# Honeywell LTS101-600A-2 - Type: Engine model (FAA registry) - Registry code: 33817 - Manufacturer (registry): HONEYWELL - Model: LTS101-600A-2 - Engine type: Turbo-shaft - Power: 615 hp - Data sheet: [TCDS E5NE](https://openairdocs.org/tcds/E5NE) (OpenAirDocs) - Holder: Intermountain Turbine Services Inc. - Installed in: 0 registered aircraft - Page: https://openairdocs.org/engine/honeywell-lts101-600a-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 2009-24-12](https://openairdocs.org/ad/2009-24-12): Gas generator · Honeywell International LTP 101-600A-1A, LTP 101-700A-1A, LTS101-600A-2 and 12 more. Effective Jan 4, 2010 - [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 2001-25-04](https://openairdocs.org/ad/2001-25-04): Fuel Controls · Honeywell International LTP 101-600A-1A, LTP 101-700A-1A, LTS101-600A-2 and 1 more. Effective Jan 23, 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 2001-17-15](https://openairdocs.org/ad/2001-17-15): Engine Fuel Pumps · Honeywell International LTP 101-600A-1A, LTP 101-700A-1A, LTS101-600A-2 and 2 more. Effective Oct 1, 2001 - [AD 96-12-27](https://openairdocs.org/ad/96-12-27): Gas Generator Turbine Disk · Honeywell International LTP 101-600, LTP 101-600A, LTP 101-600A-1A and 21 more. Effective Aug 19, 1996 - [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 - [AD 96-10-04](https://openairdocs.org/ad/96-10-04): Fuel control · Honeywell International LTS101-600A-2 and LTS101-600A-3. Effective Jun 13, 1996 - [AD 96-06-10](https://openairdocs.org/ad/96-06-10): Power turbine (PT) disk · Honeywell International LTS101-600A-2, LTS101-600A-3 and LTS101-750B-2. Effective May 28, 1996 - [AD 95-16-04](https://openairdocs.org/ad/95-16-04): Axial Compressor Rotors · Honeywell International LTP 101-600, LTP 101-600A, LTP 101-600A-1A and 21 more. Effective Oct 2, 1995 - [AD 94-18-06](https://openairdocs.org/ad/94-18-06): Bearings · Honeywell International LTP 101-600, LTP 101-600A, LTP 101-600A-1A and 21 more. Effective Sep 26, 1994 - [AD 93-13-11](https://openairdocs.org/ad/93-13-11): Gas Generator Turbine Rotor Disk · Honeywell International LTP 101-600, LTP 101-600A, LTP 101-600A-1A and 22 more. Effective Nov 8, 1993 - [AD 92-15-07](https://openairdocs.org/ad/92-15-07): Integrally Cast Power Turbine (PT) Rotor Blade · Honeywell International LTP 101-600, LTP 101-600A, LTP 101-600A-1A and 21 more. Effective Sep 2, 1992 - [AD 88-14-01](https://openairdocs.org/ad/88-14-01): Power Turbine Disk · Honeywell International LTS101-600A, LTS101-600A-1, LTS101-600A-2 and 17 more. Effective Jul 6, 1988 - [AD 86-10-04](https://openairdocs.org/ad/86-10-04): Gas Producer (G.P.) Blade · Honeywell International LTP 101-600A-1A, LTP 101-700A-1A, LTS101-600A-2 and 11 more. Effective May 16, 1986 - [AD 84-02-07](https://openairdocs.org/ad/84-02-07): Output Gear Assembly and Torquemeter Gear Assembly · Honeywell International LTS101-600A-2. Effective May 7, 1984 - [AD 83-16-03](https://openairdocs.org/ad/83-16-03): Install Overspeed Limiter · Honeywell International LTS101-600A-2. Effective Aug 25, 1983 - [AD 79-06-06 R2](https://openairdocs.org/ad/79-06-06-R2): Lubrication System Contamination · Honeywell International LTP 101-600, LTP 101-600A, LTS101-600A and 3 more. Effective Jun 2, 1980 - [AD 79-20-03](https://openairdocs.org/ad/79-20-03): Fuel Control, Fuel Pump And Oil Pump Drive Gears · Honeywell International LTP 101-600, LTP 101-600A, LTP 101-600A-1A and 5 more. Effective Sep 26, 1979 - [AD 84-14-01](https://openairdocs.org/ad/84-14-01): T4 Indicator System Check · Honeywell International LTS101-600A-2 Historical (superseded or no