · PMA PQ0108NE · Replaces 4-301-377-13 · Mar 20, 2019 - [2537678HT](https://drs.faa.gov/browse/excelExternalWindow/089BB4F387781C0986257F0F008149F9.0001): Screw. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2537678 · Nov 22, 2015 - [AC6091F-8Y99](https://drs.faa.gov/browse/excelExternalWindow/CFA269032F540EDB862571D1004A38E4.0001): Filter Element. Pall Aeropower Corp · PMA PQ1021CE · Replaces 4-301-216-01 · Apr 26, 2006 - [ACA684F-40Y2](https://drs.faa.gov/browse/excelExternalWindow/CDFC4BD4EE0CCD3F862571D1004A38BA.0001): Filter Element. Pall Aeropower Corp · PMA PQ1021CE · Replaces 4-301-106-04 · Apr 26, 2006 --- 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.