longer in force): - [AD 95-09-02](https://openairdocs.org/ad/95-09-02) (historical): Fuel Pumps · Honeywell International LTP 101-600, LTP 101-600A, LTP 101-600A-1A and 12 more. Effective May 10, 1995 ## Registered aircraft None registered with this engine model now. ## NTSB investigations None matched to aircraft with this engine model. ## FAA accident and incident reports None matched to aircraft with this engine model. ## Service difficulty reports (23) As reported by operators and repair stations, by the model named in the report. - [SDR CA111007001](https://openairdocs.org/sdr/CA111007001), Oct 5, 2011: COMPRESSOR. STALLED. (CAN) WHILE ON FINAL APPROACH TO A WELL SITE, THE PILOT HEARD A LOUD BANG FOLLOWED BY A SEVERE AIRFRAME VIBRATION. AN AUTOROTATION WAS INITIATED AND A NORMAL LA - [SDR CA080117003](https://openairdocs.org/sdr/CA080117003), Jan 11, 2008: BYPASS VALVE. CRACKED. (CAN) THE AC LANDED AFTER FLYING SEVERAL HOURS ON A SEISMIC JOB. WHILE DOING A QUICK DI, THE ENGINEERS NOTICED FUEL ON THE TRANSMISSION DECK. IT WAS DISCOVERED - [SDR CA071211008](https://openairdocs.org/sdr/CA071211008), Dec 10, 2007: WYE PIPE. LEAKING. (CAN) THE AC WAS BEING REFUELED OUT SIDE WHEN FUEL STARTED POURING ON THE GROUND FROM SOMEWHERE IN THE FUEL TANK AREA. FURTHER INVESTIGATION REVEALED THE (Y) CO - [SDR CA070321010](https://openairdocs.org/sdr/CA070321010), Mar 16, 2007: FCU. FAILED. (CAN) THE ENGINE FLAMED OUT WHILE THE THROTTLE WAS BEING RETARDED DURING A PRACTICE AUTOROTATION. THE POSITION OF THE THROTTLE AT THE TIME OF THE FLAME OUT WAS - [SDR CA070204001](https://openairdocs.org/sdr/CA070204001), Feb 1, 2007: CHANNEL. CRACKED. (CAN) DURING AN UNSCHEDULED MAINTENANCE PROCEDURE OF THE VIBRATION DAMPER ASSEMBLIES UNDER THE CABIN FLOOR, IT WAS FOUND THROUGH THE USE OF A BOROSCOPE THAT THE - [SDR CA060612006](https://openairdocs.org/sdr/CA060612006), Jun 10, 2006: UNKNOWN. UNKNOWN. ON FINAL APPROACH, APPROX 300 FT AGL, PILOT HEARD LOW ROTOR HORN ACTIVATE AND ENG LOOSE PWR. A SUCCESSFUL AUTOROTATION WAS COMPLETED WITH NO FURTHER INCIDENT. A - [SDR CA060605011](https://openairdocs.org/sdr/CA060605011), May 29, 2006: GOVERNOR. MALFUNCTIONED. (CAN) HELICOPTER STARTED NORMALLY BUT WHEN THE THROTTLE WAS ADVANCED TO THE GATE (100 PERCENT NR), THE MAIN ROTOR STARTED OVERSPEEDING (400 RPM APPROX). THE THR - [SDR CA050609016](https://openairdocs.org/sdr/CA050609016), Apr 6, 2005: FUEL CONTROL. MISRIGGED. (CAN) FCU INSTALLED. PILOT DID THE FIRST START AND THE T4 INDICATED 865C AT THE HIGHEST POINT BEFORE HE SHUT IT DOWN. FCU CHECKED AND FOUND THROTTLE RIGGING WAS - [SDR CA041110010](https://openairdocs.org/sdr/CA041110010), Aug 20, 2004: CONNECTOR. UNSERVICEABLE. (CAN) WHEN INSTALLING A REPLACEMENT BATTERY, NOTICED THE TEMP SENSOR WIRING HARNESS DID NOT HAVE A JUMPER WIRE. FURTHER INSPECTION REVEALED THAT THERE WAS NO SH - [SDR CA040604007](https://openairdocs.org/sdr/CA040604007), May 24, 2004: MODULATOR. FAILED. (CAN) PILOT HEARD AND FELT LOUD POPPING NOISE FROM ENGINE ACCOMPANIED WITH LOSS OF POWER. AIRCRAFT LANDED SUCCESSFULLY. FLOW FENCE PROBLEM SUSPECTED. AIRFLOW MO - [SDR CA040315007](https://openairdocs.org/sdr/CA040315007), Sep 11, 2003: LINK. BROKEN. (CAN) DURING NORMAL CRUISE FLIGHT, THE PILOT NOTICED A SUDDEN SHARP RISE IN T4 (TOT) STILL WITHIN LIMITS. AFTER RETURNING TO BASE, ONE OF THE LINKS CONTROLLING - [SDR CA040315006](https://openairdocs.org/sdr/CA040315006), Aug 27, 2003: GOVERNOR. FAILED. (CAN) MAIN ROTOR RPM WAS FOUND TO OSCILLATE DURING CRUISE FLIGHT AND SOMETIMES DROOP DOWN -5 RPM NR. REPLACING FUEL CONTROL UNIT, FUEL PUMP AND GOVERNOR DID NOT - [SDR CA030312003](https://openairdocs.org/sdr/CA030312003), Feb 26, 2003: BELT. BROKEN. (CAN) ON DESCENT FOR THE BASE, THE CAUTION HORN AS WELL AS (HYDRAULIC PRESSURE) LIGHT CAME ON. A/C LANDED WITHOUT INCIDENT. UPON INSPECTION, HYDRAULIC PUMP BELT - [SDR CA021217001](https://openairdocs.org/sdr/CA021217001), Nov 10, 2002: NOZZLE. ERODED. (CAN) DURING DISASSEMBLY OF ENGINE, THE THREE RING SEALING FEATURE OF NOZZLE WAS FOUND SEPARATED FROM THE NOZZLE, AFT OF THE VANE TRAILING EDGE. SEPARATION IS A - [SDR CA011109008](https://openairdocs.org/sdr/CA011109008), Oct 9, 2001: FRICTION RING. FAILED. (CAN) LOCK PIN NR 10 EITHER NOT PROPERLY INSTALLED OR CAME LOOSE ALLOWING NUT NR 9 TO VIBRATE LOOSE FROM LOWER THREAD PORTION OF COLLAR NR 8, THIS ALLOWED THE E - [SDR CA010725024](https://openairdocs.org/sdr/CA010725024), Jul 4, 2001: ROD END. SEPARATED. (CAN) DURING POST FLIGHT INSPECTION OF AIRCRAFT IT WAS NOTICED THAT THE MAIN ROTOR PITCH LINK ROD AND RETAINER HAD SEPARATED FROM ROD END. PILOT CONFIRMED THAT - [SDR CA010704003](https://openairdocs.org/sdr/CA010704003), Jun 28, 2001: MANIFOLD. LEAKING. (CAN) FUEL FOUND ON ENGINE DECK DURING DAILY INSPECTION. GROUND RUN AND LEAK CHECKPERFORMED. FUEL FOUND EMANATING FROM LEAK IN FUEL MANIFOLD ASSEMBLY. MANIFOLD - [SDR CA001218015](https://openairdocs.org/sdr/CA001218015), Nov 8, 2000: PIN. BROKEN. (CAN) THE BROKEN PIN WAS DISCOVERED STILL SITTING IN PLACE INSIDE THE TWO BLADE PINS. THE PILOT CLAIMS TO HAVE DONE AN APPROPRIATE PRE-FLIGHT CHECK THAT MORNING - [SDR CA000511010](https://openairdocs.org/sdr/CA000511010), Mar 30, 2000: LATCH. MALFUNCTIONED. (CAN) IT WAS NOTICED THAT 2 OF THE FOUR SEAT BELT LATHCHES DO NO ALWAYS ENGAGE PROPERLY. WHEN THE BUCKLE IS INSERTED ALL THE WAY INTO THE LATCH, IT SOUNDS AN D - [SDR CA991210002](https://openairdocs.org/sdr/CA991210002), Oct 22, 1999: SHACKLE. FAILED. (CAN) WHILE TESTING A SKISMIC BIRD, THE PILOT FELT THE LOAD RELEASE FROM THE AIRCRAFT. THE CARGO HOOK WAS FUNCTIONALLY TESTED BEFORE AND AFTER THE FLIGHT AND FO - [SDR CA990323025](https://openairdocs.org/sdr/CA990323025), Jan 27, 1999: COWL. SEPARATED. (CAN) DURING FLIGHT, THE FORWARD BELLY COWLING SEPARATED FROM THE AIRCRAFT AND LANDED IN A FIELD. THE AIRCRAFT LANDED WITHOUT INCIDENT. SUBSEQUENT INVESTIGATION - [SDR CA970916017](https://openairdocs.org/sdr/CA970916017), Sep 3, 1997: SCREW. WRONG PART. (CAN) DURING DISASSEMBLY OF DRIVE SHAFT, 3 OF 12 SCREWS FOUND WERE THE WRONG TYPE. THERE WAS NO SPLIT PIN HOLE, AND THEY HAD BEEN INSTALLED WITH A HEXAGONAL, IN - [SDR 96ZZZX1032](https://openairdocs.org/sdr/96ZZZX1032), Apr 1, 1995: BEARING. FAILED. AFTER ENGINE TEAR-DOWN, THE NR 19 BEARING WAS FOUND BROKEN IN 3 PLACES AROUND THE OUTER RACE. THE BEARING IS A SLIP/FIT IN THE GEARBOX AND THE BORE WAS WORN FRO ## PMA parts (OpenAirDocs) (195, first 50) 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 - [2539533HT](https://drs.faa.gov/browse/excelExternalWindow/FDF710A0D9BAAADD8625855000632B9C.0001): Bearing, Sintered. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2539533 · Apr 30, 2019 - [951190HT](https://drs.faa.gov/browse/excelExternalWindow/FC8B8869AAFBA24A8625855000632D54.0001): Pin, Sraight, Headless. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 951190 · Apr 30, 2019 - [197498HT](https://drs.faa.gov/browse/excelExternalWindow/F58363F6C29A0E2C8625855000636674.0001): Nut, Self-Locking. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 197498 · Apr 30, 2019 - [2543791HT](https://drs.faa.gov/browse/excelExternalWindow/F497876A15FC19DE8625855000638525.0001): Nut, Plain. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2543791 · Apr 30, 2019 - [2543598HT](https://drs.faa.gov/browse/excelExternalWindow/ECA18564BCB7E7E0862585500063865B.0001): Bellows Assembly (Governor). HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2543598 · Apr 30, 2019 - [336132HT](https://drs.faa.gov/browse/excelExternalWindow/E07190E2A02F10498625855000636717.0001): Tapered Pin, Split. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 336132 · Apr 30, 2019 - [2537184HT](https://drs.faa.gov/browse/excelExternalWindow/CF0C0BE63149DF618625855000638483.0001): Split Head Ring. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2537184 · Apr 30, 2019 - [2520561HT](https://drs.faa.gov/browse/excelExternalWindow/C93D07A85055A49E86258550006358AA.0001): Roller. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2520561 · Apr 30, 2019 - [2522105HT](https://drs.faa.gov/browse/excelExternalWindow/C831F72FFA3592EE8625855000633FF3.0001): Spacer. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2522105 · Apr 30, 2019 - [2543133HT](https://drs.faa.gov/browse/excelExternalWindow/C1075D8C43C8BBEE8625855000632CB1.0001): Cover Assembly. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2543133 · Apr 30, 2019 - [2523475HT](https://drs.faa.gov/browse/excelExternalWindow/C0E2E0F3CEAF58978625855000632DF6.0001): Gasket. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2523475 · Apr 30, 2019 - [2522102HT](https://drs.faa.gov/browse/excelExternalWindow/BE78A04D762789BA8625855000635942.0001): Pin, Straight, Headless. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2522102 · Apr 30, 2019 - [2523280HT](https://drs.faa.gov/browse/excelExternalWindow/BD2D6F5C8ACE954186258550006329A7.0001): Seat, Valve. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2523280 · Apr 30, 2019 - [2537508HT](https://drs.faa.gov/browse/excelExternalWindow/AB6226D24673A7D586258550006330BA.0001): Washer, Spring Tension. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2537508 · Apr 30, 2019 - [2523237HT](https://drs.faa.gov/browse/excelExternalWindow/A3761C3D79364D138625855000631D0C.0001): Bearing, Ball. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2523237 · Apr 30, 2019 - [2529242HT](https://drs.faa.gov/browse/excelExternalWindow/A0D34607F558EA0D862585500063302A.0001): Spring, Helical, Extension. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2529242 · Apr 30, 2019 - [2520488HT](https://drs.faa.gov/browse/excelExternalWindow/9CC32778DD3467368625855000635816.0001): Gasket. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2520488 · Apr 30, 2019 - [2538982HT](https://drs.faa.gov/browse/excelExternalWindow/9C95C51F6250D76586258550006343F2.0001): Nut. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2538982 · Apr 30, 2019 - [2525104HT](https://drs.faa.gov/browse/excelExternalWindow/984FA7DADBC0CFED8625855000632EF8.0001): Gasket. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2525104 · Apr 30, 2019 - [2520569HT](https://drs.faa.gov/browse/excelExternalWindow/9432CA88F2F1B9128625855000633EBF.0001): Bushing. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2520569 · Apr 30, 2019 - [2543734HT](https://drs.faa.gov/browse/excelExternalWindow/8B394A535BB0AE8E862585500062E3A5.0001): Bearing, Ball. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2543734 · Apr 30, 2019 - [2523282HT](https://drs.faa.gov/browse/excelExternalWindow/889B68627F1BF6D78625855000632A53.0001): Seat, Valve. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2523282 · Apr 30, 2019 - [2523242HT](https://drs.faa.gov/browse/excelExternalWindow/7299489DDD08CEDB8625855000634089.0001): Spacer. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2523242 · Apr 30, 2019 - [2520503HT](https://drs.faa.gov/browse/excelExternalWindow/6FF55BB83A1236CA8625855000631AD3.0001): Bearing, Ball. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2520503 · Apr 30, 2019 - [366783HT](https://drs.faa.gov/browse/excelExternalWindow/6BDB9F5E1EB61600862585500063679B.0001): Washer, Crush. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 366783 · Apr 30, 2019 - [2526008HT](https://drs.faa.gov/browse/excelExternalWindow/6539AB53666D674686258550006391D3.0001): Shaft Assy., Drive. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2526008 · Apr 30, 2019 - [2543226HT](https://drs.faa.gov/browse/excelExternalWindow/5A59E752DA8E60A98625855000632C18.0001): Cover Assembly. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2543226 · Apr 30, 2019 - [2523106HT](https://drs.faa.gov/browse/excelExternalWindow/4CC17275E02B523986258550006359D3.0001): Screen. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2523106 · Apr 30, 2019 - [2539179HT](https://drs.faa.gov/browse/excelExternalWindow/4C489B323A9992148625855000632AF7.0001): Bearing, Sintered. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2539179 · Apr 30, 2019 - [2523549HT](https://drs.faa.gov/browse/excelExternalWindow/45FC85266F9461F58625855000632E87.0001): Tube. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2523549 · Apr 30, 2019 - [2543792HT](https://drs.faa.gov/browse/excelExternalWindow/457DF2F181776F0486258550006385AC.0001): Insert Assembly, Carboloy. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2543792 · Apr 30, 2019 - [2537677HT](https://drs.faa.gov/browse/excelExternalWindow/40BC85624A10FBDE8625855000633134.0001): Pin, Straight, Headless. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2537677 · Apr 30, 2019 - [2523333HT](https://drs.faa.gov/browse/excelExternalWindow/3F8DC35D3825035F862585500063411D.0001): Nut. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2523333 · Apr 30, 2019 - [2544028HT](https://drs.faa.gov/browse/excelExternalWindow/3B1E3F42228359F88625855000636835.0001): Ring, Damper, Bellows. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2544028 · Apr 30, 2019 - [2523240HT](https://drs.faa.gov/browse/excelExternalWindow/3999BB6F4232A600862585500063206A.0001): Packing, Preformed O Ring. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2523240 · Apr 30, 2019 - [2537747HT](https://drs.faa.gov/browse/excelExternalWindow/24F79C028AC52BA486258550006331C3.0001): Diaphragm, By-Pass Valve. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2537747 · Apr 30, 2019 - [2529153HT](https://drs.faa.gov/browse/excelExternalWindow/0D41BC0586E5BAF88625855000632F86.0001): Spring, Helical, Extension. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2529153 · Apr 30, 2019 - [2537678HT](https://drs.faa.gov/browse/excelExternalWindow/0B599622025D67ED86258550006342B5.0001): Screw. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2537678 · Apr 30, 2019 - [343698HT](https://drs.faa.gov/browse/excelExternalWindow/075870B02E230B5B862585500063359B.0001): Pin. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 343698 · 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 - [2522102HT](https://drs.faa.gov/browse/excelExternalWindow/F021B8411976F1BB86257F0F00815030.0001): Pin, Straight, Headless. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2522102 · Nov 22, 2015 - [343698HT](https://drs.faa.gov/browse/excelExternalWindow/E8F990AC4967641486257F0F00814655.0001): Pin. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 343698 · Nov 22, 2015 All of them: https://openairdocs.org/engine/honeywell-lts101-600a-2/pma.md --- 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.